PART NUMBER | DESCRIPTION | EQUIV. | EQUIV. | EQUIV. | EQUIV. | |
---|---|---|---|---|---|---|
001U532A5100000 | DORNIER 328/328 JET SE.4.48A CALIBRATION STANDARD | . | . | . | . | |
00401800-015 | Custom ET Strut Axial Calibration Standard. Material: 7075-T7451 Aluminum. Hole Size: .9062" 1 Coner EDM Notch and 1 Mid-Wall EDM Notch. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
00701058-006 | Custom ET Calibration Standard. Material: 7050-T7451 Aluminum. Hole Size: .9062" 1 Coner EDM Notch and 1 Mid-Wall EDM Notch. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
01083060-001 | Custom Elite Metal Finishing Calibration Standard. Material: 7050-T7451 Aluminum. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
019 | BOEING REFERENCE STANDARD 7075-T6 ALUMINUM 707 57-10-07 PART 6 PG.216..PART 6, 57-10-07 PG.216 | . | . | . | . | |
038 | BOEING 707 REFERENCE STANDARD 2024-T3 ALUMINUM DETAIL 1 FIGURE 8 SHEET 7 BBL 70.5 SPLICE 707-300/400..PART 6, 57-30-07 PG.71 | . | . | . | . | |
039 | BOEING 707 REFERENCE STANDARD 2024-T3 ALUMINUM DETAIL 3 FIGURE 8 SHEET 9 BBL 70.5 SPLICE 707-300/400..PART 6, 57-30-07 PG.73 | . | . | . | . | |
1.0"-1.8" Sizing Cal Block | Ultrasonic Calibration Sizing Standards 1.0"-1.8". Slot MTD's 1.000", 1.200", 1.400",1.600" and 1.800". Size: 1.250"Wide x 2.000" Tall x 12.00" Long | . | . | . | . | |
1/N-02-384 | Nomad Series N22 & N24 Reference Standard. for the inspection of Wing Strut Upper Fittings, Figure 27 Page 51. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
10-0109-00 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, INCONEL 718, 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
1002 | BOEING REFERENCE STANDARD PT 6 51-00-00 Part 6 FIG 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
1003 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 14 and 51-00-06. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
1004 | BOEING REFERENCE STANDARD PT 6 51-00-0 FIG 14 PARAGRAPPH 2.C. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
1005 | BOEING REFERENCE STANDARD PT 6 51-00-00 and 51-00-06, MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
10RS.01.1 | BOEING REFERENCE STANDARD KC10 | . | . | . | . | |
10RS.02 | BOEING REFERENCE STANDARD KC10 FASTENER (NAS1097AD6, S4931919-6 + NAS1252 + NAS21042L) | . | . | . | . | |
10RS.05 | DC-10 REFERENCE STANDARD FASTENER (HLT335-6-4 + NAS1252 + MS21042L, NAS1097-AD6) | . | . | . | . | |
10RS.08 | DC-10 REFERENCE STANDARD FASTENER (MS20426AD5, 2L426-V08 + MAS1080-8, SL426-V06 + NAS1080-6, HL329-5 + MS21042L + NAS1252BL) | . | . | . | . | |
10RS.10.1 | DC-10 REFERENCE STANDARD 55.10.005/.006 FASTENER (HLT335-8 + NAS1252-416H + MS21042L4, HLT335-12 + NAS1252-616H + MS21042L6, HLT335-6 +HL386-6) | . | . | . | . | |
10RS.15a | DC-10 SID REFERENCE STANDARD DETAILS -3,-5 & -7 PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.15b | DC-10 SID REFERENCE STANDARD DETAILS -3,-5, & -5, -501 ASSEMBLY PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.15c | DC-10 SID REFERENCE STANDARD DETAILS -7, -9 & -11, -503 ASSWMBLY PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.17 | DC-10 SID REFERENCE STANDARD DETAIL -3 & -5 PAGE 2-3. MATERIAL: 2024-T3 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.17.1 | DC-10 SID REFERENCE STANDARD DETAIL -3 & -5 PAGE 2-3. MATERIAL: 2024-T3 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.21 | DC-10 REFERENCE STANDARD DETAIL -1 PAGE 1. MATERIAL: 718 INCONEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
10RS.22a | DC-10 REFERENCE STANDARD 54-10-029/.030 | . | . | . | . | |
10RS.23 | DC-10 SID REFERENCE STANDARD DETAIL -1 SHEET 1 PAGE 1. MATERIAL: 6AL-4V TITANIUM. | . | . | . | . | |
10RS.25a | DC-10 SID REFERENCE STANDARD DETAIL -3 PAGE 1. MATERIAL: 7075-T7 ALUMNIUM. | . | . | . | . | |
10RS.25b | DC-10 SID REFERENCE STANDARD DETAIL -1 PAGE 1. MATERIAL: 7075-T7 ALUMNIUM. | . | . | . | . | |
10RS.25c | DC-10 SID REFERENCE STANDARD DETAIL -5 PAGE 1. MATERIAL: 7075-T7 ALUMNIUM. | . | . | . | . | |
10RS.26.1bM | DOUGLAS DC-10 REFERENCE STANDARD 54.10.031/.032 PAGES 1-8 (SHEET1-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
10RS.27b | DC-10 SID REFERENCE STANDARD DETAILS -7,-9 & -11 PAGE 1-6. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.32 | DEC-10 REFERENCE STANDARD 54-10-027 | . | . | . | . | |
10RS.33a | DC-10 REFERENCE STANDARD 54-10-027 | . | . | . | . | |
10RS.33b | DC-10 REFERENCE STANDARD 54-10-027 | . | . | . | . | |
10RS.35 | DC-10 REFERENCE STANDARD, SHEETS 1-4, PAGES 1-4. MATERIAL: 6AL-4V TITNIUM. Includes Test Report and Certificate of Conformance. 54.10.027 | . | . | . | . | |
10RS.36a | DC-10 REFERENCE STANDARD DETAIL RA11005-12-1, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027 | . | . | . | . | |
10RS.36aN | DC-10 REFERENCE STANDARD DETAIL RA11005-12-1, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027 | . | . | . | . | |
10RS.36b | DC-10 REFERENCE STANDARD DETAIL RA11005-12-2, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027 | . | . | . | . | |
10RS.36bN | DC-10 REFERENCE STANDARD DETAIL RA11005-12-2, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027. | . | . | . | . | |
10RS.39.1 | DC-10 SID REFERENCE STANDARD DETAIL -1, -3 & -5 PAGE 1-5. MATERIAL: 7075-T6 ALUMNIUM. Includes Certification Report and COC. | . | . | . | . | |
10RS.43 | DC-10 REFERENCE STANDARD PAGE 1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
10RS.48 | BOEING REFERENCE STANDARD - KC10 FASTENER (NAS1097AD6, MS20470AD6, HLT335-6 + NAS1252-10L + MS21042L3) | . | . | . | . | |
10RS.50 | DOUGLAS DC-10 REFERENCE STANDARD 54.10.031/.032 PAGES 1-5 (SHEET1-5). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
10RS.51-MLG-FTG-FF | MD-10 REFERENCE STANDARD FIGURE 1.1, SHEET 1&2. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.52-1-MLG-FTG-AF | MD-10 REFERENCE STANDARD FIGURE 1.2, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-1-HLDR | MD-10 REFERENCE STANDARD FIXTURE FIGURE 1.3. MATERIAL: BLACK ACETAL(DELRIN). Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-1-MLGF-BUSHG | MD-10 REFERENCE STANDARD FIXTURE FIGURE 1.2. MATERIAL: BLACK ACETAL(DELRIN). Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-1-MLG-FTG-CC-UPR | MD-10 REFERENCE STANDARD FIGURE 1.4, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-2&3-HLDR | MD-10 REFERENCE STANDARD FIXTURE FIGURE 1.4. MATERIAL: BLACK ACETAL(DELRIN). Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-2&3-MLGF-BUSHG | MD-10 REFERENCE STANDARD FIXTURE FIGURE 1.2. MATERIAL: BLACK ACETAL(DELRIN). Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-2-MLG-FTG-AA | MD-10 REFERENCE STANDARD FIGURE 1.5, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.53-3-MLG-FTG-DD | MD-10 REFERENCE STANDARD FIGURE 1.6, SHEET 1&2. MATERIAL: 7075 ALUMINUM. INCLUDES 10RS.53-1 MLGF BUSHG and HLDR. Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
10RS.55-1 | BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -3 SKIN, -53 TEAR STRAP, -63 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
10RS.55-3 | BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -3 SKIN, -53 TEAR STRAP, -163 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
10RS.55-5 | BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -3 SKIN, -53 TEAR STRAP, -363 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
10RS.55-7 | BOEING KC10 ET REFERENCE STANDARD. INCLUDES: -103 SKIN, -53 TEAR STRAP, -563 SHEAR CLIP. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
10RS.bN | DC-10 REFERENCE STANDARD DETAIL RA11005-12-2, SHEET 1 PAGE 1&2. MATERIAL: 4130 STEEL. Includes Test Report and Certificate of Conformance. 54.10.027 | . | . | . | . | |
10RS-52-2-MLG-FTG-AF | MD-10 REFERENCE STANDARD FIGURE 1.3, SHEET 1&2. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. MDC-99K1082 | . | . | . | . | |
125 | BOEING REFERENCE STANDARD 767 PT 6 -51-00-05 FIG 2 PAGE 6 & 737 pART 6 51-00-00 FIGURE 2 PAGE 6 DETAIL II. HOLE SIZES: 0.1875, 0.250, 0.3125, 0.375, 0.4375, 0.500. Material: 4130 or 4340 Cres Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
126 | BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.032 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.036 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.040 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.050 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.063 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.071 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.080 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.090 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.100 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.110 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127-0.125 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.032 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.036 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.040 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.050 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.063 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.072 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.080 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.090 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.100 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.110 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
127A-.125 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
128 | BOEING REFERENCE STANDARD 767 PT 6 51-00-06 FIG 1 | . | . | . | . | |
130A | BOEING THICKNESS STANDARD FOR X-BAND RADOMES DETAIL IV 737 PT 6 53-50-00. MATERIAL: LUCITE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
130B | BOEING THICKNESS STANDARD FOR C-BAND RADOMES DETAIL V 737 PT 6 53-50-00. MATERIAL: LUCITE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
130C | BOEING REFERENCE STANDARD PT 6 53-50-00 | . | . | |||
145-15998-001 | EMBRAER REFERENCE STANDARD 54-50-00 FIG 603, 4340 STEEL | . | . | . | . | |
145-44131-001 | EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Aluminum(7050-T745) Includes Test Report and Certificate of Conformance. | . | . | . | . | |
145-44131-003 | EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Steel(15-SPH 5/8") Includes Test Report and Certificate of Conformance. | . | . | . | . | |
145-44131-005 | EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Titanium(Titanium Galy US AMS2631 CLAI 1/2") Includes Test Report and Certificate of Conformance. | . | . | . | . | |
145-54-0008 | EMBRAER REFERENCE STANDARD 54-50-00 FIG 606, 4340 STEEL | . | . | . | . | |
171-00844-601 16E1 | EMBRAER REFERENCE STANDARD 7075-T7 ALUMINUM, DAN5-5 FASTENER.Includes Test Report and Certificate of Conformance. | 92 | . | . | ||
171T17969-401 | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance. | GSE 503 | . | . | .. | |
171T17973-401 | EMBRAER 170/175/190/195 CALIBRATION STANDARD. PART NUMBER 171T17973-401. Includes Test Report and Certificate of Conformance. | GSE 506 | . | . | . | |
17-4PH BLOCK | 17-4 PH Steel Block 110mm(3.937") x 18mm(7.09") x 15mm(.591") Block. Material: 17-4PH Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
181 | BOEING REFERENCE STANDARD 707 PART 6 55-10-07 PAGE 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
185 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 & 777-200/300 51-00-04 PROCEDURE 1 PAGE 8. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
186A | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.1875. Includes Test Report and Certificate of Conformance. | . | . | |||
186ABCDEF | BOEING CUSTOM COMBINATION REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.1875", .2500", .3125", .3750", .4375", .500. Each hole size marked with the corresponding Boeing Part number 186A-186F Includes Test Report and Certific... | . | . | . | . | |
186B | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.2500. Includes Test Report and Certificate of Conformance. | . | . | |||
186C | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.3125. Includes Test Report and Certificate of Conformance. | . | . | |||
186D | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.3750. Includes Test Report and Certificate of Conformance. | . | . | |||
186E | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.4375. Includes Test Report and Certificate of Conformance. | . | . | |||
186F | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.5000. Includes Test Report and Certificate of Conformance. | . | . | |||
188A | BOEING REFERENCE STANDARD PT 651-00-00-1 FIG 6. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
189 | BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4 PG.13 & 737 PT 6 51-00-00 PROCEDURE 23 PG.11 FIG.7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
192 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
194 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 FIGURE 1., BOEING 757 PART 6 53-30-02 PAGE 5 FIGURE 2 | . | . | . | . | |
194A | BOEING REFERENCE STANDARD 767 PT 6 53-30-02 FIG 3 PAGE 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
1TD1133D07001-2001 | Seyer Industries reference standard. Material: 2024-T351 Aluminum...Chamfer EDM Notch Size: .030" x .030" x .005" +/- .002"...Bore EDM Notch Size: .030" x .030" x .005" +/- .002". Includes Test Report and Certificate of Conformance. Part Serial Number:... | . | . | . | . | |
204-94034-1 | Boeing Reference Standard- Lower Lug APE-1 Primary , D204-12769-6 ASIP Inspection Program. Material: 4340 Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
208 FRONT SPAR | CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 FRONT SPAR LOWER CAP. Drawing NO. 2683201 | . | . | . | . | |
208 REAR SPAR | CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 REAR SPAR LOWER CAP. Drawing NO. 2683202 | . | . | . | . | |
212-A1325-01 | AIRBUS MILITARY REFERENCE STANDARD COM 212-266 PG 13 | . | . | . | . | |
2-164-501 | AIRBUS EDDY CURRENT CALIBRATION BLOCK 4340 STEEL, 51-10-00-250-801 and 51-63-991-001 PAGE 601 FIGURE 601. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-164-551 | AIRBUS CALIBRATION STANDARD, A350-A-51-90-01-01001-040A-A-NDT & 51-63-01-991-001-A PT 6 FIG 601, 2024-T351 ALUMINUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
23-55 | Olympus NDT Standard: Multi-hole 2024-T3 Aluminum | . | . | . | . | |
23-55T | Olympus NDT 8 step wedge 2024-T3 Aluminum | . | . | . | . | |
2506F | S/B 57-200 Douglas DC-9 Reference Standard 7075-T6 Aluminum. Figure 5, 6,7 | . | . | . | . | |
262 | BOEING REFERENCE STANDARD 727 PT 6 53-10-27 | . | . | . | . | |
262A | BOEING REFERENCE STANDARD 727 PT 6 53-10-27 | . | . | . | . | |
263 | BOEING REFERENCE STANDARD 727 PT 6 53-10-27 PAGE 4 FIG 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2683301-1 | Cessna reference standard 55-10-02-0 (Rev 1).Model 208 Inspection of Horizontal Stabilizer Spars. Fasteners: MS20470AD5-3 and CM3827AD5-3 | . | . | . | . | |
27-1-6033 | Fokker 50/60 calibration standard Part 6 53-40-05 pages 7&8 figure 4&5. Material 2024-T3 Aluminum. Fasteners: MS20426AD4 and MS20426AD5. | . | . | . | . | |
272 | BOEING REFERENCE STANDARD 727, PT 6 55-10-27 FIG. 2 | . | . | . | . | |
27-95031-001 | Fairchild METRO 23, Model SA227-CC, METRO 23, Model SA227-DC,Reference standard for inspection of the MLG and NLG Yoke Assembly. Material: 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
28-0-6049 | Fokker 70/100 Calibration Standard, Part 6 53-10-18 Page 12 Figure 8. Material: 2024-T351 Aluminum, Rivet = MS20426AD5. Paint with Primer. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-835-01-9301 | AIRBUS CALIBRATION BLOCK, STAINLESS STEEL, 0.2mm, 0.5mm, 1mm EDM SLOTS. PART 6: 51-63-01 page 601 figure 601 | . | . | . | . | |
2-835-01-9330 | AIRBUS CALIBRATION BLOCK, 6AL-4v TITANIUM, 0.2mm, 0.5mm, 1mm EDM SLOTS. PART 6: 51-63-01 page 601 figure 601 | . | . | . | . | |
2-887-01-9313S | SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T351 ALUMINUM TYPE SCCS3-7, A318 51-63-07. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-887-01-9314S | SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T251 ALUMINUM ..TYPE SCCS7-14, A318 51-63-07. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-887-01-9315S | SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T351 ALUMINUM ..TYPE SCCS14-21 , A318 51-63-06-PB1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-887-01-9316S | SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T351 ALUMINUM ..TYPE SCCS21-28, A318 51-63-07. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-887-01-9321S | SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-887-01-9323S | SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
2-887-01-9325S | SPLITTED CONICAL CALIBRATION STANDARD IN 6AL-4V Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
296 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
29A028 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601. MATERIAL: 4340 STEEL. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance..... | 31A008 | . | . | . | |
29A029 | AIRBUS CALIBRATION STANDARD, A350-A-51-90-01-01001-040A-A-NDT & 51-63-01-991-001-A PT 6 FIG 601, 2024-T351 ALUMINUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | 640-050-002 | . | . | . | |
29A029YS | AIRBUS CALIBRATION STANDARD, A318/A319/A320/A321 51-63-01-991-001-A PB 1 FIG 60 & A350-A-51-90-01-01001-040A-A-NDT 1, 2024-T351 ALUMINUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x 0.13mm(.0051") WIDE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
29A032 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, MATERIAL: 6AL-4V TITANIUM, 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
29A047 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, Aluminum(7075-T7)(39.5% IACS) 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | 2-410-1000-3 | . | . | . | |
29A049 | AIRBUS CALIBRATION STANDARD, A350-A-51-90-01-01001-040A-A-NDT & 51-63-01-991-001-A PT 6 FIG 601, 304 stainless steel.. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
29A120 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, MAGNESIUM. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
301 GUIDE | BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION | . | . | . | . | |
301SS | BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-70-001. ALSO IN 53-10-01 PART 6 PAGE 5 FIGURE 1. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL: 301 STAINLESS . SIZE: 1.5"W x 3.75"L x .25" | SS TYPE 301 | . | . | . | |
302 GUIDE | BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION | . | . | . | . | |
305 | BOEING REFERENCE STANDARD 737 PART 6 57-10-18 FIGURE 2 PAGE 6. | . | . | . | . | |
312 | BOEING REFERENCE STANDARD 737 PART 6 53-10-17 PAGE 6 FIGURE 2. 2024-T3 ALUMINUM | . | . | . | . | |
3-1251 | NOSE WHEEL BEAD SEAT WHEELL PROBE FOR BOEING 707 | . | . | . | . | |
313A/313B | BOEING REFERENCE STANDARD 737 PART 6 53-10-17 PAGE 7 FIGURE 3. 2024-T3 ALUMINUM | . | . | . | . | |
315 | BOEING REFERENCE STANDARD 737 PART 4 55-30-01 FIGURE 1 PAGE 4. | . | . | . | . | |
316 | BOEING REFERENCE STANDARD 737 PART 4 55-30-01 FIGURE 2 PAGE 5. | . | . | . | . | |
31A008 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601. MATERIAL: 4340 STEEL. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance... | 29A028 | . | . | . | |
320 | BOEING REFERENCE STANDARD 737 PART 6 55-10-19 FIGURE 2 PAGE 5. | . | . | . | . | |
321 | BOEING REFERENCE STANDARD 737 PART 6 53-10-19 FIGURE 3 PAGE 6. | . | . | . | . | |
323A | BOEING REFERENCE STANDARD 737 PART 4 55-50-01 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
323B | BOEING REFERENCE STANDARD 737 PART 4 53-10-38 FIGURE 2 PAGE 6. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
326 | BOEING REFERENCE STANDARD 737 PART 6 53-10-28 FIGURE 1 PAGE 4. | . | . | . | . | |
328A/328B | BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 2 PAGE 7. | . | . | . | . | |
328C/328D | BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 3 PAGE 8. | . | . | . | . | |
335 | BOEING REFERENCE STANDARD 737 PT 6 53-10-31. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
336A | BOEING REFERENCE STANDARD 737 PART 6 57-30-02 FIGURE 2 PAGE 5. | . | . | . | . | |
336B | BOEING REFERENCE STANDARD 737 PART 6 57-30-02 FIGURE 2 PAGE 5. | . | . | . | . | |
338A | BOEING REFERENCE STANDARD 737 PART 6 53-10-35 FIGURE 1 PAGE 6. MATERIAL: 2024-T3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
338B | BOEING REFERENCE STANDARD 737 PART 6 53-10-35 FIGURE 1 PAGE 6. MATERIAL: 301 1/2 HARD. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
341 | BOEING REFERENCE STANDARD 737 PART 4 53-10-40 FIGURE 1 PAGE 4. | . | . | . | . | |
345 | BOEING REFERENCE STANDARD 737 PART 6 57-40-01 FIGURE 2 PAGE 5. | . | . | . | . | |
349 | BOEING REFERENCE STANDARD 737 PART 4 32-10-01 FIGURE 2 PAGE 5. | . | . | . | . | |
350 | BOEING REFERENCE STANDARD 737 PT 4 32-20-01 | . | . | . | . | |
350P | BOEING POISTIONING FIXTURE 737 PT 4 32-20-01 | . | . | . | . | |
351A | BOEING REFERENCE STANDARD 737 PT 6 53-10-01 | . | . | . | . | |
351B | BOEING REFERENCE STANDARD 737 PT 6 53-10-01 | . | . | . | . | |
353ABC | BOEING REFERENCE STANDARD 737 PT6 53-10-12 | . | . | . | . | |
353D | BOEING REFERENCE STANDARD 737 PT 6 53-10-12 | . | . | . | . | |
354A | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | . | . | . | . | |
354B | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | . | . | . | . | |
354C | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | . | . | . | . | |
355A | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | . | . | . | . | |
355B | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | . | . | . | . | |
355C | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | . | . | . | . | |
356 | BOEING REFERENCE STANDARD 737 53-30-04 PART 6 PAGE 4 FIGURE 1. Includes test report and Certificate of Conformance. | . | . | . | . | |
363 | BOEING REFERENCE STANDARD PART 6 53-30-03 FIGURE 1 PAGE 6. Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
365 | BOEING REFERENCE STANDARD 737 PART 4 71-20-01 PG.4 FIGURE 1 DETAIL I. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
367 | BOEING REFERENCE STANDARD 737 PT 6 71-20-01 Figure 4, PG. 10-12 (Sheets 1-3) | . | . | . | . | |
369 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 & 737 Part 6 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
370 | BOEING REFERENCE STANDARD 737 PT 6 53-30-02 | . | . | . | . | |
375 | BOEING REFERENCE STANDARD 737 PT 4 55-10-02. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
378 | BOEING REFERENCE STANDARD 737 PT 6 53-10-44 PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
382-57-74 82-688 | HERCULES CALIBRATION BLOCK 382-57-74 82-688 | . | . | . | . | |
383 | BOEING REFERENCE STANDARD 737 PART 6 53-30-07 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
4004 | BOEING REFERENCE STANDARD 747 PART 4 53-40-01 PAGE 10 FIGURE 6. Includes Test Report and Certificate of Confromance. | . | . | . | . | |
402 | BOEING REFERENCE STANDARD 747 PT 4 57-10-04 Page 5 Figure 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
4028 | BOEING REFERENCE STANDARD 747 PART 4 57-40-03 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
4036 | BOEING REFERENCE STANDARD 747 PART 4 57-40-05 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
4057 | BOEING REFERENCE STANDARD 747 PT 6 53-30-03 | . | . | . | . | |
410 | BOEING REFERENCE STANDARD 747 PT 4 57-10-05 Page 6 Figure 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
432 | BOEING REFERENCE STANDARD 747 PT 6 57-30-02 Page 4 Figure 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
4340-3-0050 | DC9 REFERENCE STANDARD S/B 57-118 SERVICE SKETCH 2671 SHEET 4 OF 7. MATERIAL: 4340 STEEL. | . | . | . | . | |
437 | BOEING REFERENCE STANDARD 747 53-10-01 PART 4 PAGE 11 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | .. | |
438 | BOEING REFERENCE STANDARD 747 53-10-01 PART 4 PAGE 11 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
441 | BOEING REFERENCE STANDARD 747 PT 4 57-10-10 Page 9 Figure 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
45-127-1 | Custom Probe Locating Bushing Tool Figure 1 Page 6 Item #1. Material 2024-T3 Aluminum. | . | . | . | . | |
45-127-2 | Custom Probe Locating Bushing Tool Figure 1 Page 6 Item #2. Material 2024-T3 Aluminum. | . | . | . | . | |
45-128 | Custom 8 Hole Calibration Standard Test Coupon Assembly Figure 5 Page 10 to include the following Pieces. Figure 2 Page 7. Material .071" 2024-T3 Clad Aluminum, 7 EDM Flaws total. Figure 3 Page 8 .250" 4130or4340 Steel 0 EDM Flaws total and Figure 4... | . | . | . | . | |
45-128-1 | Custom 8 Hole Calibration Standard Test Coupon. Figure 1 Page 7. Material .071" 2024-T3 Clad Aluminum. 7 EDM Flaws total. | . | . | . | . | |
45-128-2 | Custom 8 Hole Calibration Standard Test Coupon. Figure 3 Page 8. Material .250" 4130/4340 Steel. 0 EDM Flaws total. | . | . | . | . | |
45-128-3 | Custom 8 Hole Calibration Standard Test Coupon. Figure 4 Page 9. Material .125" 2024-T3 Clad Aluminum. 0 EDM Flaws total. | . | . | . | . | |
460 | BOEING REFERENCE STANDARD 747 PART 6 57-10-28, PAGE 3 FIGURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
460 | BOEING REFERENCE STANDARD 747 PART 6 57-10-28, PAGE 3 FIGURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
475 | BOEING 747 REFERENCE STANDARD PART 6 57-10-27 FIGURE 1 PAGE 4. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
482 | BOEING 747 REFERENCE STANDARD PART 6 55-10-08 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
483 | BOEING 747 REFERENCE STANDARD PART 6 55-10-08 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
497 | BOEING REFERENCE STANDARD 767 PT 6 53-00-05 | . | . | . | . | |
506 | BOEING REFERENCE STANDARD 757 PT 4 57-40-01 FIG 3 | . | . | . | . | |
506 | NO BID - BOEING REFERENCE STANDARD 757 PT 4 57-40-01 FIG 3 | . | . | . | . | |
5290020-4 | Cessna Model 401/402 Calibration Standard Figure 4 part 2 & 3 Inspection. Plate A - 7075-T6 Aluminum and Plate B - 2024-T3 Aluminum. | . | . | . | . | |
53-10-110A | Raytheon 125 Series Calibration Standard. Material: 4340 Cres Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-126/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-0126/1 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-130/158/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-01 PT 6 FIGURES 5&6 PAGES 10&11. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-137 | BAE 146-RJ SERIES REFERENCE STANDARD SET OF 8 UNITS, 53-10-12 PT 6 FIGURE 7 PAGES 907-910. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-153/155/175/193/194/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-08 PT 6 FIGURES 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-153/155/175/194/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-06 PT 6 FIGURES 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-189/1 | BAE 146-RJ SERIES PROBE GUIDE 53-10-15 PT 6 PAGES 1&2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-10-192/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-25 PT 6 FIGURES 6&7 PAGES 10&11. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-104/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-00-86 PT 6 FIGURES 7&8 PAGES 14&15. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-140A/1 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-26 PG 10 FIG 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-140A/2 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-26 PG 10 FIG 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-145/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-03 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | SPO-310 | . | . | . | |
53-20-148/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-01 PT 6 FIGURES 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-149/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-65 PT 6 FIGURE 11&12 PAGES 16&17. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-155/1/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 7&8 PAGES 13&14. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-155/1/2 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 9&10 PAGES 15&16. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-155/1/3 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 11&12 PAGES 17&18. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-155/1/4 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-36 PT 6 FIGURES 13&14 PAGES 19&20. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-157/2 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-84 PT 6 FIGURE 8 PAGE 12. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-165 | BAE 146 BRITISH AIRCRAFT PT 4 53-20-14, 2024-T6 | . | . | . | . | |
53-20-167/1 | BAE REFERENCE STANDARD 146-RJ 53-238 53-20-21 PT 4 FIGURE 4 PAGE 519. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-169/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-21 PT 4 FIGURE 3 PAGES 505. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-171/1 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-21 PG 512 FIG 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-179/2 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-14 PT 6 FIGURE 5&6 PAGES 10&11. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-20-180/3 | BAE REFERENCE STANDARD 146-RJ 53-20-88 FIG 4&5, PAGES 8&9. Includes Test Report and Certificate of Conformance. | SP80-306 | . | . | . | |
53-30-126/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-02 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-30-131/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-01 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-30-131/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-01 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-30-174/177/179/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-03 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-30-174/177/179/2 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-04 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-40-125/1 | BAE REFERENCE STANDARD 146-RJ 53-238 53-40-06 PT 6 FIGURE 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
53-41-04-991-002-A | Airbus Reference standard 53-41-04-991-002-A Sheet 01 part 6 page 11. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
55-31-105/1 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-31-42 PG 7 FIG 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
55-31-109/2 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-31-43 PG 8 FIG 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
55-31-NDT 1 | BAE REFERENCE STANDARD 146-RJ 53-238 55-20-11 PT 6 FIGURE 5 PAGE 9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
55-33-101/1 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-33-10 PG 7/8 FIG 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
55-33-101/2 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-33-10 PG 7/8 FIG 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
55-33-101/3 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-33-10 PG 7/8 FIG 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-035/044/1 | BAE JETSTREAM SERIES 4100 57-10-36 PT 6 | . | . | . | . | |
57-10-102/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-12 PT 4 FIGURE 6&7 PAGES 11&12. Includes Test Report and Certificate of Conformance. | H51128-6-K7 | . | . | . | |
57-10-102/2 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-12 PT 4 FIGURE 6&7 PAGES 11&12. Includes Test Report and Certificate of Conformance. | H51128-6-K7 | . | . | . | |
57-10-107/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-52 PT 6 FIGURE 5&6 PAGES 11&12. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-107/2 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-52 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-111/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-55 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-111/2 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-55 PT 4 FIGURE 5&6 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-117/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-50 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-117/2 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-48 PT 6 FIGURE 3&4 PAGES 7&8. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-41/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-41 PT 4 FIGURE 2 PAGE 506. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-10-41/2 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-41 PT 4 FIGURE 3 PAGES 507. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-14222-1WR | Custom Isotec wing repair reference standard. Material: 7075-T6 Aluminum | . | . | . | . | |
57-20-179/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-20-10 PT 4 FIGURES 4 PAGE 8. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
57-54-103C | CUSTOM BOEING REFERENCE STANDARD 7075-T6 ALUMINUM | . | . | . | . | |
601PA | POISTIONER | . | . | . | . | |
601PF | POSTIONER FIXTURE | . | . | . | . | |
602 | BOEING REFERENCE STANDARD 767 PT 4 32-10-01 FIG 2 | . | . | . | . | |
603 | BOEING REFERENCE STANDARD 767 PT 4 55-10-01 | . | . | . | . | |
603P | TRANSDUCER POSITIONER | . | . | . | . | |
604A | BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1 | . | . | . | . | |
604B | BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1 | . | . | . | . | |
605 | BOEING REFERENCE STANDARD 767 PT 6 22-10-01 | . | . | . | . | |
605A | BOEING REFERENCE STANDARD 767 PT 6 22-10-01 | . | . | . | . | |
6061 AL BLOCK | Aluminum Block 110mm(3.937") x 18mm(7.09") x 15mm(.591") Block. Material: 6061-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
608 | BOEING REFERENCE STANDARD 767 PT 4 27-80-01 FIG 4 | . | . | . | . | |
608P1 | TRANSDUCER WEDGE | . | . | . | . | |
608P2 | TRANSDUCER WEDGE | . | . | . | . | |
610 | BOEING REFERENCE STANDARD 767 PT 4 32-20-01 | . | . | . | . | |
672-VEESCAN/6061-T6 | CUSTOM EDDY CURRENT REFERENCE BLOCK MADE OF 6061-T6 ALUMINUM with a 1.52mmL X 0.1mmW X 0.76mmD EDM FLAW. | . | . | . | . | |
672-VEESCAN/7075-T6 | CUSTOM EDDY CURRENT REFERENCE BLOCK MADE OF 7075-T6 ALUMINUM with a 1.52mmL X 0.1mmW X 0.76mmD EDM FLAW. | . | . | . | . | |
6AL-6V-2SN-Ti | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" +/-.001 DEEP, (MAX WIDTH .005"), 6AL-6V-2SNTi | . | . | . | . | |
71658-10-42 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-10-42 (5/8" X 4.1") | . | . | . | . | |
71658-10-46 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-10-46 (5/8" X 4.4") | . | . | . | . | |
71658-14-45 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-14-45 (7/8" X 4.8") | . | . | . | . | |
71658-14-50 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-14-50 (7/8" X 5.1") | . | . | . | . | |
71658-16-55 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-16-55 (1.0" X 6.0") | . | . | . | . | |
71658-18-53/2&3 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39 | . | . | . | . | |
71658-18-59 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-8-59 (1 1/8" X 6.25") | . | . | . | . | |
71658-18-64 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-18-64 (1 1/8" X 6.5") | . | . | . | . | |
71658-20-68 | DOUGLAS DC-10 HORIZONTAL STABILIZER REFERENCE STANDARD 4130 or 4340 STEEL, SB A55-17 PAGE 21 FIG.1(SHEET 3) BOLT IDENTIFICATION 71658-20-68 (1 1/4" X 7.0") | . | . | . | . | |
71658-7-35/1&4 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39 | . | . | . | . | |
717RS1 | 717-200 REFERENCE STANDARD ISOLATOR LUG. FIG. 1.1 SHEET 1, PAGE 1. MATERIAL: 4340 NORMALIZED STEEL PER MIL-S-5000. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RS12 | 717-200 REFERENCE STANDARD...FIG. 1.16 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | S4932867-6/NAS1080-6 | . | . | . | |
717RS15 | 717-200 REFERENCE STANDARD...FIG. 1.4 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RS20 | 717-200 REFERENCE STANDARD...FIG. 1.21 SHEET 1-3, PAGES 1-3. MATERIAL: 2014-T6 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RS23 | 717-200 REFERENCE STANDARD...FIG. 1.8 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RS2A | 717-200 REFERENCE STANDARD...FIG. 1.12 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | MS21042L-4 | . | . | . | |
717RS2B | 717-200 REFERENCE STANDARD...FIG. 1.13 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | MS21042L-4 | . | . | . | |
717RS2C | 717-200 REFERENCE STANDARD...FIG. 1.14 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | MS21042L-4 | . | . | . | |
717RS2D | 717-200 REFERENCE STANDARD...FIG. 1.15 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | MS21042L-4 | . | . | . | |
717RS4 | 717-200 REFERENCE STANDARD FIGURE 1.17 SHEETS (1-4 ), PAGES 1-4. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RS7 | 717-200 REFERENCE STANDARD...FIG. 1.22 SHEET 1-7, PAGES 1-7. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RS8 | 717-200 REFERENCE STANDARD...FIG. 1.23 SHEET 1-6, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | NAS1252-416H | . | . | . | |
717RS9 | BOEING 717-200 REFERENCE STANDARD FIGURE 1.24. MATERIAL: 6AL-4V. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
717RST5 | 717-200 REFERENCE STANDARD...FIG. 1.18 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | NAS1080-6 | . | . | . | |
717RST6 | 717-200 REFERENCE STANDARD...FIG. 1.19 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | NAS1080-6 | . | . | . | |
7637987-9 | A53-142 Douglas DC-9 7637987-9 Reference Standard Assembly 2024-T3 Clad Aluminum. Figure 1, Sheets 2&3 | . | . | . | . | |
7947479-10 | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | NSN 6635-01-092-5129 | AFK-A | . | . | |
7947479-10 Ti | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | NSN 6635-01-390-1768 | . | . | . | |
7947479-10/17-4PH | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | 6635-01-092-5129 | . | . | . | |
7947479-10/4340 | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | NSN 6635-01-512-4952 | . | . | . | |
7947479-10/MAG | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | 7947479-10 | . | . | . | |
7947479-10-T | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | NSN 6635-01-092-5129 | 6635-01-092-5129 | 6635-01-390-1768 VM Products | . | |
80RS10 | MD-80 REFERENCE STANDARD SECTION 2-1 FIGURE13 FASTENER (NSA1097AD6) | . | . | |||
80RS11 | MD-80 REFERENCE STANDARD 57.80.007 FASTENER (S4931918-6 + S4933653-3, S4932868-08 + NAS1080-08) | . | . | . | . | |
80RS12 | MD-80 REFERENCE STANDARD FASTENER (HLT335-6-7 + NAS1252-10L + MS21042L3, MS20426AD5-8, S4932867-08-8 + NAS1080-08) | HLT335-6 | MS20426AD5-8 | . | . | |
80RS13 | MD-80 REFERENCE STANDARD 57.80.012 FASTENER (HLT335-6-7 + NAS1252-10L + MS21042L3, MS20426AD5, NAS1478 + NAS1080-08) | . | . | . | . | |
80RS14 | 717-200 REFERENCE STANDARD...FIG. 1.6 SHEET 1-4, PAGES 1-4. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
80RS16 | MD-80 REFERENCE STANDARD FASTENER (MS20470-AD5, NAS1097-AD6, NAS1097-AD5) | NAS1097-AD6 | NAS1097-AD5 | . | . | |
80RS18 | 717-200 REFERENCE STANDARD...FIG. 1.5 SHEET 1-5, PAGES 1-5. MATERIAL: 7075-T6 CLAD ALUMINUM, 2014-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.53.80.003 FASTENER (S4932868-06 + NAS1080-6, 3D0009-6 + 3D0007-3, NAS1097-AD6) | . | . | . | . | |
80RS19 | 717-200 REFERENCE STANDARD...FIG. 1.2 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 or 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. FASTENER (NAS1097-AD6) | . | . | |||
80RS21 | MD-80 REFERENCE STANDARD 54.80.002 | . | . | . | . | |
80RS24 | BOEING REFERENCE STANDARD. MATERIALS: -3 DETAIL ALUMINUM SKIN 2024-T351, -5 DETAIL ALUMINUM STRINGER 2024-t351, -7 DETAIL ALUMINUM 7075-T6511, -9 DETAIL ALUMINUM 7075-T73 and -11 DETAIL ALUMINUM 7075-T73. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
80RS25 | BOEING REFERENCE STANDARD. MATERIALS: -3 DETAIL ALUMINUM SKIN 2024-T351, -5 DETAIL ALUMINUM STRINGER 7075-T6511, -7 DETAIL ALUMINUM 7075-T73. FASTENERS: S4932869-6-6 (8 EA. ), S4932869-8-6 (12 EA. ), S4932869-8-7 (16 EA. ). COLLARS: NAS 1080-06 (8 EA... | . | . | . | . | |
80RS3 | MD-80 REFERENCE STANDARD FASTENER (S4932867-08 + NAS1080-08) | . | . | . | . | |
80RS4 | MD-80 REFERENCE STANDARD FASTENER (S4932867-06 + NAS1080-06, MS20426AD8) | . | . | . | . | |
80RS5 | MD-80 REFERENCE STANDARD FASTENER (S4932867-06 + NAS1080-06, MS20426AD8) | . | . | . | . | |
80RS6 | MD-80 REFERENCE STANDARD FASTENER (S4932867-06 + NAS1080-06, MS20426AD8) | NAS1080-08 | . | . | . | |
80RS7 | MD-80 REFERENCE STANDARD FASTENER (S4932867-08-7 + NAS1080-08) | NAS1080-08 | . | . | . | |
80RS8 | MD-80 REFERENCE STANDARD FASTENER (S4932868-08 + NAS1080-08) | S4932868-08-7 | NAS1080-08 | . | . | |
80RS9 | MD-80 REFERENCE STANDARD FASTENER (S4932867-06-5 + NAS1080-06) | NAS1080-6 | . | . | . | |
95605718 | MAIN WHEEL BEAD SEAT WHEELL PROBE FOR BOEING 707 | . | . | . | . | |
98A53803014001 | AIRBUS REFERENCE STANDARD, 53-16-02 Part 6 FIGURE 603 PG. 605-606 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A53803018000 | AIRBUS REFERENCE STANDARD PT 6 57-10-33 PAGE 404 FIGURE 404. . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A5380301900 | AIRBUS REFERENCE STANDARD A300-600 57-10-46 PT 4 FIG 404 | . | . | . | . | |
98A5380302000 | AIRBUS REFERENCE STANDARD A300-600 57-10-46 PT 4 FIG 404 | . | . | . | . | |
98A54003019 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 13 FIGURE 8, SSI NO. 54-10-07. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003069 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.41 FIGURE 29, SSI NO. 54-10-08. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003072 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.25 FIGURE 16, SSI NO. 54-40-09. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003072000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 FIG 403 | . | . | . | . | |
98A54003073 | IRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.28 FIGURE 21, SSI NO. 54-40-09. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003073000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 FIG 404 | . | . | . | . | |
98A54003074 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.19 FIGURE 12, SSI NO. 54-40-07. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003074000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 54-50-15 PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003075 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 5 FIGURE 3, SSI NO. 54-10-03 Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003077 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 5 FIGURE 3, SSI NO. 54-10-03. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98A54003096 | AIRBUS A310 REFERENCE STANDARD PART4 54-50-20 PAGE 402 FIGURE 401. Includes Test Report and certificate of Conformance. | . | . | . | . | |
98A54403026000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 | . | . | . | . | |
98A57103016001 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-04 PAGE 404 FIGURE 403. Includes Test Report and Cerificate of Conformance. | . | . | . | . | |
98L57103002000 | AIRBUS A380-800 FIGURE 57-11-03-991-008-A PAGE 39. MATERIAL: 2024 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S51605001-200 | ATR REFERENCE STANDARD PT 6 51-60-00 PAGE 628 FIGURE 615 | . | . | . | . | |
98S51605001-202 | ATR72 CALIBRATION STANDARD PART 4 57-14-03 PAGE 403 FIGURE 401. MATERIAL: 15-5PH Steel | . | . | . | . | |
98S51605001-204 | ATR REFERENCE STANDARD PT 6 51-60-00. MATERIAL: TITANIUM TA6V(6AL-4V). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S51605001-206 | MINI ANGLE BEAM ALUM V2 BLOCK ½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version). Aluminum 7075-T6. Includes form fitted case. | V2-AL | . | . | . | |
98S51605001-208 | MINI ANGLE BEAM BLOCK CS V2 BLOCK..½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version).1018 Carbon Steel with form fitted case | V2-CS | . | . | . | |
98S51605001-212 | ATR REFERENCE STANDARD 2024-T3 Aluminum PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes: ( 9.5mm, 9.9mm, 10.3mm, 11.1mm, 11.5mm, 11.9mm, 12.7mm, 13.5mm, 14mm ). Includes Test Report and Certificate of C... | . | . | . | . | |
98S51605001-214 | ATR REFERENCE STANDARD 15-5PH Steel PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes: ( 9.5mm, 9.9mm, 10.3mm, 11.1mm, 11.5mm, 11.9mm, 12.7mm, 13.5mm, 14mm ). Includes Test Report and Certificate of Confo... | . | . | . | . | |
98S51605001-216 | ATR REFERENCE STANDARD ..TA6V(6AL-4V) Titanium PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes: ( 9.5mm, 9.9mm, 10.3mm, 11.1mm, 11.5mm, 11.9mm, 12.7mm, 13.5mm, 14mm ). Includes Test Report and Certifica... | . | . | . | . | |
98S51605001-218 | ATR REFERENCE STANDARD 2024-T3 Aluminum PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes:( 3.6mm, 4mm, 4.8mm, 5.2mm, 5.7mm, 6.4mm, 6.7mm, 7.1mm, 7.9mm, 8.3mm, 8.7mm ). Includes Test Report and Certificat... | . | . | . | . | |
98S51605001-220 | ATR REFERENCE STANDARD PT 6 51-60-00 15-5PH stainless steel Calibration Standard for Rotary Probes Figure 616 (Sheet 1) Page 629, Hole Sizes:( 3.6mm, 4mm, 4.8mm, 5.2mm, 5.7mm, 6.4mm, 6.7mm, 7.1mm, 7.9mm, 8.3mm, 8.7mm ). Includes Test Report and Certifi... | . | . | . | . | |
98S51605001-222 | ATR REFERENCE STANDARD TA6V(6AL-4V) Titanium PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes:( 3.6mm, 4mm, 4.8mm, 5.2mm, 5.7mm, 6.4mm, 6.7mm, 7.1mm, 7.9mm, 8.3mm, 8.7mm ). Includes Test Report and Cert... | . | . | . | . | |
98S51605001-224 | ATR REFERENCE STANDARD 2024-T3 Aluminum PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes:( 14.3mm, 14.6mm, 15.1mm, 15.9mm, 16.3mm, 16.7mm, 28.9mm, 19.8mm, 22.2mm, 22.6mm, 23mm ). Includes Test Report and... | . | . | . | . | |
98S51605001-226 | ATR REFERENCE STANDARD 15-5PH Steel PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes:( 14.3mm, 14.6mm, 15.1mm, 15.9mm, 16.3mm, 19.0mm, 19.4mm, 19.8mm, 22.2mm, 22.6mm, 23mm ). Includes Test Report and Cer... | . | . | . | . | |
98S51605001-228 | ATR REFERENCE STANDARD TA6V(6AL-4V) Titanium PT 6 51-60-00. Calibration Standard for Rotary Probes..Figure 616 (Sheet 1) Page 629, Hole Sizes:( 14.3mm, 14.6mm, 15.1mm, 15.9mm, 16.3mm, 19.0mm, 19.4mm, 19.8mm, 22.2mm, 22.6mm, 23mm ). Includes Test Repor... | . | . | . | . | |
98S51605001-230 | ATR REFERRENCE STANDARD PT 6 51-60-00 | . | . | . | . | |
98S51605001-232 | ATR REFERRENCE STANDARD PT 6 51-60-00 | . | . | . | . | |
98S51605001-234 | ATR REFERRENCE STANDARD PT 6 51-60-00 | . | . | . | . | |
98S52305005-000 | ATR CALIBRATION STANDARD PT 4 53-31-04 PAGE 404 FIGURE 401. MATERIAL: 2024-T3, 15-5 CRES. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S52305008-200 | ATR72 REFERENCE STANDARD 52-31-04 PT 4 | . | . | . | . | |
98S53005005-000 | ATR CALIBRATION STANDARD 53-31-01 PART 6 PAGE 607 FIGURE 601 SHEET 2. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005006-000 | ATR CALIBRATION STANDARD 53-31-01 PART 6 PAGE 606 FIGURE 601 SHEET 2. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005008-000 | ATR CALIBRATION STANDARD 53-31-21 PART 6 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005009-000 | ATR CALIBRATION STANDARD 53-51-02 PART 6 PAGE 606 FIGURE 601. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005010-000 | ATR CALIBRATION STANDARD 53-51-03 PART 6 PAGE 606 FIGURE 601 SHEET 2. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005011-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-31-21 FIGURE 601 SHEETS 1&2 PAGE 608 & 609. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005012-000 | ATR CALIBRATION STANDARD 53-81-14 PART 6 PAGE 606 FIGURE 601 SHEET 1. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005013-000 | ATR CALIBRATION STANDARD 53-81-14 PART 6 PAGE 607 FIGURE 601 SHEET 2. MATERIAL: 2024-T3. | . | . | . | . | |
98S53005015-000 | ATR CALIBRATION STANDARD 53-51-01 PART 6 PAGE 608 FIGURE 601. MATERIAL: 2024-T3, 7075-T6 | . | . | . | . | |
98S53005016-000 | ATR42-400/500 SERIES REFERENCE STANDARD 53-51-20 PART 4, 2024-TT3 Aluminum | . | . | . | . | |
98S53005017-000 | ATR CALIBRATION STANDARD 53-81-16 PART 6 PAGE 606 FIGURE 601 SHEET 1. MATERIAL: 2024-T3, 7075-T6 | . | . | . | . | |
98S53005018-000 | ATR CALIBRATION STANDARD 53-51-01 PART 6 PAGE 607 FIGURE 601 SHEET 2. MATERIAL: 2024-T3, 7075-T6 | . | . | . | . | |
98S53005020-000/1 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. | . | . | . | . | |
98S53005020-000/2 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 609 FIGURE 601 SHEET 2. MATERIAL: 2024-T3 Aluminum. | . | . | . | . | |
98S53005020-200 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-202 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-204 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-206 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-208 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-210 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-212 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-214 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005020-216 | ATR72 CALIBRATION STANDARD PART 6 53-00-01 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005021-000 | ATR72 CALIBRATION STANDARD 53-51-01 PART 6 PAGE 608 FIGURE 601 SHEET 1. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005024-000 | ATR REFERENCE STANDARD PT 6 53-61-03 | . | . | . | . | |
98S53005025-000 | ATR REFERENCE STANDARD PT 6 53-61-02 | . | . | . | . | |
98S53005026-000 | ATR REFERENCE STANDARD PT 6 53-61-01 | . | . | . | . | |
98S53005027-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-61-01 FIGURE 606 SHEET 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005028-000 | ATR REFERENCE STANDARD PT 6 53-31-04 | . | . | . | . | |
98S53005029-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-31-01 FIGURE 601 SHEET 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005030-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-31-21 FIGURE 601 SHEET 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005031-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-31-04 FIGURE 601 SHEET 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005032-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-61-01 FIGURE 601 SHEET 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53005033-000 | ATR42-400/500 CALIBRATION STANDARD PART 6 53-61-02 FIGURE 601 SHEET 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53105000-200 | ATR72 CALIBRATION STANDARD PART 6 53-11-23 PAGE 612 FIGURE 603. MATERIAL: 15-5PH Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53305006-000 | ATR42-400/500 NON-CONDUCTIVE PROBE GUIDE | . | . | . | . | |
98S53305006-001 | ATR42-400/500 NON-CONDUCTIVE PROBE GUIDE | . | . | . | . | |
98S53505003-200 | ATR72 CALIBRATION STANDARD PART 4 53-56-01 PAGE 405 FIGURE 402. MATERIAL: 2024-T3 Aluminum. | . | . | . | . | |
98S53505006-000 | ATR REFERENCE STANDARD PT 4 53-51-23 FIG 403. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S53805002-000 | ATR REFERENCE STANDARD 53-61-18 PT 6 FIGURE 603 PAGE 609. INSPECTION OF REAR PRESSURE BULKHEAD PERIPHERY OF DOME SKIN AND CONNECTION WITH VERTICAL FLANGE OF DOME VERTICLAL CHORD. Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
98S54305001-200 | ATR REFERENCE STANDARD 54-31-70 PT 4 FIG 401 | . | . | . | . | |
98S54305001-202 | ATR REFERENCE STANDARD 54-31-70 PT 4 FIG 401. Includes Test Report and Certificate of Conformance. | . | ||||
98S54305002-200 | ATR REFERENCE STANDARD ART72 PART 4 54-31-70 PAGE 403 FIGURE 401. MATERIAL: 6AL-4V Titanium. | . | . | . | . | |
98S57105003-200 | ATR REFERENCE STANDARD PT 4 57-15-21 | . | . | . | . | |
98S57105004-200 | ATR72 CALIBRATION STANDARD PART 4 57-15-21 PAGE 403 FIGURE 401. MATERIAL 4340 STEEL (35NCD16) | . | . | . | . | |
98S57105005-200 | AIRBUS REFERENCE STANDARD 57-12-11 PT 4 FIG 401 | . | . | . | . | |
98S57105006-200 | ATR72 CALIBRATION STANDARD PART 4 57-12-11 PAGE 404 FIGURE 401. MATERIAL: 2024-T3 Aluminum | . | . | . | . | |
98S57105007-200 | ATR72 CALIBRATION STANDARD PART 4 57-14-03 PAGE 403 FIGURE 401. MATERIAL: 2024-T3 Aluminum. | . | . | . | . | |
98S57105009-200 | ATR REFERENCE STANDARD PT 4 57-15-10 PAGE 403 FIGURE 401. 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S57105010-200 | ATR REFERENCE STANDARD PT 4 57-15-10 PAGE 403 FIGURE 401. TA6V TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S57105011-200 | ATR CALIBRATION STANDARD 57-15-11 PART 4 PAGE 403 FIGURE 401. MATERIAL: 6AL-4V TITANIUM | . | . | . | . | |
98S57105012-200 | ATR REFERENCE STANDARD PT 4 57-15-11 PAGE 403 FIGURE 401. 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S57105015-200 | ATR REFERENCE STANDARD PT 4 57-1403 FIG 401 | . | . | . | . | |
98S57105016-200 | ATR72 CALIBRATION STANDARD PART 6 57-14-04 PAGE 603 FIGURE 601. MATERIAL: PLEXIGLASS. | . | . | . | . | |
98S57105019-200 | ATR72 CALIBRATION STANDARD PART 6 57-14-01 PAGE 603 FIGURE 601. MATERIAL: 2024-T3 Aluminum. | . | . | . | . | |
98S57105030-200 | AIRBUS REFERENCE STANDARD 57-15-12 PT 4 FIG 401 | . | . | . | . | |
98S57105031-200 | ATR REFERENCE STANDARD PART 4 57-12-12 PAGE 404 FIGURE 401. 2024-T351 | . | . | . | . | |
98S57105032-200 | ATR72 REFERENCE STANDARD PART 4 57-12-12 PAGE 404 FIGURE 401. 2024-T351. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S57105032-202 | ATR72 REFERENCE STANDARD PART 4 57-12-12 PAGE 405 FIGURE 402. 2024-T351. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S57105033-200 | ATR REFERENCE STANDARD PART 4 57-12-11 PAGE 404 FIGURE 401. 2024-T351 | . | . | . | . | |
98S57105034-200 | ATR REFERENCE STANDARD PART 4 57-14-03 PAGE 403 FIGURE 401. 2024-T351 | . | . | . | . | |
98S57205024-200 | ATR REFERENCE STANDARD PT 4 57-24-09 PAGE 403 FIGURE 401. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
98S57205025-200 | ATR REFERENCE STANDARD PT 4 57-24-10 | . | . | . | . | |
98S57205026-200 | AIRBUS REFERENCE STANDARD 57-24-12 FIG 401 PT 4 | . | . | . | . | |
98S57205027-200 | ATR REFERENCE STANDARD PT 4 57-24-13 | . | . | . | . | |
98S57205027-202 | ATR REFERENCE STANDARD PT 4 57-24-13 | . | . | . | . | |
99A51003000000 | AIRBUS REFERENCE STANDARD 53-00-02 99A51003000000 FASTENER (NSA5050-3, EN6114-3-3, EN6114V-3-3) | EN6114-3-3 | E6114V3-3 | . | . | |
99A51107299001 | AIRBUS REFERENCE STANDARD A300-600 51-10-13 FIG 4 FASTENER (NAS5410-48). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A51107300000 | AIRBUS A330 REFERENCE STANDARD FOR SUBSURFACE CRACKS IN AL-ALLOY 51-10-16-991-011-A. PART 6, PAGE 615 FIGURE 610PROCEDURE B. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
99A53003001100 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 6AL-4V TITANIUM | . | . | . | . | |
99A53003001100 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 6AL-4V TITANIUM. Includes Test Report an Certificate of Conformance. | . | . | . | . | |
99A53003001101 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM.. | . | . | . | . | |
99A53003001101/A1 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. Note: Holes A1-A6 | . | . | . | . | |
99A53003001101/A13 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. Note: Holes A13-A18 | . | . | . | . | |
99A53003001101/A7 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. Note: Holes A7-A12 | . | . | . | . | |
99A53003001102 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: STEEL | . | . | . | . | |
99A53003001103 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A 2024-T3 ALUMINUM. Includes. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53003001104 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A. MATERIAL: 6AL-4V (AMS4911)TITANIUM. Includes Test Report anc Certificate of Conformance... | . | . | . | . | |
99A53003001105 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A MATERIAL: AISI4130 STEEL. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
99A53003001106 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A . MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53003001107 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A. MATERIAL: 6AL-4V(AMS4911) TITANIUM. Includes Test Report anc Certificate of Conformance. | . | . | . | . | |
99A53003001108 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A MATERIAL: AISI4130 STEEL. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
99A53003005001 | AIRBUS REFERENCE STANDARD A300-600/ A310 PT 4 53-12-52 PG.404 FIGURE 404. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53103002000 | AIRBUS REFERENCE STANDARD PT 4 53-12-50 | . | . | . | . | |
99A53103003000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 53-12-20 PAGE 407 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53107215000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 53-31-81 99A53107215000 FASTENER (HL11VF6-6, HL70-6). Includes Test Report and Certificate of Conformance. | HL70-6 | . | . | . | |
99A53107251000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 53-19-14 FIGURE 402, PG. 403 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53107265001 | AIRBUS REFERENCE STANDARD A300-600 PT 6 53-19-21 FASTENER (NAS1474A4, LN9198, LN9199) | LN9198 | LN6199 | . | . | |
99A53107282000 | AIRBUS REFERENCE STANDARD A300 PT 6 53-33-00 | . | . | |||
99A53107283000 | AIRBUS A330 REFERENCE STANDARD 7075-T7451 ALUMINUM. PART 4 53-40-18-270-801-A-01 - Bulk Cargo Compartment Door Cut-out Lateral Frame at Bulk Door-Fittings, FR67 at STGR37 and FR69 at STGR38, RH, FIGURE 53-40-18-991-015-A. Includes Test Report and Cer... | . | . | . | . | |
99A53107287000 | AIRBUS REFERENCE STANDARD A318-A321 52-31-16 FASTENER (DAN5-5-5, NAS5075-5). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53107290000 | AIRBUS REFERENCE STANDARD A300-600 PT6 53-19-24 FIGURE 604, PG. 604 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53203007000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 53-12-23 | . | . | . | . | |
99A53307203000 | AIRBUS A300 REFERENCE STANDARD PART 4 53-30-10; PG. 5, FIG. 2 ALSO USED FOR PART 6; 53-30-20 | . | . | . | . | |
99A53307225000 | AIRBUS A300 REFERENCE STANDARD PART 6; 53-30-20 | . | . | . | . | |
99A53307236000 | AIRBUS REFERENCE STANDARD A330 53-21-36 FIG 618. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53307244000 | AIRBUS A300 RESONANCE FREQUENCY STANDARD, PART 5; 53-30-30 PG.9 FIG.2 | . | . | . | . | |
99A53307267000 | AIRBUS A300-600 CALIBRATION BLOCK PART 4 53-30-52 PAGE 413 FIGURE 407. Material Aluminum 2024-T3 or T4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53307267000 304 | AIRBUS A300-600 CALIBRATION BLOCK PART 4 53-30-52 PAGE 413 FIGURE 407. Material: 304 Stainless Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53307267000 7075T6 | AIRBUS A300-600 CALIBRATION BLOCK PART 4 53-30-52 PAGE 413 FIGURE 407. Material Aluminum 7075-T6. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53307274000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD 51-10-16-991-005A, PAGE 10. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53307292001 | AIRBUS REFERENCE STANDARD A318-A321 51-10-15-991-004-A FASTENERS:(NAS5410-48). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53307319000 | AIRBUS A318/A319/A320/A321 REFERENCE BLOCK 51-10-31-PB4. FIGURE 51-10-31-991-004-A SHEET 01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53403003001 | AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53403003001 | AIRBUS REFERENCE STANDARD A300-600 53-16-02 FIGURE 603, PG. 607-608 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53403005001 | AIRBUS REFERENCE STANDARD PT 6 53-12-25 PAGE 605 FIGURE 604. . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53407285000 | AIRBUS A318/319/320/321 NTM 53-30-01-PB6 PAGE 9.. | . | . | . | . | |
99A53507286000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-51-09. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53803004001 | AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A53803024000 | AIRBUS REFERENCE STANDARD A300-600 53-12-98 FIGURE 403, PG. 404 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A54403004000 | AIRBUS REFERENCE STANDARD A300-600 A300-54-6015. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A55107288000 | AIRBUS REFERENCE STANDARD A300-600 PT4 55-10-14 FIGURE 404, PAGE 406 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A55107289000 | AIRBUS REFERENCE STANDARD A300-600 PT4 55-10-14 FIGURE 405, PAGE 407 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A55109003000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 55-10-72 FASTENER (HST756CB-6, HST881-8) | . | . | . | . | |
99A55307306000 | MUST BE MANUFACTURED FROM AN ACTUAL AIRCRAFT!!!....AIRBUS A318/A319/A320/A321 REFERENCE STANDARD. Figure 55-30-01-991-007-A. PART 4, PAGE 56. MATERIAL: MULTIDIRECTIONAL FABRIC. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A55407291000 | AIRBUS REFERENCE STANDARD A318-A321 PT 5 51-10-19 PAGE 16 FIGURE 51-10-16-991-005-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A55407322000 | AIRBUS REFERENCE STANDARD A318-A321 51-10-26PB9 | . | . | . | . | |
99A57004001291 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-53-05, PAGE 405 FIGURE 403 | . | . | . | . | |
99A57004001292 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-54-04 PAGE 405 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57004001320 | AIRBUS A310 REFERENCE STANDARD PART 4 57-21-85 PAGE 404 FIGURE 403 | . | . | . | . | |
99A57004101000 | AIRBUS REFERENCE STANDARD 57-21-25-270-801-A01 use green primer and silver metallic top coat for paint | . | . | . | . | |
99A57103001000 | AIRBUS A310 REFERENCE STANDARD 57-10-24 PART 4 FIGURE 403 PAGE 404. MATERIAL: 2024-T351 ALUMINUM...Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103003000 | AIRBUS A310 REFERENCE STANDARD 57-10-24 PART 4 FIGURE 404 PAGE 405. MATERIAL: 2024-T351 ALUMINUM...Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103005002 | AIRBUS A310 REFERENCE STANDARD PART 4 57-10-47 PAGE 406 FIGURE 403 2024-T351 ALUMINUM | . | . | . | . | |
99A57103006000 | AIRBUS SHOE PT 6 57-10-39 PAGE 404 FIGURE 403. . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103007000 | AIRBUS REFERENCE STAMDARD PT 6 57-10-39 PAGE 404 FIGURE 404. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103010000 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-41 FIGURE 403 PAGE 404. | . | . | . | . | |
99A57103011000 | AIRBUS A300-600 REFERENCE STANDARD PART 4, 57-10-41 FIGURE 404 PAGE 405 | . | . | . | . | |
99A57103012000 | AIRBUS A300-6-- REFERENCE STANDARD PART 4, 57-10-41 FIGURE 405 PAGE 406 | . | . | . | . | |
99A57103015000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-10-34 PAGE 405/406 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103025001 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-10 PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103028000 | AIRBUS REFERENCE STANDARD A300-600, PT 4 57-10-22 FASTENER (EN6115-7-13, NSA5050-7) | NSA5050-7 | . | . | . | |
99A57103029000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-10-06 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103030000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-10-06 PAGE 405 FIGURE 404. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103031000 | AIRBUS A310 REFERENCE STANDARD PART 4 53-15-42 PAGE 408 FIGURE 403 2024 ALUMINUM | . | . | . | . | |
99A57103033000 | AIRBUS REFERENCE STANDARD A310 PT 4 57-10-06 | . | . | . | . | |
99A57103034001 | AIRBUS A310 CALIBRATION STANDARD PART 4 57-10-28 PAGE 411/412 FIGURE 403 | . | . | . | . | |
99A57103036000 | AIRBUS REFERENCE STANDARD 57-10-67 FIG 403 | . | . | . | . | |
99A57103041000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-10-45 PAGE 406 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103042000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-10-45 PAGE 421 FIGURE 408. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103043000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 54-10-45 PAGE 440 FIGURE 413. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103044000 | AIRBUS REFERENCE STANDARD A300-600, 57-10-53 PT 4 FIG 403 | . | . | . | . | |
99A57103045000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 54-10-51 PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103046000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4 57-10-52 PAGE 415 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103048000 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-36 PAGE 407/408 FIGURE 403. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103048001 | Airbus A300-600 Reference Standard Part 4 57-10-68 Page 409/410 figure 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57103050000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 57-10-64 PAGE 407/408 FIG. 403 | . | . | . | . | |
99A57103051000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 57-10-22 | . | . | . | . | |
99A57103053000 | AIRBUS REFERENCE STANDARD A310 PT 4 57-10-07 | . | . | . | . | |
99A57103054000 | AIRBUS REFERENCE STANDARD PT 4 57-10-24 | . | . | . | . | |
99A57103056000 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-50 PAGE 411 FIGURE 403. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance(COC) | . | . | . | . | |
99A57104331000 | AIRBUS CALIBRATION BLOCK A318/A319/A320/A321: PART 4 57-00-00-991-003-A SHEET 01, PAGE 10. MATERIAL: 2024-T3 ALUMINUM | . | . | . | . | |
99A57104353000 | AIRBUS REFERENCE STANDARD A 330 PT 4 57-26-08 | . | . | . | . | |
99A57104353001 | AIRBUS REFERENCE STANDARD A330 PT 4 57-26-08 FIG 404 MATERIAL:2024-T3. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57104354000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-26-08. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57104355000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-26-08. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57204106000 | AIRBUS REFERENCE STANDARD PT 4 57-20-52 | . | . | . | . | |
99A57204387000 | AIRBUS A310 REFERENCE STANDARD PART 4 57-25-02 PAGE 405 FIGURE 404 2024-T351 ALUMINUM | . | . | . | . | |
99A57204390001 | AIRBUS REFERENCE STANDARD A300-600 PT4 57-21-30 FIGURE 405, PG. 406 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57204391001 | AIRBUS A310 REFERENCE STANDARD PART 4 57-25-26 PAGE 605 FIGURE 604 2024-T351 ALUMINUM | . | . | . | . | |
99A57204394000 | AIRBUS A310 REFERENCE STANDARD PART 4 57-25-65 PAGE 406 FIGURE 404 2024-T351 ALUMINUM | . | . | . | . | |
99A57204401000 | AIRBUS A310 REFERENCE STANDARD PART 4 57-25-49 PAGE 406 FIGURE 405 | . | . | . | . | |
99A57204402000 | AIRBUS REFERENCE STANDARD A300 PT 4 57-23-07-991-003-A . MATERIAL 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57204403000 | AIRBUS REFERENCE STANDARD A300 PT 4 57-00-11 FIG.3 SHEET 1 PG.5-6, A310 PT 4 57-51-24. MATERIAL 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57204403001 | AIRBUS CALIBRATION BLOCK A300-600 PART 4 57-21-96 PAGE 404&405 and A318/A319/A320/A321: PART 4 57-20-64-991-006-A SHEET 1-2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57204406000 | AIRBUS A300-600 CALIBRATION STANDARD PART 4, 57-20-16 PAGE 405 FIGURE 403 | . | . | . | . | |
99A57204408000 | AIRBUS A300-600 CALIBRATION STANDARD PART4, 57-20-16 PAGE 406 FIGURE 404 | . | . | . | . | |
99A57204410000 | AIRBUS A310 REFERENCE STANDARD PART 4 57-21-16 PAGE 408 FIGURE 404 | . | . | .. | . | |
99A57204425000 | AIRBUS REFERENCE STANDARD A300-600 57-21-25 FIGURE 402, PAGE 403 . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99A57204438001 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 406 FIGURE 403. Includes Test Report and certificate of Conformance. | . | . | . | .. | |
99A57204453000 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 406 FIGURE 403. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99A57204454000 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 407/408 FIGURE 404. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99A57204455000 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 407/408 FIGURE 404. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99A57504294000 | AIRBUS A300-600 CALIBRATION STANDARD PT 6 57-52-05 PAGE 606 FIGURE 602 (SHEET 2). MATERIAL: 2024-T3 ALUMINUM. CR3222-4-02, ALT FOR(NSA542-12) RIVET Includes Test Report and Certificate of Conformance. | CR3222-4-02 RIVET | NSA542-12 | . | . | |
99A57504296000 | AIRBUS REFERENCE STANDARD A300 57-42-11, A300-600 57-51-34 and A310 57-51-11 PART PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D51103001000 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, FIGURE 51-10-04-991-014-A. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D51103016000 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, FIGURE 51-10-31-991-004-A. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D51107295000 | AIRBUS REFERENCE STANDARD A318-A321 51-10-11 FIG 604 FASTENER (LN9199) | . | . | . | . | |
99D52103001000 | AIRBUS Reference standard A318/319/320/321 NTM 52-11-04, PB 6 Page 10.. | . | . | . | . | |
99D52809004000 | AIRBUS REFERENCE STANDARD A318-A321 52-81-06-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D53103000000 | AIRBUS A318/A319/A320A/A321 REFERENCE STANDARD PART 4 53-11-04 PAGE 404 FIGURE 404 | 119 | . | . | . | |
99D53103001000 | AIRBUS REFERENCE STANDARD A318/319/320/321 NTM 53-11-82-PB6 Page 14 Figure 403.. | . | . | . | . | |
99D53103002000 | AIRBUS Reference standard A318/319/320/321 NTM 57-11-85, Part 4 Page 405/405A, Figure 403. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
99D53203000002 | AIRBUS REFERENCE STANDARD A318-A321 PT 6 53-21-86 FASTENER (ASN-A2026V3-4, ASN-A2026V3-5, ASN-A258-3) | ASNA2026V3-5 | ASNA2528-3 | . | . | |
99D53203001000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD, 53-00-13 PB6 PAGE 6 | . | . | . | . | |
99D53207304000 | AIRBUS REFERENCE STANDARD A318-A321 PT 6 53-41-45 FASTENER (LGPL2SCV06-05, LGPL2SCV06-06, ASNA2025-3) | . | . | . | . | |
99D53409001000 | AIRBUS REFERENCE STANDARD A318-A321 PT 6 53-41-37 FASTENER (NAS1097D5-6) | . | . | . | . | |
99D54403000004 | AIRBUS REFERENCE STANDARD A320 PT4 54-51-02-PB4:PG12..FIG54-51-02-991-004-A SHEET01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D54403001000 | AIRBUS REFERENCE STANDARD A318/319/320/321 NTM 54-51-01-PB6 PAGE 606 FIGURE 604.. | . | . | . | . | |
99D54403001002 | AIRBUS REFERENCE STANDARD 54-51-01-991-003-A, 4340 STEEL.HOLE SIZES: 11.1mmØ, 11.5mmØ, 11.9mmØ and15.8mmØ. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D54403002000 | AIRBUS REFERENCE STANDARD A318-A321 54-51-23 | . | . | . | . | |
99D54403003000 | AIRBUS REFERENCE STANDARD A318-A321 54-51-23 | . | . | . | . | |
99D54403004000 | AIRBUS REFERENCE STANDARD A318-A321 54-51-15 PT 4 FIG 404 | . | . | . | . | |
99D54403005000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 54-51-15 | . | . | . | . | |
99D54403007000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD 54-51-80 PART 4 PYLON AFT FIXED FAIRING UPPER SPAR. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D54503004000 | AIRBUS CALIBRATION BLOCK A318/A319/A320/A321: PART 4 54-52-17-991-003-A SHEET 01, PAGE7. MATERIAL: 15-5PH STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D54503006000 | AIRBUS CALIBRATION BLOCK : PART 4 54-53-08-991-007-A SHEET 01. MATERIAL: 15-5PH STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D54503007000 | AIRBUS CALIBRATION BLOCK : PART 4 54-53-09-991-003-A SHEET 01. MATERIAL: 15-5PH STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D55109001000 | AIRBUS A318/A319/A320/A321 CARBON STANDARD PT 4 51-10-06 PAGE 7. MULTIDIRECTIONAL TAPE MATERIAL BLOCK SET OF 4 includes waterproof case. NOMINAL THICKNESS (1mm, 3mm, 5mm, 7mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D55109001000/1MM | AIRBUS A318/A319/A320/A321 CARBON STANDARD PT 4 51-10-06 PAGE 7. MULTIDIRECTIONAL TAPE MATERIAL BLOCK NOMINAL THICKNESS (1mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57004000000 | Airbus Calibration Standard Block Set. A340-200/-300 51-63-03 Pg. 2-3, A300, A300-600, A310, A318/A319/A320/A321, A330, A340, A380 51-34-03, Figure 1 Sheett 1 Pg.1-2. Material: AMS-QQ-A-250 2024-T351 Aluminum. Includes Test Report and Certificate of C... | . | . | . | . | |
99D57004001000 | AIRBUS A318/A319/A320/A321 CALIBRATION BLOCK SET. 51-63-03-PB1 PAGES 4&5, FIGURE 51-63-03-991-002-A SHEET 01 and FIGURE 51-63-03-991-002-A SHEET 03 | . | . | . | . | |
99D57004001001 | AIRBUS A318/319/320/321 REFERENCE STANDARD 51-63-03-PB1 PAGE 4 | . | . | . | . | |
99D57004001002 | AIRBUS A318/319/320/321 REFERENCE STANDARD 51-63-03-PB1 PAGE 5 | . | . | . | . | |
99D57103002001 | AIRBUS REFERENCE STANDARD A318-321 57-1-85-PB4 | . | . | . | . | |
99D57103004000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-81 | . | . | . | . | |
99D57103005001 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-83 | . | . | |||
99D57103006000 | AIRBUS REFERENCE STANDARD PT 4 57-11-83. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103007000 | AIRBUS REFERENCE STANDARD , A320 PT4 57-11-81-PB4:PG15 - CAA+PRIMER | . | . | . | . | |
99D57103008000 | AIRBUS REFERENCE STANDARD PT 4 57-11-82 | . | . | . | . | |
99D57103009000 | AIRBUS REFERENCE STANDARD. MATERIAL: 7175-T7 ALUMINUM ANODIZED. PAINT WITH PRIMER | . | . | . | . | |
99D57103010000 | AIRBUS REFERENCE STANDARD 57-11-82 PT 4 FIG 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103011000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-82. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103012000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-82. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103013000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 PT 4 57-11-47 FIGURE 403 SHEETS 1&2 PAGE 405-406. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103014000 | AIRBUS REFERENCE STANDARD A318 - A321 57-11-85-PB 4. Surface Annodizing, Primer+ Top Coat. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103015000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-47 FIG 412. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103016000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-47 FIG 417. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103017000 | AIRBUS REFERENCE STANDARD A318-A321 57-11-75-991-012-A FASTENER (ASNAA2027V7-8, NAS5050-7). Includes Test Report and Certificate of Conformance. | . | . | |||
99D57103018000 | AIRBUS REFERENCE STANDARD A318-A321 57-11-75-991-012-A FASTENER (ASNAA2027V7-8, NAS5050-7). Includes Test Report and Certificate of Conformance. | . | . | |||
99D57103019000 | AIRBUS REFERENCE STANDARD A318-A321 57-11-75-991-012-A FASTENER (ASNAA2027V7-8, NAS5050-7). Includes Test Report and Certificate of Conformance. | . | . | |||
99D57103020000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-74 FASTENER (ASNA2027V7-7, NAS5050-7) | . | . | . | . | |
99D57103021000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-47 FIG 411 | . | . | . | . | |
99D57103023000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-12-04 Page 47 Sheet 01, 57-12-04-991-013-A REVISION 114 | . | . | . | . | |
99D57103024000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-12-04 Page 11 Sheet 01, 57-12-04-991-020-A REVISION 114 | . | . | . | . | |
99D57103025000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-11-73 Page 52 Sheet 01, 57-11-73-991-020-A REVISION 114. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103026000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-11-73 Page 52 Sheet 01, 57-11-73-991-020-A SHEET 02 REVISION 115. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103027000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-12-03 Page 73 Sheet 01, 57-12-03-991-020-A REVISION 114 | . | . | . | . | |
99D57103028000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-12-03 Page 99 Sheet 01, 57-12-03-991-020-A REVISION 114 | . | . | . | . | |
99D57103029000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-12-02 Page 99 Sheet 01, 57-12-02-991-003-A SHEET 1. | . | . | . | . | |
99D57103031000 | Airbus A318/A319/A320/A321 Reference Block. 2024 Aluminum. PB4 57-12-04 Page 114 Sheet 01, 57-12-04-991-020-A REVISION 114. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57103032000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-82-991-003-A SHEET 01 PG.6. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99D57103033000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-82-991-008-A PAGE 406 MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99D57103034000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-81-991-008-A PAGE 1. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99D57103035000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-81-991-003-A PAGE 1. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99D57103036000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-47-991-003-A . Material: 7075 Aluminum Includes Test Report and certificate of Conformance. | . | . | . | . | |
99D57204101000 | AIRBUS PROBE GUIDE A318-A321 PT 6 57-26-54 | . | . | . | . | |
99D57204105000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-26-54 | . | . | . | . | |
99D57204107000 | AIRBUS REFERENCE STANDARD A330 57-20-55-991-007-A (SHEET O1 and SHEET 02, PAGE 8&9 and ( A318-A321 57-21-10-PB4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57204108000 | AIRBUS GUIDE BLOCK A318-A321 PT 4 57-21-10 FIG 412 | . | . | . | . | |
99D57204116000 | AIRBUS SEARCH UNIT GUIDE BLOCK A318A-321 PT 4 57-26-54 | . | . | . | . | |
99D57204125000 | AIRBUS REFERENCE STANDARD A318/319/320/321 NTM 57-29-04-PB4 PAGE 405 FIGURE 403.. | . | . | . | . | |
99D57204163000 | 3 Titanium Aircraft Bolts, 99D57204163000-A, 99D57204163000-B, and 99D57204163000-C | . | . | . | . | |
99D57204164000 | AIRBUS REFERENCE STANDARD A318/319/320/321 NTM 57-29-07-PB4 PAGE 17.. | . | . | . | . | |
99D57204164001 | AIRBUS REFERENCE STANDARD A318-A321 57-29-07-PB4 PAGE 23 FIGURE 57-29-07-991-003-A SHEET 01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57204169000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.9 FASTENER (EN6114K4-5, EN6114K5-9). MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includest Certification and COC. | EN6114K5-4/-1 | HILOCK | . | ||
99D57204169001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.9 FASTENER (EN6114K4-5, EN6114K5-9). MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includest Certification and COC. | . | . | . | . | |
99D57204170000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11 FASTENER (EN6114K4-6, EN6114K5-9). MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includest Certification and COC. | EN6114K5-4/-1 | HILOCK | . | ||
99D57204170001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11 FASTENER (EN6114K4-6, EN6114K5-9). Includes Test Report and Certificate of Conformance | . | . | . | . | |
99D57204171000 | AIRBUS REFERENCE STANDARD A318-A321 57-29-09-PB4 2024-T6(ALTERNATE TO 2014-T6) | . | . | . | . | |
99D57204175000 | AIRBUS REFERENCE STANDARD A318-A321, 57-29-13-003-A | . | . | . | . | |
99D57204175000/S | AIRBUS REFERENCE STANDARD A318-A321, 57-29-13-003-A, 4340 | . | . | . | . | |
99D57204183000 | Airbus Tap Test Tool Figure 51-10-03-991-008-A. Corrosion Resistant Steell or Commercial Milled Steel. Includes Certificate of Conformance. | . | . | . | . | |
99D57204188000 | AIRBUS A320 CALIBRATION STANDARD FIGURE 2 PROCEDURE D. A320 FWD SPAR LOWER FLANGE RIB 22-27. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57204193000 | AIRBUS CALIBRATION STANDARD, Material AL 7010/7050-T7651, EDM Notch 5mm (H) x 5mm (L) x 0.18mm (W) +/- 0.02mm, Paint all surfaces with primer (Material No. 16-006) . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57204196000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11 FASTENER (EN6114K4-6, EN6114K5-9). MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57204197000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11 FASTENER (EN6114K4-6, EN6114K5-9). MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includes Test Report and Certificate of Conformance. Note: Repair Plate = .236" | . | . | . | . | |
99D57504100000 | AIRBUS REFERENCE STANDARD INBOARD LUG 2024-T351 ALUMINUM. PART 4: 57-52-50 FIGURE 403 PAGE 404 | . | . | . | . | |
99D57504102000 | AIRBUS REFERENCE STANDARD OUTBOARD LUG 2024-T351 ALUMINUM. PART 4: 57-52-50 FIGURE 403 PAGE 404 | . | . | . | . | |
99D57504103001 | AIRBUS REFERENCE STANDARD A318-A321 PT 04 57-51-01 | . | . | . | . | |
99D57504107000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD INBOARD LUG 2024-T351 ALUMINUM. PART 4: 57-53-50 FIGURE 403 PAGE 404 | . | . | . | . | |
99D57504108000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD OUTBOARD LUG 2024-T351 ALUMINUM. PART 4: 57-53-50 FIGURE 404 PAGE 405 | . | . | . | . | |
99D57504109000 | AIRBUS REFERENCE STANDARS A318-A321 57-51-63-991-004-A FASTENER (ASNA2027VBV6-8 + ABS0117-6K7, ASNA2027VBV4-8 + ABS0117-4K7). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99D57704100000 | AIRBUS REFERENCE STANDARD A318/319/320/321 57-70-06, PG. 404, FIGURE 402. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103000000 | AIRBUS REFERENCE STANDARD A300 SERIES PT 6 53-12-25 FASTENER (ASNA2019-36) Annodize per(13-002) Primer(16-006) top coat(16-008) sealant(09-002) | . | . | . | . | |
99F53103003000 | AIRBUS REFERENCE STANDARD A330 53-11-65-PB4. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103004000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 53-11-08-991-004-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103005000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 53-11-09-991-003-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103006000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 53-11-48-991-004-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103007000 | AIRBUS REFERENCE STANDARD A330, 53-11-82-991-003-A FASTENER (ASNA2391-3-6 + ASNA2025-3). lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103009000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-11-08-009-A. MATERIAL: 2024 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53103010000 | AIRBUS REFERENCE STANDARD A330 53-11-79-991-003-A PB4. MATERIAL: 2024-T3 ALUMINUM. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53113000000 | AIRBUS A330/200-300 REFERENCE STANDARD PART 4 53-11-96 FIGURE 403 SHEET 1, 2024-T3 ALUMINUM. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53113002000 | AIRBUS CALIBRATION STANDARD A330-200/300 53-11-55 PAGE 28 FIGURE 53-11-55-013-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53113005000 | AIRBUS CALIBRATION STANDARD A330-200/300 53-11-55 PAGE 15 FIGURE 53-11-55-007-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53207310000 | AIRBUS REFERENCE STANDARD A330 53-21-56-PB6 FASTENER (LN9199). lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53207313000 | AIRBUS REFERENCE STANDARD A330 53-21-36 FIG 619. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53207314000 | AIRBUS CALIBRATION STANDARD A330 PART 6 53-21-36 PAGE 637 FIGURE 620. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53207316000 | AIRBUS REFERNCE STANDARD A330 53-21-36-PB6. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53207317000 | AIRBUS REFERNCE STANDARD A330 53-21-36-PB6. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53207318000 | AIRBUS REFERNCE STANDARD A330 53-21-36-PB6. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303000001 | AIRBUS CALIBRATION STANDARD A340-200/-300 FIGURE 53-31-39-991-003-A. MAERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303001001 | A340-200/-300 AIRBUS REFERENCE BLOCK FIGURE 53-31-39-991-008-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303005000 | AIRBUS REFERENCE STANDARD A30 PT 6 53-31-09 FASTENER (ASNA2391-3-06 + ASNA2025-3) | . | . | |||
99F53303008000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-31-07 FIGURE 403 PAGE 407/408, MATERIAL 7075 ALUMINUM. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303008001 | AIRBUS REFERENCE STANDARD A330 53-31-07-PB4. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303009000 | AIRBUS REFERENCE STANDARD A330 PT 6 53-30-10 FASTENER (ASNA 2391-4-07 + ASNA2025-4). lncludes Test Report and Certificate of Conformance. | ASNA2528-4 | . | . | . | |
99F53303010000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-31-14. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303011000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-31-56. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303012000 | AIRBUS REFERENCE STANDARD A330 53-31-61-991-010-A. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303013000 | AIRBUS REFERENCE STANDARD PT 4 53-31-61, PAGE 404 FIGURE 403 | . | . | . | . | |
99F53303015000 | AIRBUS REFERENCE STANDARD A340-200/-300 53-31-13-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303017000 | AIRBUS REFERENCE STANDARD A330 53-11-84-PB6 FASTENER (ASNA2019-48-13). lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303018000 | AIRBUS REFERENCE STANDARD A300 SERIES PT 6 53-11-88 FASTENER (ASNA2019-36) Annodize per(13-002) Primer(16-006) top coat(16-008) sealant(09-002) | . | . | . | . | |
99F53303019000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-11-30. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303020000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-11-44. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303021000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-11-44. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303023000 | AIRBUS REFERENCE STANDARD 53-30-16-PB6 FASTENER (ASNA2391-3-05, ASNA2391-3-06, ASNA2025-3) | ASNA2391-3-06 | ASNA2025-3 | |||
99F53303026000 | AIRBUS REFERENCE STANDARD A330 PT 6 53-30-18-PB6 FASTENER (EN6114V3-5, EN6114V3-6, ASNA2528-3). lncludes Test Report and Certificate of Conformance. | EN6114V3-6 | ASNA2528-3 | |||
99F53303027000 | AIRBUS REFERENCE STANDARD A330 PT 6 53-30-18-PB6 FASTENER (EN6114V3-6, ASNA2026V3-6, ASNA2528-3). lncludes Test Report and Certificate of Conformance. | ASNA2026V3-8 | ASNA2528-3 | |||
99F53303029000 | AIRBUS REFERENCE STANDARD A330 53-31-45-991-003-A . PAGE 1. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303030000 | AIRBUS REFERENCE STANDARD A330 PT 6 53-30-19. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303073000 | AIRBUS CALIBRATION STANDARD A340-500/-600 FIGURE 53-39-22-991-038-A SHEET 1. MAERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303080000 | AIRBUS REFERENCE STANDARD A340-500/600 FIGURE 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303084000 | AIRBUS CALIBRATION STANDARD A340-500/-600 FIGURE 53-39-22-991-038-A SHEET 2. MAERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303085000 | AIRBUS REFERENCE STANDARD A330 53-31-62-991-013-A. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303086000 | AIRBUS REFERENCES STANDARD A330, 53-31-87-PB4 FASTENER (EN6115V3-3, NAS5050-3). lncludes Test Report and Certificate of Conformance. | NSA5050-3 | . | . | ||
99F53303087000 | AIRBUS REFERENCES STANDARD A330, 53-31-87-PB4 FASTENER (EN6115V3-3, NAS5050-3). lncludes Test Report and Certificate of Conformance. | NSA5050-3 | . | . | ||
99F53303088000 | AIRBUS REFERENCE STANDARD A330 53-31-11-PB4. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303090000 | AIRBUS REFERENCE STANDARD A340-200/-300 53-31-12-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303091000 | AIRBUS REFERENCE STANDARD A330 53-31-12-PB4. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303092000 | AIRBUS REFERENCE STANDARD Figure 53-31-96-991-003-A. Includes Test Report and Certificate of Conformance | . | . | . | . | |
99F53303094000 | AIRBUS REFERENCE STANDARD A330 53-30-22-PB4 FASTENER (ASNA2391). lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303095000 | AIRBUS REFERENCE STANDARD A340-200/-300 53-30-24-PB4 FASTENER (ASNA2391). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303096000 | AIRBUS REFERENCE STANDARD A330/A340-200/-300 53-30-29-PB4. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303097000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-70 PAGE 6. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303098000 | AIRBUS A340 REFERENCE STANDARD FIGURE 53-30-66-991-006-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303099000 | AIRBUS REFERENCE STANDARD A330 Figure 53-30-42-991-003-A, page 8, FUSELAGE INTERNAL SPLICING TO FR40 FORWARD FITTING AND REAR FITTING. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303100000 | AIRBUS A330 REFERENCE BLOCK 53-30-51-991-003-A. MATERIAL: 7075 OR EQUIVQLENT ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303101000 | AIRBUS A330 REFERENCE BLOCK 53-30-52-991-003-A. MATERIAL: 7050 OR EQUIVALENT ALUMINUM. US INSPECTION OF MAIN LONGERON EXTENSION BETWEEN FR53.2 AND FR53.3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303103000 | AIRBUS REFERENCE STANDARD A330 53-31-89. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303104000 | AIRBUS A330 REFERENCE BLOCK, 2024 ALUMINUM 53-30-65 PART 4. ATTACHMENT FITTING OF ROD LINK BETWEEN CROSS BEAL FLOOR AND FRAME AT FR53.3 TO FR54 LH/RH | . | . | . | . | |
99F53303105000 | AIRBUS A330 REFERENCE STANDARD. 53-30-30-991-003-A , PAGE 6. FUSELAGE LONGITUDINAL BUTT JOINT ATSTR 30, FROM 38 TO FR 40, LH/RH | . | . | . | . | |
99F53303107000 | AIRBUS REFERENCE STANDARD A340-500/-600 53-39-08-22-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303108000 | AIRBUS REFERENCE STANDARDS A340-500/-600 53-39-08-22-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303109000 | AIRBUS REFERENCE STANDARD A340-500/-600 53-39-19-270-801-A-01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303113000 | AIRBUS REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. 2 CORNER EDM SLOTS: 3mm x 3mm(.120" x .120") x 0.3mm(.012") Wide. Paint with primer. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303115000 | AIRBUS REFERENCE STANDARD A330 53-30-54 PAGE 6. US INSPECTION OF FUSELAGE INTERNAL STRUCTURE, SKIN PANEL JUNCTION WITH FR53.2 BULKHEAD FWD FACE BETWEEN STR39 AND STR42. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303118000 | AIRBUS A330/200-300 REFERENCE STANDARD PART 4 53-30-23 FIGURE 403 SHEET 1, PAGE 407. 2024-T3 ALUMINUM | . | . | . | . | |
99F53303119000 | AIRBUS A330 REFERENCE STANDARD PART 4 53-30-70-991-008-A PAGE 7. MATERIAL: 7050 or EQUIVALENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303119001 | AIRBUS A330 REFERENCE STANDARD PART 4 53-30-70 PAGE 9. MATERIAL: 7050 or EQUIVALENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303120000 | AIRBUS A330-300/A340-200 CALIBRATION STANDARD 53-30-28 FIGURE 53-30-28-005-A. MATERIAL: 7075-T7351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53303121000 | AIRBUS A330 REFERENCE STANDARD PART 4 53-30-71-991-004-A SHEET 1, 7175-T7351 ALUMINUM. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F53307305001 | AIRBUS REFERENCE STANDARD A330 51-31-80 PB6 PAGE 12. A340 53-31-81 PB6 PAGES 609-610. FASTENER (HL11VF6-4, HL11VF6-5, HL70-6). Includes Certification Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
99F53507256000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-51.09 FIG 404. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54403000001 | AIRBUS REFERENCE STANDARD A330 54-51-38 PT 4 FIG 403. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54403001001 | AIRBUS REFERENCE STANDARD A330 PT 4 54-51-36. ludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54403002001 | AIRBUS REFERENCE STANDARD A330 PT 4 54-51-40. ludes Test Report and Certificate of Conformance. | . | . | |||
99F54403002002 | AIRBUS REFERENCE STANDARD A330 54-51-40-991-008-A Page 15. Material 15-5PH. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54503009000 | AIRBUS REFERENCE STANDARD A330 54-51-40-PB4 PAGE 46 FIGURE 54-51-40-991-014-A SHEET 01. FASTENER (NAS5415-36). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54503010000 | AIRBUS REFERENCE STANDARD A330 FIGURE 54-51-40-991-019-A .FASTENER (NAS5415-36). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54503011000 | AIRBUS REFERENCE STANDARD A330 54-51-40-PB4. MATERIAL 15-5PH STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F54503012000 | AIRBUS REFERENCE STANDARD A330 54-51-04-PB6. ludes Test Report and Certificate of Conformance. | . | . | |||
99F54503015000 | AIRBUS REFERENCE STANDARD A330 54-54-19-991-003-A. MATERIAL: TA6V TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F55109001000 | AIRBUS REFERENCE STANDARD A330 PT 4 55-10-09. Includes Test Report and Certificate of Conformance | . | . | . | . | |
99F55109002000 | AIRBUS REFERNECE STANDARD A330 PT 4 55-10-09. Includes Test Report and Certificate of Conformance | . | . | . | . | |
99F57004100001 | AIRBUS REFERENCE STANDARD A340-500/-600 57-00-11-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57004101001 | AIRBUS REFERENCE STANDARD A330 57-00-11 FIG 403. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103006000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-48. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103007000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-44. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103008000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-11-07. PAGE 404 FIGURE 403. Includes test Report and Certificate of Conformance(COC). | . | . | . | . | |
99F57103009000 | AIRBUS REFERENCE STANDARD A340-200/*-300 57-11-38-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103010000 | AIRBUS REFERENCE STANDARD A330 57-11-52. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103011000 | AIRBUS REFERENCE STANDARD 330 57-11-00-200-822A A340-200/-300 57-11-52-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103012001 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-22. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103016001 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-46 FASTETNER (ASNA2027V7-11 + NSA5050-7, ASNA2027V8-11 + NSA5050-8). | . | . | . | . | |
99F57103017000 | AIRBUS REFERENCE STANDARD A330 [T 4 57-11-59. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103018000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-45. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103019000 | AIRBUS REFERENCE STANDARD A330 PT46 57-11-25. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103026000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-11-62-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103028000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-11-63-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103029000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-57. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103030000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-58. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103031000 | AIRBUS REFERENCE STANDARD Figure 57-11-10-991-033-A. Includes Test Report and Certificate of Conformance | . | . | . | . | |
99F57103032000 | AIRBUS REFERENCE STANDARD 57-11-22-991-003-A.. | . | . | . | . | |
99F57103041000 | AIRBUS REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. Includes Test Report and Certificate of Conformance(COC) | . | . | . | . | |
99F57103042001 | AIRBUS REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. APPLY TOP COAT 16-008. Includes Test Report and Certification of Conformance(COC) | . | . | . | . | |
99F57103046000 | AIRBUS REFERENCE STANDARD A340 57-18-11-991-036-A FASTENER (EN6115V6-11 + NSA5050-6). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103048000 | AIRBUS REFERENCE STANDARD A340-200/300 57-11-63-PB4 FASTENER (NSA5359-6-8 + NSA5050-6). Includes Test Report and Certificate of Conformance. | NSA-5050-6 | . | . | ||
99F57103051000 | AIRBUS REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. APPLY TOP COAT 16-008 | . | . | . | . | |
99F57103052000 | AIRBUS REFERENCE STANDARD 57-11-71-PB4 | . | . | . | . | |
99F57103054000 | AIRBUS REFERENCE STANDARD A330 57-20-96-991-003-A. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103056000 | AIRBUS REFERENCE STANDARD A340-500/600 57-18-25-991-004-A . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103057000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-79-991-003-A. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57103059000 | AIRBUS REFERENCE STANDARD57-11-68-991-007-A. MATERIAL: 7175 or 7075 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57203000000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-20-84. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57203001000 | AIRBUS A340 REFERENCE STANDARD FIGURE 57-20-84-991-008-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57203002000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-20-86-991-003-A. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204102000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-20-16-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204106000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-20-52. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204108000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-26-10. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204109001 | AIRBUS REFERENCE STANDARD A330 PT 4 57-26-10. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204110000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-11-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204111000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-11-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204114000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-10 PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204115000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-10. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204118000 | AIRBUS PROBE GUIDE A340 PT 6 57-26-08. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204120000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-26-12. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204122000 | AIRBUS PROBE GUIDE A340 PT 6 57-26-09. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204124000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-08. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204124001 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-08-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204125000 | AIRBUS PROBE GUIDE A330 PT 4 57-26-08-PB6. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204128000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-09. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204128001 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-09-PB4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204130000 | AIRBUS REFERENCE STANDARD A330 57-20-47 FIG 405. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
99F57204133000 | AIRBUS GUIDE BLOCK A340 PT 4 57-26-09. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204134000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-08. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204135000 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403 SHEET 1 PAGE 407. Includes Test Report and Certificate of Conformance. | NSA5472-10K7 | . | . | ||
99F57204136000 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403 SHEET 1 PAGE 407. Includes Test Report and Certificate of Conformance. | NSA5472-12K7 | . | . | ||
99F57204137000 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403. Includes Test Report and Certificate of Conformance. | NSA5472-12K7 | . | . | ||
99F57204138001 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403. Includes Test Report and Certificate of Conformance. | NSA5472-14K7 | . | . | ||
99F57204140000 | AIRBUS REFERENCE STANDARD A330 57-20-02 FIG 603 FASATENER (ASNA2027VHK5-13, ABS0813-5C) | ABS0813-5C | . | . | ||
99F57204144000 | AIRBUS REFERENCE STANDARD A330 57-20-93 FIG 403 FASTENER (ASNA2026-7-19, NSA472-7K7) | NSA5472-7K7 | . | . | ||
99F57204145000 | AIRBUS REFERENCE STANDARD A330 57-20-15 FIG 402 Includes Certification Report and Certificate of Conformance. | . | . | . | ||
99F57204146000 | AIRBUS REFERENCE STANDARD A330 57-20-49 FIG 403 SHEET 1 PAGE 406. Includes Test Report and Certificate of Conformance. | NSA5050-9 | . | . | ||
99F57204171000 | AIRBUS REFERENCE STANDARD A340-500/-600 57-26-59-PB6. Includes Test Report and Certificate of Conformance. | . | . | |||
99F57204172000 | Airbus A330-300} {A330-200}, 57-29-05 SPIGOT FITTING ATTCHMENT FLANGE AT HOLES 5 AND 11, LH/RH WINGS (2017-02-23 09:21:37) Mateial: 2024-T351. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204173000 | AIRBUS A330 REFERENCE STANDARD 57-20-46-270-801-A-01 PAGE 12. OUTER WING REAR SPAR UPPER & LOWER FLANGES BETWEEN RIB7 and RIB12 LH/RH. MATERIAL: 7010 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204174000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204175000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204176000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57204177000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57244001000 | AIRBUS A330 REFERENCE STANDARD PART 4 57-24-04-991-010-A SHEET 1, 2024-T351 ALUMINUM. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57500001000 | AIRBUS CALIBRATION STANDARD A340-200/-300, FIGURE 57-29-02-991-003-A. MATERIAL: 7050-T7651 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57603001000 | AIRBUS REFERENCE STANDARD PT 4 57-61-16 | . | . | . | . | |
99F57603002000 | AIRBUS REFERERENCE STANDARD A330 PT 4 57-61-06. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57603004000 | AIRBUS REFERENCE STANDARD A330 57-61-14-PB4. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57603005000 | AIRBUS REFERENCE STANDARD A330 57-61-14-PB4. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99F57603006000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 57-61-21-991-003-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99L52103000000 | AIRBUS REFERENCE STANDARD A380 52-81-01-991-012-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L52107325000 | AIRBUS REFERENCE STANDARD A380 52-11-01-01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53103000000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-11-03-991-009-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53103001000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-11-12-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53103002000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-11-03-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53103004000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-09-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53103005000 | A380 REFERENCE STANDARD 7010 ALUMINUM; FIGURE:53-11-23-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53103006000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-07-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53103008000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-11-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53103010000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-31-24-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53103012000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.53-11-22-991-009-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53103013000 | A380 REFERENCE STANDARD 7010 OR EQUIVALENT ALUMINUM; FIG.53-11-20-991-003-A SHEET 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53103020000 | AIRBUS A380 REFERENCE STANDARD FIGURE 7 53-11-10-010-A PG. 25. Material: 7075-T751 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53103021000 | AIRBUS A380 REFERENCE STANDARD FIGURE 6 53-11-02-009-A PG. 17-18. Material: 7075-T7 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53113002000 | AIRBUS A380 REFERENCE STANDARD FIGURE 6 53-11-10-009-A PG. 24. Material: 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303000000 | AIRBUS REFERENCE STANDARD A380 53-31-37-991-006-A FASTENER (EN6115V6-9, NSA5050-6). Includes Test Report and Certificate of Conformance. | NSA5050-6 | . | . | ||
99L53303001000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-36-991--003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303002000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-31-22-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303003000 | AIRBUS REFERENCE STANDARD A380-800 53-31-22-991-009-A (SHEET 02). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303004000 | AIRBUS REFERENCE STANDARD A380-800 53-31-22-991-009-A (SHEET 03). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303005000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-21-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303008000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-19-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303009000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-31-20-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53303016000 | A380 REFERENCE STANDARD 7075-T6 OR 7075-T7 ALUMINUM; FIGURE:53-31-30-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53303017000 | A380 REFERENCE STANDARD 7050-T73 OR 7075-T73 ALUMINUM; FIG.53-31-30-991-009-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L53303019000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-11-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303021000 | AIRBUS A380-800 CALIBRATION BLOCK 53-31-33-991-006-A (SHEET 01& 02) PAGES 20-21. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303022000 | AIRBUS A380-800 FIGURE 53-31-12-991-003-A PAGE 445. MATERIAL: 2024 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303024000 | AIRBUS REFERENCE STANDARD A380-800 53-31-22-991-009-A (SHEET 01). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303025000 | AIRBUS A380-800 53-31-04-010-A. MATERIAL: 2024 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303027000 | AIRBUS REFERENCE STANDARD A380-800 53-31-37-991-013A. MATERIAL: 7475 OR EQUIVALENT 7050 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303030000 | AIRBUS REFERENCE STANDARD A380-800 53-31-62-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303031000 | AIRBUS REFERENCE STANDARD A380-800 53-31-60-991-015-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303032000 | A380-800 REFERENCE STANDARD 7075 ALUMINUM; FIGURE:53-31-53-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303033000 | AIRBUS REFERENCE STANDARD A380-800 53-31-63-991-003-A. MATERIAL: 7175-T73 OR EQUIVALENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53303035000 | AIRBUS REFERENCE STANDARD A380 53-31-27-991-021-A PAGE 23. MATERIAL: 7175 OR 7075 ALUMINUM. Includes Certificate of Conformance. | . | . | . | . | |
99L53303037000 | AIRBUS REFERENCE STANDARD A380 53-31-27-991-020-A PAGE 22. MATERIAL: TEFLON. Includes Certificate of Conformance. | . | . | . | . | |
99L53509001000 | AIRBUS A380 REFERENCE STANDARD 7050-T7 OR 2024 ALUMINUM; FIGURE:53-51-02-991-008-A. Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
99L53509002000 | AIRBUS REFERENCE STANDARD A380-800 53-51-36-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53509003000 | AIRBUS REFERENCE STANDARD A380-800 53-51-08-991-004-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53509006000 | AIRBUS REFERENCE STANDARD A380-800 53-51-37-270-801-A-01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L53509008000 | AIRBUS A380-800 REFERENCE STANDARD TITANIUM 6AL 4V; FIGURE:53-51-58-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L54503000000 | AIRBUS A380 REFERENCE STANDARD FIGURE:54-51-04-991-012-A. MATERIA L: 600/700 SERIES INCONEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L54503003000 | AIRBUS A380 REFERENCE STANDARD 7050-T7 OR 2024 ALUMINUM; FIGURE:54-51-06-991-010-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L54503004000 | AIRBUS A380-800 54-51-05 SHEET 02 UPPER SPAR. MATERIAL: TA6V B(6AL-4V TITANIUM). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L54503005000 | AIRBUS REFERENCE STANDARD A380-800 54-51-03-991-004-A. MATERIAL: TA6V B Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L54503005000 | AIRBUS REFERENCE STANDARD A380-800 54-52-02-991-021-A. MATERIAL: TA6V B Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L54503006000 | AIRBUS REFERENCE STANDARD A380-800 54-52-02-991-022-A, MATERIAL:TA6VB Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L55209001000 | AIRBUS REFERENCE STANDARD 55-21-03-991-003-1. 7050-T7451 ALUMINUM | . | . | . | . | |
99L57103002000 | A380-800 REFERENCE STANDARD FIGURE:53-11-03-991-008-A. Material: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57203000000 | AIRBUS REFERENCE STANDARD A380 FIGURE 57-21-10-991-003-A. MATERIAL: 7175 OR EQUIVALENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57203001000 | AIRBUS REFERENCE STANDARD A380 FIGURE 57-21-10-991-009-A. MATERIAL: 7175 OR EQUIVALENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57203002000 | AIRBIS REFERENCE STANDARD A380-800, 57-21-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57203003000 | AIRBUS A380 REFERENCE STANDARD FIGURE 57-21-02-991-003-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57203005000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.57-11-03-991-008-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L57203006000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.57-11-03-991-014-A. Includes Test Report and Certificate of Conformance. | . | . | |||
99L57203006000 | AIRBUS REFERENCE STANDARD A380-800 7075 ALUMINUM; FIG.57-21-10-991-016-A. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57203009000 | AIRBUS A380 REFERENCE BLOCK ISB-8263 57-21-18 FIGURE 005. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57204005000 | AIRBUS A300-600, A319,A320, A321, A330, A340, A380 REFERENCE STANDARD FIGURE:57-26-01-991-003-A. MATERIA L: 7010-T7651 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | |||
99L57204008000 | AIRBUS A310 CALIBRATION SENSITIVITY BLOCK PART4 57-29-01 PAGE 418 FIGURE 408. Includes Test Report and certificate of Conformance. | . | . | . | . | |
99L57204059000 | AIRBUS A380 ISB-8263 FAMILIIARIZATION BLOCK FIGURE 007 SHEET 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99l57204062000 | AIRBUS A380 REFERENCE BLOCK ISB-8263 57-21-18 FIGURE 006. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57204066000 | AIRBUS A380 GUIDE RING 53-21-17 FIGURE 011. MATERIAL: BLACK ACETAL. Includes Certificate of Conformance. | . | . | . | . | |
99L57204067000 | AIRBUS SEARCH UNIT GUIDE A380-800 57-21-17-991-025-A. MATERIAL: DELRIN. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57204068000 | AIRBUS CALIBRATION BLOCK A380-800 57-21-17-991-024-A. MATERIAL: 2024 HDT T351. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57204069000 | AIRBUS SEARCH UNIT GUIDE A380-800 57-21-17-991-026-A. MATERIAL: DELRIN. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99L57603000000 | AIRBUS REFERENCE STANDARD A330-200F 57-61-21-991-006-A PAGE 1. . lncludes Certificate of Conformance. | . | . | . | . | |
99N28207315000 | AIRBUS REFERENCE STANDARD A318-A321 28-28-03-PB6. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99N51107332000 | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT BLOCK SET. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99N51107332000-A | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99N51107332000-B | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99N51107332000-C | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99PNF54503009000 | AIRBUS REFERENCE STANDARD A330 54-51-40-991-014-A FASTENER (NSA5415-36). lncludes Test Report and Certificate of Conformance. | . | . | . | . | |
99T045-1 | Western Global Airlines LFEC Satcom Antenna Cutout Reference Standard, Appendix 1 (Sheet 1). Material: 2024-T3 Clad Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99V52307336000 | AIRBUS REFERENCE STANDARD A380 52-31-01 FIGURE 5-52-31-01-005-A.MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
99V57200003000 | AIRBUS CALIBRATION BLOCK A330 NTM 54-54-18. MATERIAL: TA6v BETA TITANIUM...Includes Test Report and Certificate of Confromance. | . | . | . | . | |
9RS1 | DC-9 REFERENCE STANDARD FASTENER (NAS1097AD6) | . | . | . | . | |
9RS11 | 717-200 REFERENCE STANDARD...FIG. 1.3 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
9RS13 | MD-80 REFERENCE STANDARD...FIG.9 SHEETS 1-5, MD-80 SID SECTION 2-1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
9RS17 | MD-80 REFERENCE STANDARD 2-1 FIG 26 | . | . | . | . | |
9RS5 | DC-9 REFERENCE STANDARD PAGES 17-20, SHEETS 1-4. MATERIAL: 2024-T3 CLAD ALUMINUM | . | . | . | . | |
9RST1 | 717-200 REFERENCE STANDARD...FIG. 1.11 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 2024-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.FASTENER (MS20470AD8, NAS1478-6 + NAS1080-8) | . | . | . | . | |
9RST8 | 717-200 REFERENCE STANDARD FIGURE 1.10 SHEETS (1-6 ), PAGES 1-6. MATERIAL: 2024-T3 ALUMINUM and PHENOLIC(DMS1558). Includes Test Report and Certificate of Conformance. FASTENER (NAS1203 + NAS1252-10H + NAS679-A3, S432867-8 + NAS1080-8) | . | . | . | . | |
A266 | BOEING REFERENCE STANDARD 727 PT 6 57-50-27 | . | . | . | . | |
A27288 | BOEING REFERENCE STANDARD DC9-27A307 | . | . | . | . | |
A306 | BOEING REFERENCE STANDARD 737 PART 6 57-10-07 FIGURE 1 PAGE 4. | . | . | . | . | |
A320 51-10-04 | Airbus A318/A319/A320/A321 51-10-04 Page 402 Figure 401, Measurement of Remaining Thickness in Large Blended Out Areas-Procedure A. Material: 6Al-4v Titanium. Steps: 0.5mm, 1mm, 2mm, 3mm, 4mm, 5mm +/-.05mm(.002"). Step Pad Size: 20mm(.787") x 20mm(.7... | . | . | . | .. | |
A352 | BOEING REFERENCE STANDARD 737 PART 6 53-10-04 PAGE 4 FIGURE 1. 2024-T3 CLAD ALUMINUM OR 7075-T6 BARE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
A376 | BOEING REFERENCE STANDARD 737 PT 6 53-10-45 | . | . | . | . | |
A386 | BOEING REFERENCE STANDARD 737 PT 6 53-10-45 | . | . | . | . | |
A389A | BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. | BACR15BB6B* | . | . | ||
A389B | BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. | BACR15BB6B* | . | . | ||
A389C | BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. | BACR15BB6B* | . | . | ||
A607 | BOEING REFERENCE STANDARD 767 PT 6 53-80-02 | . | . | . | . | |
A607A | BOEING REFERENCE STANDARD 767 PT6 53-80-02 | . | . | . | . | |
ACR53-172942 | CALIBRATED CONDUCTIVITY REFERENCE STAND SET. 17%,29%, 42% IACS NOMINAL VALUES | . | . | |||
ACRS3-172942 | CALIBRATED CONDUCTIVVITY REFERENCE STANDARD SET OF 3. KIT CONSISTS OF MAGNESIUM, 6061-T6 AL AND 2024-T3 AL ( IACS Nominal values of 17%, 29% and 42% respectively) | . | . | |||
ACWM-E175-IB | Inner Wheel Standard, Embraer..175 90000582: 1. Contains a Total of 3 EDM Flaws in the Bead Seat Area of the Reference Standard. Flaw sizes: 1.52mm Long x 0.76mm Deep x 0.10mm Wide Tolerance= +/- 0.05mm. Includes Test Report and Certificate of Confor... | . | . | . | . | |
ACWM-E175-OB | Outer Wheel Standard, Embraer..175 90000582-1. Contains a Total of 3 EDM Flaws in the Bead Seat Area of the Reference Standard. Flaw sizes: 1.52mm Long x 0.76mm Deep x 0.10mm Wide Tolerance= +/- 0.05mm. Includes Test Report and Certificate of Conform... | . | . | . | . | |
AF125-4801-DEV | Custom Boeing Reference Standard. Material: ST Aeromet 100. Quantity of 1 (A) .030" x .030" and 1 (B) .050" x .050" corner EDM notch. Reference standard must be fabricated using round bar since Aeromet 100 is only commercially available in this form.... | . | . | . | . | |
AF-5098RS/.875 | BOEING DC9 REFERENCE STANDARD -57-225 FIG 6 | NEC1002RS | . | . | . | |
AF5-2024-T3-.020-.100 | UT 5 STEP WEDGE .020", .040", .060", .080", .100. MATERIAL: 2024-T3 ALUMINUM | . | . | |||
AF-5271 | CUSTOM FLEX SHAFT PROBE, 9.8mmØ(.386") 500KHz, 12.20"(310mm) LONG SUPPLIED WITH A 4 PIN FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. Reference: Airbus A300-600 Part 6 57-10-35 page 606 Figure 604 | . | . | . | . | |
AF5-7075-T6-.020-.100 | UT 5 STEP WEDGE .020", .040", .060", .080", .100. MATERIAL: 7075-T6 ALUMINUM | . | . | . | . | |
AFHS20-2A-5 | Aluminum Multi-hole reference standard with certificate. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains two EDM corner... | U8862079 | MHS-20-2A-5 | . | . | |
AFL-1070AT | 70° ALUMINUM, ANGLE BEAM TRANSDUCER 10MHZ .375"x.375" ELEMENT, CASE SIZE( 1.030L X .500W X .625H )TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFM-570AT-2 | 70° in ALUMINUM MINIATURE ANGLE BEAM TRANSDUCER , 5MHz, .25" x .25" ELEMENT, CASE SIZE: .750"(19.05mm) L x .330" W(8.4mm) x .500"(12.7mm) H SUPPLIED WITH A TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance. | . | ||||
AFNDT-001/.08 | 2024-T351 ALUMINUM THICKNESS BLOCK 3.0" x 3.0" x .080" | . | . | . | . | |
AFNDT-001/.25 | 2024-T351 ALUMINUM THICKNESS BLOCK 3.0" x 3.0" x .250" | . | . | . | . | |
AFNDT-0212-1 | EDDY CURRENT SURFACE REFERENCE BLOCK. 2 EDM NOTCHES ( .012"D, .020"D, x .005" W +/- .001"), INCONEL 718. SIZE: 1.0"W x 3.0"L x .25" | RS0212-1 | . | . | . | |
AFNDT-032/10MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-0512A | Eddy Current Hole and Surface Crack Standard: 7075-T651 Aluminum. | TEK-6812A | VM89A-14-1 | . | . | |
AFNDT-0512A. | Eddy Current Surface Crack Standard. EDM Notch Size: Total of 3 Notches, 0.005, 0.010, 0.020 Deep x .005W +/- .002 per 33B-1-2 WP 402 00. Includes Certification Report. | SRS-0512A | . | . | . | |
AFNDT-0512T | Eddy Current Hole and Surface Crack Standard: 6AL-4v Titanium. | TEK-6812T | VM89T-14-1 | . | . | |
AFNDT-1000/4340 | 12 HOLE REFERENCE STANDARD 4340 STEEL WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH | RM120-C30C20-4340 | . | . | . | |
AFNDT-1000/SA | 12 HOLE REFERENCE STANDARD ALUMINUM WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH | RM120-C30C20-2024T3 | . | |||
AFNDT-1000SA-1 | 12 HOLE REFERENCE STANDARD ALUMINUM WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH | . | . | |||
AFNDT-1000SS | 12 HOLE REFERENCE STANDARD STAINLESS STEEL WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH | . | . | |||
AFNDT-1000TI | 12 HOLE REFERENCE STANDARD 6AL4V WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH | RM120-C30C20-T6AL4V | . | |||
AFNDT-1002 | CUSTOM 3 HOLE 7075-T6 ALUM. EC REFERENCE STANDARD WITH a .020x.020" CORNER NOTCH IN EACH HOLE. HOLE SIZES 1.063", .687", .625" DIA | . | . | . | . | |
AFNDT-1003/2024-T3 | CUSTOM METRIC STEP WEDGE WITH 7 1.0"x1.0" STEPS MADE OF 2024-T3 ALUMINUM. STEP SIZES ( 1.6mm, 2.4mm, 3.2mm, 4.0mm, 4.8mm, 5.6mm, 6.4mm )..+/- .05mm | . | . | . | . | |
AFNDT-1003/5086 | CUSTOM METRIC STEP WEDGE WITH 7 1.0"x1.0" STEPS MADE OF 5086 ALUMINUM. STEP SIZES ( 1.6mm, 2.4mm, 3.2mm, 4.0mm, 4.8mm, 5.6mm, 6.4mm ) +/- .05mm | . | . | . | . | |
AFNDT-1003/7075-T6 | CUSTOM METRIC STEP WEDGE WITH 7 1.0"x1.0" STEPS MADE OF 7075-T6 ALUMINUM. STEP SIZES ( 1.6mm, 2.4mm, 3.2mm, 4.0mm, 4.8mm, 5.6mm, 6.4mm )..+/- .05mm | . | . | . | . | |
AFNDT-1004CS | ARMY STRIKER THICKNESS BLOCK 3.0"L x 1.0"W x 7.31mm. THICK. MATERIAL: 4130 CARBON STEEL | . | . | . | . | |
AFNDT-1005 | 14 HOLE ROTARY STANDARD 6AL4V 5/32, 7/32, 11/32, 3/16, 5/16, 13/64, 15/64, 17/64, 19/64, 21/64, 1/4, 3/8, 1/2, 28 EDM NOTCHES .050 TOP, .030 CORNER BOTTEM | . | . | |||
AFNDT-1006AL | CUSTOM 3 STEP CALIBRATION BLOCK 2024-T3 ALUMINUM, STEP SIZES 1.0" x 2.0" FACE. STEP THICKNESSES OF 0.100", 0.200" and 0.400" +/-.002" | . | . | . | . | |
AFNDT-1006CS | CUSTOM 3 STEP CALIBRATION BLOCK 4340 CARBON STEEL, STEP SIZES 1.0" x 2.0" FACE. STEP THICKNESSES OF 0.100", 0.200" and 0.400" +/-.002" PER DC-10 54-10-11 FIGURE 603 SHEET 43 PAGE 655 | . | . | . | . | |
AFNDT-1010-177SS | BOEING TOOL ST8809C LETTER CODE D 17-7 PH ANNEALED STAINLESS STEEL | . | . | |||
AFNDT-1010A | BOEING TOOL ST8809C LETTER CODE B 2024-T3 ALUMINUM | . | . | |||
AFNDT-1010-ALNIBR | BOEING TOOL ST8809C LETTER CODE F Al-NI-BR | . | . | . | . | |
AFNDT-1010S | BOEING TOOL ST8809C LETTER CODE E 4340 STEEL | . | . | |||
AFNDT-1010SA | BOEING TOOL ST8809C LETTER CODE A 7075-T73 ALUMINUM | . | . | |||
AFNDT-1010TI | BOEING TOOL ST8809C LETTER CODE C 6AL-4V TITANIUM | . | . | |||
AFNDT-1012 | Bombardier / Challenger 300 Custom UT Thickness Reference Standard Figure 2 Part 1 Section 4 page 11. Material: 2024-T351 Clad. Standard machine milling, no Chemical mill. Step Tolerance: +/-.002" | . | . | . | . | |
AFNDT-1015 | EDDY CURRENT CALIBRATION BLOCK 2024-T351, WITH .020"Lx.005"W COUNTERSINK SURFACE EDM NOTCH IN EACH HOLE.0.190-0.194, countersink: 100 degrees, 0.3748-0.3819 diameter....0.203-0.207, countersink: 100 degrees, 0.3748-0.3819 diameter....0.2172-0.2182, co... | . | . | . | . | |
AFNDT-1015/2024 | CUSTOM 4 STEP CALIBRATION BLOCK 2024-T3 ALUMINUM, STEP SIZES .75"x.75" FACE WITH STEP THICKNESSES OF .040",.060",.080",.100" +/-.001" | . | . | .. | . | |
AFNDT-1015-CALCS | CALIBRATION BLOCK 4140S | . | . | |||
AFNDT-1015-CALSS | CALIBRATION BLOCK 304SS | . | . | |||
AFNDT-1015-CS/MM | CUSTOM 4 STEP CALIBRATION BLOCKS CARBON STEEL , 54MM, 10MM, 15MM, 20MM | . | . | . | . | |
AFNDT-1015-INC625 | CALIBRATION STANDARD INCOLNEL BLOCK 625 5X1 OAL .10,.20,.30,.40,.50 | . | . | |||
AFNDT-1015-SS/MM | CUSTOM 4 STEP CALIBRATION BLOCKS STAINLESS STEEL , 54MM, 10MM, 15MM, 20MM | . | . | . | . | |
AFNDT1016-12S-2024 | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .625", .688" Ø MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
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AFNDT1016-12S-7075 | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .625", .688" Ø MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | |||
AFNDT-1017AL | Custom Eddy Current Hole Standard 7075-T7 Aluminum ( Equivalent substitute for 7010 Aluminum). Hole Sizes 1.77" and 0.58" diameter. EDM flaw size: 0.5mm(.020") x 0.1mm (0.004") +/- .002" | . | . | . | . | |
AFNDT-1025AL | Multi-Hole reference standard. Material: 7075-T6 Aluminum. 12 Holes 3/16", 7/32", 1/4" ,9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4" .020" x .020" x .005" Wide ± .002" Through EDM Notches in each hole. Standard also includes 3 surface EDM notches .008", .020" and .040" Deep x .005" wide ± .002". Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-1025TI | Multi-Hole reference standard. Material: 6Al-4v Titanium. 12 Holes 3/16", 7/32", 1/4" ,9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4" .020" x .020" x .005" Wide ± .002" Through EDM Notches in each hole. Standard also includes 3 surface EDM notches .008", .020" and .040" Deep x .005" wide ± .002". Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-1030 | CUSTOM BRILE RIVET/ 100 DEGREE COUNTERSINK MULTI HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. BRILE HOLE SIZES: 5/32", 3/16" and 1/4". 100 DEGREE COUNTERSINK HOLE SIZES: 5/32", 3/16", 1/4", 5/16", 3/8". .030"X.030" CORNER / COUNTERSINK EDM NOTCHES. DIM... | . | . | |||
AFNDT-1030/10MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1030/12MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 12mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1030/6MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 6mm diameter hole. Midwall EDM notch( 9.5mm long +/- 0.95 )x ( 0.13mm deep +/- 0.01 ) x ( 0.18mm MAX width ) | . | . | |||
AFNDT-1031/12MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 12mm diameter hole. Midwall EDM notch( 1.5mm long +/- 0.15 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1031/8MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 8mm diameter hole. Midwall EDM notch( 1.5mm long +/- 0.15 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1032/10MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 10mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1032/12MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 12mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1032/6MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 6mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1032/8MM | CUSTOM EDDY CURRENT CALIBRATION BLOCK 4130 or 4340 STEEL. 50mm x 50mm x 15mm with 8mm diameter hole. Corner EDM notch( 0.76mm long +/- 0.07 )x ( 0.76mm deep +/- 0.07 ) x ( 0.18mm MAX width ) | . | . | . | . | |
AFNDT-1035/7075 | 5 hole reference standard sizes; 1/4", 5/16", 3/8", 7/16" and1/2" inch diameters.( .030" X .030" x .005" +/-.001" corner EDM notch. 7075-T6 Aluminum | . | . | . | ||
AFNDT-1035TI | REFERENCE STANDARD 7/16" THICK 6AL-4V | . | . | |||
AFNDT-1040 | THREE HOLE CALIBRATION STANDARD | . | . | |||
AFNDT-1045 | 5 STEP ACRYLIC WEDGE. STEP SIZES: .250", .500",. 750", 1.00", 1.250" MATERIAL: CAST ACRYLIC. PAD SIZE: 1.0" x 1.0" TOLEREANCE = +/- .002". Includes Certification and Certificate of Conformance. | . | . | |||
AFNDT-1046 | STEP ACRYLIC WEDGE. STEP SIZES: 0.1", 0.3", 0.5", 0.7", 0.9", 1.1" MATERIAL: CAST ACRYLIC. PAD SIZE: 1.0" x 1.0" TOLEREANCE = +/- .002". Includes Certification and Certificate of Conformance. | . | . | . | . | |
AFNDT-1060 | NON-PIPING CALIBRATION BLOCK, 3/4 X 6 1/4 X 12 | . | . | |||
AFNDT-1061AL | EDDY CURRENT SURFACE BLOCK 7075-T6. 2 EDM SLOTS ( 0.2mm deep +/-0.05 & 0.12mm wide +/- 0.01),( 0.5mm deep +/- 0.01. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-1061CS | EDDY CURRENT SURFACE BLOCK, 4130/4140 STEEL. 2 EDM SLOTS ( 0.2mm deep +/-0.05 & 0.12mm wide +/- 0.01),( 0.5mm deep +/- 0.01. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-1062 | NON-PIPING CALIBRATION BLOCK FIGURE T-434.2.1 ASME SECTION V Article IV, 3" X 6 1/4" X 12". MATERIAL: 1018 CARBON STEEL. Includes Test Report and Certificate of Conformance. | . | . | |||
AFNDT-1071/2024 | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 2024 Aluminum. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-1071/301 | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 301 Stainless Steel. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-1071/4340 | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 4340 CRES Steel. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-1071/7075 | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 7075 Aluminum. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-1071/INC | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 718 Inconel. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-1071/TI | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 0.6mm, 0.7mm, 0.8mm, 0.9mm and 1.0mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm X 19mm, (Tolerance: +/- 0.5mm) Material: 6AL-4V Titanium. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-1074/713 | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 713 Inconel. Includes Certification Report for step thickness and COC of material used... | . | . | . | . | |
AFNDT-1074/718 | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 718 Inconel. Includes Certification Report for step thickness and COC of material used... | . | . | . | . | |
AFNDT-1074/TI | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 6AL-4V Titanium. Includes Certification Report for step thickness and COC of material ... | . | . | . | . | |
AFNDT-1074-3 | EDDY CURRENT SURFACE BLOCK MADE OF 6AL-4V TITANIUM WITH 3 SURFACE NOTCHES ACROSS THE WIDTH OF THE BLOCK. .1mm X .005" MAX WIDTH and .2mm X .005" MAX WIDTH, .5MM X.005" MAX WIDTH | . | . | . | . | |
AFNDT-1074AL | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1mm, 3mm, 5mm, 7mm, 9mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 7075-T6 Aluminum. Includes Certification Report for step thickness and COC of material... | . | . | . | . | |
AFNDT-1075AL | ULTRASONIC TEST BLOCK .100/.500 ALUMINUM | . | . | |||
AFNDT-1075ST | ULTRASONIC TEST BLOCK .100/.500 STEEL | . | . | |||
AFNDT-1075TI | ULTRASONIC TEST BLOCK .100/.500 TITANIUM | . | . | |||
AFNDT-1076AL | ULTRASONIC STEP BLOCK .020", .050", .075", .100", .125" 7075-T6 ALUMINUM | . | . | |||
AFNDT-1076ST | ULTRASONIC STEP BLOCK .020", .050", .075", .100", .125" 4340 STEEL | . | . | |||
AFNDT-1076TI | ULTRASONIC STEP BLOCK .020", .050", .075", .100", .125" 6AL-4V TITANIUM | . | . | |||
AFNDT-1080/4340 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES 0.5mm, 1.0mm, 2.0mm, 3.00mm, 4.0mm, 5.0mm (.004"W +/- .002, MAX.006), 4340 STEEL 1.0"W x 7.0"L | . | . | |||
AFNDT-1080-2/840 | CUSTOM REFERENCE STANDARD PER SPECS | . | . | |||
AFNDT-1085 | CUSTOM MULTI-HOLE REFERECNE STANDARD, 2024-T3 WITH .030X.030 CORNER NOTCH, .020X.020 CORNER NOTCH, HOLE SIZE 5/32,11/64,3/16,13/64,9/32,17/64,1/4,7/32 | . | . | |||
AFNDT-1090AL | 5 STEP WEDGE .050", .100", .150", .200", .250". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | |||
AFNDT-1090SS | 5 STEP WEDGE .050", .100", .150", .200", .250". TOLERANCE +/-.001". MATERIAL: 304 STAINLESS STEEL .PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. .. | . | . | |||
AFNDT-1090TI | 5 STEP WEDGE .050", .100", .150", .200", .250". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM .PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-1095 | 8 STEP THIN WEDGE, STEP SIZES OF .030", 0.040",.050", .060", .070", .080", .090", and .100" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | UT-RC-8-TS-AL | . | |||
AFNDT-1096 15-5PH | 10 STEP REFERENCE BLOCK .025,.030,.040,.050,.063,.071,.080,.090,.100,.125 15-5PH | . | . | . | . | |
AFNDT-1096/2024T3 | 10 STEP REFERENCE BLOCK .025,.030,.040,.050,.063,.071,.080,.090,100,.125 2024-T3 | . | . | . | . | |
AFNDT-1096/304SS | 9 STEP REFERENCE BLOCK WITH ACETAL HOLDER. MATERIAL: 304 STAINLESS STEEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | |||
AFNDT-1096/304SS | 9 STEP REFERENCE BLOCK WITH ACETAL(DELRIN) HOLDING BLOCK. MATERIAL: 304 STAINLESS STEEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-1096/6061AL | 9 STEP REFERENCE BLOCK WITH HOLDER. MATERIAL: 6061 ALUMINUM. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-1096/625 | 9 STEP REFERENCE BLOCK WITH ACETAL(DELRIN) HOLDING BLOCK. MATERIAL: 625 INCONEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-1096/6AL4V | 10 STEP REFERENCE BLOCK,.030,.040,.050,.063,.071,.080,.090,100,.120 6AL4V | . | . | . | . | |
AFNDT-1096/718 | 9 STEP REFERENCE BLOCK WITH ACETAL(DELRIN) HOLDING BLOCK. MATERIAL: 625 INCONEL. STEP SIZES: .020",.050",.080", .120", .160" , .200", .300", .500", .750" +/-.010". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-1098AL | 12 HOLE REFERENCE STANDARD 2024-T3 .156, .187, .199 ,.218, .250, .281, .312, .343, .375, .406, .437, .500, .030X.030 CORNER NOTCH, .050X.050 CORNER NOTCH ( 24 EDM NOTCHES TOTAL) | . | . | . | . | |
AFNDT-1098St | 12 HOLE REFERENCE STANDARD 4340 STEEL. HOLE SIZES: .156, .187, .199 ,.218, .250, .281, .312, .343, .375, .406, .437, .500, .030X.030 CORNER NOTCH, .050X.050 CORNER NOTCH (24 EDM NOTCHES TOTAL) | . | . | . | . | |
AFNDT-1098TI | 12 HOLE REFERENCE STANDARD 6AL4V .156, .187, .199 ,.218, .250, .281, .312, .343, .375, .406, .437, .500, .030X.030 CORNER NOTCH, .050X.050 CORNER NOTCH (24 EDM NOTCHES TOTAL) | . | . | |||
AFNDT-186A-F | CUSTOM STANDARD COMBINING 186A-F INTO ONE STANDARD | . | . | |||
AFNDT-2001-909 | CUSTOM STEP WEDGE INC909, 1"X6" W/ 1" STEPS .025 -.150 IN .25 INCREMENTS | . | . | . | . | |
AFNDT-2002AL | CALIBRATION STANDARD THREE HOLES, 1.0,1.25,1.5, CORNER NOTCH .030X.030 | . | . | . | . | |
AFNDT-2003-1AL | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 7075-T6 ALUMINUM | MHS-12-1A-0 | . | . | . | |
AFNDT-2003-1S | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 4340 STEEL | MHS-12-1S-0 | . | . | . | |
AFNDT-2003-1S-1 | 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. .020 Thru EDM notches .005"(+/- .001") and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 4340 Steel. Includes Test Report and Certificate... | MHS-12-1S-1 | . | . | . | |
AFNDT-2003-2S | 12 HOLE REFERENCE STANDARD 1018 STEEL HOLE SIZES: .187", .250" ,.312", .375", .437", .500", .562", .625", .687", .750", AND 1.0" ( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) 304 STAINLESS STEEL | . | . | . | . | |
AFNDT-2004 | EDDY CURRENT SURFACE STANDARD WITH 3 EDM NOTCHES: ( .005", .010", .020" Deep x .004"Wide +/- .002 ), MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2005A | 12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001" | . | . | . | . | |
AFNDT-2005CS | 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters, .030X.030 Corner EDM Notches .005"(+/- .001") wide, .020" full bore thru EDM notches .005"(+/- .001") deep and 3 SURFACE NOTCHES .010", .020", .040" D... | . | . | . | . | |
AFNDT-2005TI | 12 HOLE REFERENCE STANDARD 6AL-4v TITANIUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001" | . | . | . | . | |
AFNDT-2006/13-8 | 12 HOLE REFERENCE STANDARD 13-8 PH STAINLESS STEEL (3/16, 7/32 ,1/4, 9/32, 5/16,11/32, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4), .030X.030 | VM89SS-PH13-8 | . | . | . | |
AFNDT-2006/17-4 | 12 HOLE REFERENCE STANDARD 17-4PH (3/16, 7/32 ,1/4, 9/32, 5/16,11/32, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4), .030X.030 | VM89SS | VM89SS | . | ||
AFNDT-2006/300M | 12 HOLE REFERENCE STANDARD 300M STEEL.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040" DEEP .005" ... | VM89S/300M | . | . | . | |
AFNDT-2006A | 12 HOLE REFERENCE STANDARD 7075-T6 aluminum. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.004" ±.002" WIDE CORNER EDM NOTCH in EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020",... | VM89A | SH-7075-12' | VM89A | . | |
AFNDT-2006S | 12 HOLE REFERENCE STANDARD 4130 or 4340 STEEL.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040" DEE... | VM89S | VM89S | . | ||
AFNDT-2006SS | 12 HOLE REFERENCE STANDARD 304 304 STAINLESS STEEL.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040... | VM89SS | VM89SS | . | ||
AFNDT-2006TI | 12 HOLE REFERENCE STANDARD 6AL-4V.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.005"WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020", .040" DEEP .005" WIDE... | VM89T | . | . | . | |
AFNDT-2007AL | CUSTOM 4 STEP WEDGE. MATERIAL: 7075-T6 ALUMINUM. STEP SIZES: .020",.040",.060",.090" +/-.001. PAD SIZE: .75" x .75". Includes Test Report Traceable to NIST. | . | . | . | . | |
AFNDT-2007AL-1 | CUSTOM 4 STEP WEDGE. MATERIAL: 2024-T3 ALUMINUM. STEP SIZES: .020",.040",.060",.090" +/-.001. PAD SIZE: .75" x .75". Includes Test Report Traceable to NIST. | . | . | . | . | |
AFNDT-2008/2024-T6 | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15 ALUMINUM 2024-T6 . | . | . | . | . | |
AFNDT-2008/C | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 CAST ALUMINUM | . | . | . | . | |
AFNDT-2008/F | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15 ALUMINUM 2014-T6 CONDUCTIVITY RANGE 35-40 IACS. | . | . | . | . | |
AFNDT-2008/MAG | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3. MATERIAL: MAGNESIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2009AL | 5 STEP WEDGE, 16mm, 17mm, 18mm, 19mm, 20mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square. Includes Delrin Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2010AL | Custom McDonnell Douglas 15 bolt hole reference standard with a .060"L x .030Dx .005" max width mid-wall notch, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (.156", .172", .188", .203", .250", .266", .281", .297", .313", .328"... | . | . | . | . | |
AFNDT-2011/4130 | 10 STEP CARBON STEEL WEDGE. STEP THICKNESS OF , .019", .028", .050", .096", .148", .202", .253", .301", .350" .400" +/-.001". 1.0" x 1.0" Step Pad Face. Material: 4130 Carbon Steel. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-2011/7075 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .019", .028", .050", .096", .148", .202", .253", .301", .350" .400" +/-.001". 1.0" x 1.0" Step Pad Face. Material: 7075-T651 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-2013AL | 12 HOLE REFERENCE STANDARD 7075-T6 (3/16" x 2), 13/64", 7/32", 15/64" ,(1/4" x 2 ), 17/64",9/32", 19/64",5/16", 21/64" .020"x.020" and .030"x.030" x .005"W +/-.002" CORNER EDM NOTCH PER BOEING SPECIFICATION 747 PART 6 51-00-00 PAGE 8 FIGURE 3 | NDT1084 | . | . | ||
AFNDT-2014 | CUSTOM EC STANDARD, NOTCH .060X.030X.005 TOL PER BSS7048, 304SS | . | . | . | . | |
AFNDT-2014Ti | 12 HOLE REFERENCE STANDARD IN 6AL-4v Ti; HOLE SIZES: (3/16, 7/32 ,1/4, 9/32, 5/16,11/32, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4), .010", .020", .030", and .040" SURFACE NOTCHES. .050"x.050" CORNER EDM NOTCH and .030"x.030" CORNEREDM NOTCH, .050"Lx.030"D MID-... | . | . | . | . | |
AFNDT-2015 | CUSTOM SURFACE WAVE STANDARD, 6AL-4V | . | . | . | . | |
AFNDT-2017-INC718 | BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-70-001. ALSO IN 53-10-01 PART 6 PAGE 5 FIGURE 1. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL: 718 INCONEL. SIZE: 1.5"W x 3.75"L x .25" | C SERIES | . | . | . | |
AFNDT-2030/13-8 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 13-8PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | .A6211:H6211 | . | |
AFNDT-2030/13-8PH | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 13-8PH MO STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/15-5PH | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 15-5PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | GSE 449 | . | . | . | |
AFNDT-2030/17-4 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 17-4PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/17-7PH | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 17-7PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/2014-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2014-T6 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/2024 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T3 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | RS0824-2024T3 | . | . | . | |
AFNDT-2030/2024-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T6 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/300M | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), MATERIAL: 300M STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/301 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX.006), CRES 301 1/2 HARD(MIL-S-5059) 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/304 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 304 STAINLESS STEEL 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | VMSS3RS-1.0 | . | . | . | |
AFNDT-2030/304L | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 304L STAINLESS STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | RS0824-304L | . | . | . | |
AFNDT-2030/316SS | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 316 STAINLESS STEEL 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
AFNDT-2030/4130 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 4130 STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/4340 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 4340 STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | RS0824-4340 | . | . | . | |
AFNDT-2030/7075-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | GSE 206 | . | . | . | |
AFNDT-2030/7075-T7 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 7075-T7 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/718 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 718 INCONNEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
AFNDT-2030/I600 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 600 SERIES INCONNEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | RS0824-I600 | . | . | . | |
AFNDT-2030/MAG | Surface reference standard, Magnesium, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | . | . | . | . | |
AFNDT-2030/MAR | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008"(0.2mm), .020"(0.5mm), .040"(1.0mm) (.004"W +/- .002). MATERIAL: 250 MARAGING STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2030/TI | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX .006"), 6AL-4v TITANIUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and COC | GSE 450 | U8860550 | RS0824-6AL4V | . | |
AFNDT-2030CS | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX.006), 4130 or 4340 STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 82040CS | . | . | ||
AFNDT-2030INC | EDDY CURRENT SURFACE REFERENCE BLOCK, EDM NOTCHES ( .008", .020", .040" x .004" W +/- .002"), INCONEL 718. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2031/4340 | 7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 4340 CRES STEEL. STEP RANGE:.040", .080", .160", .250", .300", .400", .500". +/-.001". Includes certification report traceable to NIST... | . | . | . | . | |
AFNDT-2031/6AL-4V | 7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 6AL-4V TITANIUM. STEP RANGE:.040", .080", .160", .250", .300", .400", .500" +/- .001". Includes certification report traceable to NIST... | . | . | . | . | |
AFNDT-2031/7075 | 7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 7075-T6 ALUMINUM. STEP RANGE:.040", .080", .160", .250", .300", .400", .500" +/- .001". Includes certification report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2032/Al | 5 STEP REFERENCE BLOCK ..STEP SIZES 1.0" X 1.0" 7075-T6 ALUMINUM. (400",.450",.500",.550",.600") | . | . | . | . | |
AFNDT-2032/SS | 5 STEP REFERENCE BLOCK ..STEP SIZES 1.0" X 1.0" 304 STAINLESS.(400",.450",.500",.550",.600").. | . | . | . | . | |
AFNDT-2032/Ti | 5 STEP REFERENCE BLOCK ..STEP SIZES 1.0" X 1.0" 6AL-4V Ti.(400",.450",.500",.550",.600") | . | . | . | . | |
AFNDT-2035 | 6 Hole reference standard (Aluminum 7075-T6 with certifications). Hole Sizes: 1.0", 1.125", 1.250" ,1.500", 1.625", 1.750", ( .030 x .030 x .006 +/- .001) Corner EDM Notches and .010, .020, .040 Surface notches). | . | . | . | . | |
AFNDT-2037/7075T6 | 10 STEP WEDGE SUPPLIED WITH HOLDING BLOCK. STEP SIZES: .040", .080", .120", .160", .200", .240", .280", .320", .360", .400" +/-.001". Material: 7075-T6 ALUMINUM. PAD SIZE: .75" x .75". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2038AL | EDDY CURRENT CALIBRATION BLOCK 2024-T351, WITH .020"Lx.005"W COUNTERSINK SURFACE EDM NOTCH IN EACH HOLE. HOLE SIZES: .156"Ø and .187"Ø. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2040/.063-.140 | CUSTOM TEST BLOCK +/-.0004 TOL | . | . | . | . | |
AFNDT-2040/.100-.600 | CUSTOM TEST BLOCK +/-.0004 TOL | . | . | . | . | |
AFNDT-2040AL | 4 STEP WEDGE. Material: 2024-T351 Aluminum. Step Sizes: 0.5mm, 1.0mm, 1.5mm, 2.0mm, +/-0.05mm Pad Size: 19mm x 19mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2041/2024-T3 | 5 STEP WEDGE 2024-T351, Step Sizes: 0.5mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, +/-0.05mm Pad Size: 25mm x 25mm | . | . | . | . | |
AFNDT-2041/AL | 5 STEP WEDGE 7075-T6 ALUMINUM:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.**..(0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm) INCLUDED WITH CERTIFICATION REPORT | . | . | . | . | |
AFNDT-2041/AL-1 | 5 STEP WEDGE 2024-T3 ALUMINUM:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.** (0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm). IncludesTest Report Traceable to NIST and Certificate of Conformance. |
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AFNDT-2041/ST | 5 STEP WEDGE 4340 steel:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.**..(0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm) INCLUDED WITH CERTIFICATION REPORTS | . | . | . | . | |
AFNDT-2041/TI | 5 STEP WEDGE 6al-4v TITANIUM:(.030",.060",.125",.250",.250, .375" +/-.001 Note**with additional engraving marks of metric conversions on each step.**..(0.762mm, 1.524mm, 3.175mm, 6.350mm, 9.525mm) INCLUDED WITH CERTIFICATION REPORTS | . | . | . | . | |
AFNDT-2042/AL | CUSTOM 5 HOLE REFERENCE STANDARD MADE OF 7075-T6 ALUMINUM WITH (0.5mm X 0.5mm +/- .05mm) CORNER EDM FLAWS. HOLE SIZE : 13/64", 19/64", 23/64", 7/16" & 31/64" | . | . | . | . | |
AFNDT-2043/718 | AIR FORCE GENERAL PURPOSE REFERENCE STANDARD INCONEL 718 ,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. Manufactured per IAW U.S.A.F. Tech Order 33B-1-1 AIR FORCE P/N:(7947479-10). 6635-01-512-4953 | VM30889-C1 | 6635-01-512-4953 | . | . | |
AFNDT-2043/A | AIR FORCE GENERAL PURPOSE REFERENCE STANDARD 7075-T6,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. AIR FORCE P/N:(7947479-10) NSN: 6635-01-092-5129. Includes Certification Report Traceable to NIST and Certificate of conformance. | VM30889-C1A | 6635-01-092-5129 | VM30889-C1A/AF | . | |
AFNDT-2043/S | AIR FORCE GENERAL PURPOSE REFERENCE STANDARD 4340 STEEL ,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. AIR FORCE P/N:(7947479-10)..6635-01-512-4952 | VM30889-C1S | 6635-01-512-4952 | . | . | |
AFNDT-2043/SS | AIR FORCE GENERAL PURPOSE REFERENCE STANDARD 304 STAINLESS STEEL ,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. AIR FORCE P/N:(7947479-10)...6635-01-548-6659 | VM30889-C1SS | 30889-C1SS | 6635-01-548-6659 | . | |
AFNDT-2043/TI | AIR FORCE GENERAL PURPOSE REFERENCE STANDARD 6AL-4V TITANIUM ,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. Manufactured per IAW U.S.A.F. Tech Order 33B-1-1 AIR FORCE P/N:(7947479-10). 6635-01-390-1768 | VM30889-C1T | 6635-01-390-1708 | . | . | |
AFNDT-2044/15-5 | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | 7947479-10 | . | . | . | |
AFNDT-2044/304 | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | 7947479-10 | . | . | . | |
AFNDT-2044/718 | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004" for all notches. Material: 718 Inconel, QQ-A-250/12. Finished standard is anodized per MIL-A-8625, Type II, Class I. Standard can also be made out of other alloys. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49. P/N 7947479-10. Includes Certification Report Traceable to NIST. | 7947479-10 | . | . | . | |
AFNDT-2044/Ti | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | 7947479-10 | . | . | . | |
AFNDT-2044AL | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | 7947479-10 | 6635-01-092-5129 | VM30889-C1A | 7947479-10, 6635-01-092-5129 | |
AFNDT-2044S | Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4" x 7" x 1.06". Contains twenty (20) fastener holes with diameters from 0.156 to 0.750", two (2) screw holes, and two (2) dowel pins holes. Standard also... | VM30889-C1S | VM30889-C1S | 7947479-10 | . | |
AFNDT-2046/AL | 15 HOLE REFERENCE STANDARD 7075-T6 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 5/8, 15 EDM NOTCHES .030X.030 CORNER TOP | . | . | . | . | |
AFNDT-2046/TI | 15 HOLE REFERENCE STANDARD 6AL4V 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 15 EDM NOTCHES .030X.030 CORNER | . | . | . | . | |
AFNDT-2047TI | 4 STEP WEDGE. PAD SIZE 20mm X 20mm. STEP SIZES: 0.6mm, .2mm, 3mm, 4mm +/- .05mm. MATERIAL 6AL-4V | . | . | . | . | |
AFNDT-2048/17-4 | CUSTOM NAVY BLOCK. MATERIAL: 17-4PH STAINLESS STEEL. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3 | . | . | . | |
AFNDT-2048/17-7 | CUSTOM NAVY BLOCK. MATERIAL: 17-7PH STAINLESS STEEL. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3 | . | . | . | |
AFNDT-2048/2024-T3 | CUSTOM NAVY BLOCK. MATERIAL: 2024-T6 ALUMINUM CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3A | . | . | . | |
AFNDT-2048/304 | CUSTOM NAVY BLOCK. MATERIAL: 304 STAINLESS STEEL ,CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3SS | . | . | . | |
AFNDT-2048/400 | CUSTOM NAVY BLOCK. MATERIAL: 400 STAINLESS STEEL. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3 | . | . | . | |
AFNDT-2048/7075T6 | CUSTOM NAVY BLOCK. MATERIAL: 7075-T6 ALUMINUM CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | 74B119151-273 | NRK-3A | OPXV4-74B119151-273 | . | |
AFNDT-2048/718 | CUSTOM NAVY BLOCK. MATERIAL: 718 INCONEL CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3I | . | . | . | |
AFNDT-2048/AMS-6526 | CUSTOM NAVY BLOCK. MATERIAL: PER AMS-6526 NICKEL COBALT STEEL ,CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES NOTCHES. Includes Test Report and Certificate of Conformance. | NRK-3 | . | . | . | |
AFNDT-2048/AST | CUSTOM NAVY BLOCK SET, 3 Blocks Total. Materials: 7075-T6 Aluminum, 4340 Cres Steel and 6AL-4V Titanium. Each Standard Includes 20 Fastener Holes (.156-.750) Containing a total of 71 EDM Notches. Includes Custom fit Waterproof Case. Includes Test Rep... | U8860227, NRK-3AST | NRK-3T | Wespro | . | |
AFNDT-2048/AST/CASE | CUSTOM NAVY BLOCK SET, 3 BLOCKS 7075-T6, 4340, 6AL-4V ,WITH 20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES NOTCHES,( WITH CASE) | U8860227 | NRK-3AST | Wespro | . | |
AFNDT-2048/ST | CUSTOM NAVY BLOCK. MATERIAL: 4340 CRES STEEL CONTAINING 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. | 74B119151-277 | NRK-3ST | U8880206 | OPXV4-74B119151-277 | |
AFNDT-2048/TI | CUSTOM NAVY BLOCK, 6AL-4V TITANIUM ,WITH 20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES NOTCHES | 74B119151-275 | NRK-3T | U8860227 | OPXV4-74B119151-275 | |
AFNDT-2049/4130 | GENERAL PURPOSE EDDY CURRENT REFERENCE STANDARD, 4130, 0.030"X0.030", CORNER EDM NOTCH ON THE TOP SURFACE | . | . | . | . | |
AFNDT-2049/4340 | GENERAL PURPOSE EDDY CURRENT REFERENCE STANDARD, 4340, 0.030"X0.030", CORNER EDM NOTCH ON THE TOP SURFACE | . | . | . | . | |
AFNDT-2049/7075-T6 | GENERAL PURPOSE EDDY CURRENT REFERENCE STANDARD, 7075-T6, 0.030"X0.030", CORNER EDM NOTCH ON THE TOP SURFACE | . | . | . | . | |
AFNDT-2050AL | MINI ANGLE BEAM ALUMINUM V2 Calibration Block, 7075 Aluminum, Metric (Side Drilled Hole Thickness - 12.5mm. Includes Certificate of Conformance and Material Certification Report. Supplied with wood case. | . | . | . | . | |
AFNDT-2052 | LOW FREQUENCY STANDARD, 2024-T3, 4.0X.4.0X.125 & .190 | . | . | |||
AFNDT-2053 | 10 HOLE REFERENCE STANDARD 2024-T3, HOLE SIZES, 1/8, 3/16 ,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, .030" x .030" CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .750"L x .010,.020,.040 DEEP | HRS-10A-0/0824 | ||||
AFNDT-2053CS | 10 HOLE REFERENCE STANDARD 4130 STEEL, HOLE SIZES, 1/8, 3/16 ,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, .030" x .030" CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .750"L x .010,.020,.040 DEEP | . | . | . | . | |
AFNDT-2053TI | 10 HOLE REFERENCE STANDARD 6AL-4V, HOLE SIZES, 1/8, 3/16 ,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, .030" x .030" CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .750"L x .010,.020,.040 DEEP | . | . | . | . | |
AFNDT2054 | 10 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. Hole Sizes: 1/8”, 3/16”, ¼”, 5/16”, 3/8”, 7/16”, ½”, 9/16”, 5/8”. DEPTH: 0.5 +/- 0.05mm (0.020 +/- 0.002in) WIDTH: 0.1 +/- 0.05mm (0.004 +/- 0.002 in. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2054AL | CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. WITH HOLE DIAMETERS: .156",.250",.312",.375",.437",.500". CORNER E... | . | . | |||
AFNDT-2054AL-1 | CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. WITH HOLE DIAMETERS: .156",.250",.312",.375",.437",.500". CORNER E... | . | . | . | . | |
AFNDT-2054AL-2 | CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. WITH HOLE DIAMETERS: .125" .156", .187", .250",.375",.500". CORNER... | . | . | . | . | |
AFNDT-2054CS-1 | CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .156",.250",.312",.375",.437",.500". CORN... | . | . | . | . | |
AFNDT-2054CS-2 | CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .125", .156", .187" ,.250",.375", .500". ... | . | . | . | . | |
AFNDT-2055 | CUSTOM ROTARY BLOCK REFERENCE STANDARD. 10MM, 13MM, 15MM, 17MM , 19MM, .020X.020X.004 +/-.001, ALUMINUM | . | . | |||
AFNDT-2056 | CUSTOM CALIBRATION BLOCK, THREE SURFACE NOTCHES .008" , .020" , .040" SS | . | . | |||
AFNDT-2058/7075T6 | 6 STEP CALIBRATION BLOCK, CUSTOM, .030", .040", 0.60" , 0.80", .100", .150", 7075-T6 Aluminum | NEC-6096-7075 | . | . | . | |
AFNDT-2059/304SS | CUSTOM 8 STEP STANDARD, .080,.071,.063,.056,.050,.040,.030,.020, 304SS | . | . | |||
AFNDT-2059/6AL4V | CUSTOM 8 STEP STANDARD, .080,.071,.063,.056,.050,.040,.030,.020, 6AL4V | . | . | |||
AFNDT-2059/7075-T6 | CUSTOM 8 STEP STANDARD, .080,.071,.063,.056,.050,.040,.030,.020, 7075-T6 | . | . | |||
AFNDT-2060 | CUSTOM REFERENCE STANDARD 7075-T6, NOTCH .010 +/-.001 | . | . | |||
AFNDT-2061 | CUSTOM 6 STEP WEDGE, 6AL-4V .3543, .2755, .1968, .1181, .0393, .0196, 4.744L X .787 W, STEP FACE .787X.787 | . | . | |||
AFNDT-2061/15MM | CUSTOM 6 STEP WEDGE, 6AL-4V , 9MM, 7MM, 5MM, 3MM, 1MM, .0.5MM, STEP FACE 15MMX15MM | . | . | . | . | |
AFNDT-2061/MET | CUSTOM 6 STEP WEDGE, 6AL-4V , 9MM, 7MM, 5MM, 3MM, 1MM, .0.5MM, STEP FACE 20MMX20MM | . | . | |||
AFNDT-2062/MET | CUSTOM 10 STEP WEDGE, 6AL-4V, 20MM, 18MM, 16MM, 14MM, 12MM, 10MM, 8MM, 6MM, 4MM, 2MM, STEP FACE 20MMX20MM | . | . | |||
AFNDT-2062AL | Custom 10 Step Block, 2.0mm, 4.0mm, 6.0mm, 8.0mm, 10.0mm, 12.0mm, 14.0mm, 16.0mm, 18.0mm and 20.0mm, Thickness Tolerance ±.05mm. Pad Size: 19mm X 19mm. Material: 7075-T6 Aluminum. Includes certification Report Traceable to NIST. | . | . | |||
AFNDT-2062CS | Custom 10 Step Block, 2.0mm, 4.0mm, 6.0mm, 8.0mm, 10.0mm, 12.0mm, 14.0mm, 16.0mm, 18.0mm and 20.0mm, Thickness Tolerance ±.05mm. Pad Size: 19mm X 19mm. Material: 1018 Carbon Steel. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-2062SS | Custom 10 Step Block, 2.0mm, 4.0mm, 6.0mm, 8.0mm, 10.0mm, 12.0mm, 14.0mm, 16.0mm, 18.0mm and 20.0mm, Thickness Tolerance ±.05mm. Pad Size: 19mm X 19mm. Material: 304 Stainless Steel. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-2062Ti | Step Block, 2.0mm, 4.0mm, 6.0mm, 8.0mm, 10.0mm, 12.0mm, 14.0mm, 16.0mm, 18.0mm and 20.0mm, Thickness Tolerance ±.02mm. Pad Size: .75” x .75”. Material: 6AL-4v Titanium. Includes Certification Traceable to NIST. | . | . | . | . | |
AFNDT-2063 | 10 HOLE REFERENCE STANDARD 6AL-4V TITANIUM, HOLE SIZES: 1/8, 3/16 , 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, .030X.030 CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .75L X.010,.020,.040 DEEP | . | . | |||
AFNDT-2063AL | 11/16" HOLE STANDARD IN 7075-T6 with .030" x .030" CORNER EDM NOTCH. MATERIAL SIZE 2.0" x 2.0" x .375". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2063S | 10 HOLE REFERENCE STANDARD 4340 STEEL, HOLE SIZES: 1/8, 3/16 , 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, .030X.030 CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .75L X.010,.020,.040 DEEP | . | . | . | . | |
AFNDT-2064 | CUSTOM CALIBRATION PER SPEC | . | . | . | . | |
AFNDT-2064/AL | SAFRAN MESSIER-BUGATTI-DOWTY ET SURFACE REFERENCE STANDARD 32-09-01 FIGURE 67,GRAPHIC-32-09-01-041-008-A01. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of conformance. | . | . | . | . | |
AFNDT-2064/MAG | SAFRAN MESSIER-BUGATTI-DOWTY REFERENCE STANDARD 32-09-01 MAGNESIUM | . | . | . | . | |
AFNDT-2064/TI | SAFRAN MESSIER-BUGATTI-DOWTY REFERENCE STANDARD 32-09-01 6AL-4V TITANIUM | . | . | . | . | |
AFNDT-2065 | Olympus Aluminum multi-hole reference standard. Contains 5 hole sizes; 7/16, 1/2, 9/16, 3/4 and 1.0" inch hole diameters.( .030" x.030" corner EDM notch in each hole) | MHS-5 | . | . | . | |
AFNDT-2066/TI | 12 HOLE REFERENCE STANDARD 6AL-4V TITANIUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .001" WIDE THRU NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001" | RM120-C3T2-6AL4V-T6 | . | . | . | |
AFNDT-2066A | 12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .001" WIDE THRU NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001" | RM120-C3T2-7075-T6 | . | . | . | |
AFNDT-2067/1018 | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 1018 CRES STEEL PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 | UT-RC-5S1018 | . | . | . | |
AFNDT-2067/304S | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 304 STAINLESS STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 | . | . | . | . | |
AFNDT-2067/4340 | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 4340 CARBON STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 | . | . | . | . | |
AFNDT-2067/5086 | 5 STEP ALUMINUM WEDGE .100", .200", .300", .400",.500", 5086Al 1"X1" Sq..1"x5" LONG | . | . | . | . | |
AFNDT-2067/6AL-4V | 5 STEP WEDGE .100", .200", . 300", .400", .500" MATERIAL: 6AL-4V TITANIUM. PAD SIZE: .75" X .75", TOLERANCE = +/- .001". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2067/7075T6 | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 7075-T6 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 | TRS-5-1A | . | . | . | |
AFNDT-2067/7075T7 | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 7075-T7 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 | . | . | . | . | |
AFNDT-2067/TI | 5 STEP WEDGE .100"(2.54mm), .200"(5.08mm),. 300"(7.62mm), .400"(10.16mm), .500"(12.7mm) MATERIAL: 6AL-4V TiTANIUM. PAD SIZE: .75" X .75". Includes Test Report and Certificate of Conformance. ***NOTE: Must Engrave Both inch and Metric conversions on... | . | . | . | . | |
AFNDT-2067AL | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 2024-T3 ALUMINUM. PAD SIZE: 1.0" X 1.0" TOLEREANCE = +/- .001. Includes Test Report Traceable to NIST and Certificate of Conformance. | 2213E | . | . | . | |
AFNDT-2068 | CUSTOM CORROSION TEST PLATE 7075-T6 ALUMINUM. , 5%, 10%, 20%. PLATE SIZE: 8.0" x 5.0" x .125". 1.0"Ø SPOTFACE 3 PLACES. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2069/Ti | Custom Bolt Hole Standard 6Al-4v Titanium. Contains 12 hole sizes; 3/16, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 11/16, 3/4, 13/16, and 7/8 inch diameters.( .050" x .050" +/- .005" x .005"W +0.000" / -0.002" Corner EDM Notch. Per Boeing Specification 77... | . | . | . | . | |
AFNDT-2069AL | 13 HOLE REFERENCE STANDARD 7075-T6 aluminum. Hole Sizes: 3/16(.1875), 13/64(.203), 7/32(.218), 15/64(.234),1/4(.250), 17/64(.265), 9/32(.281), 19/64(.297), 5/16(.312),21/64(.328),11/32(.343), 23/64(.359), 3/8(.375). EDM NOTCH: .030" X. 030" x.005" ±.... | . | . | . | . | |
AFNDT-2069TI | 13 HOLE REFERENCE STANDARD 6AL-4V Titanium. Hole Sizes: 3/16(.1875), 13/64(.203), 7/32(.218), 15/64(.234),1/4(.250), 17/64(.265), 9/32(.281), 19/64(.297), 5/16(.312),21/64(.328),11/32(.343), 23/64(.359), 3/8(.375). EDM NOTCH: .030" X. 030" x.005" ±.00... | . | . | . | . | |
AFNDT-2070-AL | MD STACKABLE REFERENCE STANDARD, 06-20-01, .040, .050, .060, .063, .068, .071, .090, .100, .190, AL | . | . | . | . | |
AFNDT-2071 | BOEING REFERENCE STANDARD 767 PT 4 51-00-04 | . | . | . | . | |
AFNDT-2072AL | 5 STEP ALUMINUM WEDGE. Step Sizes: .600", .700", .800", .900" ,1.00", Tolerance: +/- .001'. Material: 2024-T3 Aluminum. Pad Size: 1.0"X1.0" Sq. 5.0"x1.0" LONG. Includes certification report traceable to NIST. Manufactured in accordance to Airbus A33 Figure 51-10-04-991-007-A and Boeing 777-200/300 PT 4 51-10-00 pages 1-4 | ECSBA-5 | . | . | . | |
AFNDT-2073AL | 12 HOLE REFERENCE STANDARD 7075-T6 aluminum. Hole Sizes: 25/64(.390), 13/32(.406), 27/64(.421),7/16(.437), 29/64(..453), 15/32(..468), 31/64(.484),1/2(.500), 33/64(.515),17/32(.531), 35/64(.546), 9/16(.562). EDM NOTCH: .030" X. 030" x.005" ±.001" WIDE... | . | . | . | . | |
AFNDT-2073TI | 12 HOLE REFERENCE STANDARD 6AL-4V Titanium. Hole Sizes: 25/64(.390), 13/32(.406), 27/64(.421),7/16(.437), 29/64(..453), 15/32(..468), 31/64(.484),1/2(.500), 33/64(.515),17/32(.531), 35/64(.546), 9/16(.562). EDM NOTCH: .030" X. 030" x.005" ±.001" WIDE ... | . | . | . | . | |
AFNDT-2074 | CUSTOM SURFACEREFERENCE STANDARD, 3 EDM SLOTS .008",.020",.040" .007" MAX WIDTH. MATERIAL: 7075-T6 ALUMINUM. SIZE: 4.0 x 1.5 x .25". Includes Test Report and Certifictate of Conformance. | TB-SI | TB-SI | . | ||
AFNDT-2075/1018 | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 4340 or 4130 CARBON STEEL . PAD SIZE:75"x.75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2075/4340 | Custom 6 Step Wedge .040", .050", .060", .075" ,0.090", 0.110" +/-.001", Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2075/AL/H | 5 STEP WEDGE .020, .040, .060, .080, .100 +/-.001 2024-T3 W/ HOLDER .75"x.75" FACE | . | . | . | . | |
AFNDT-2075/AL-1 | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM .PAD SIZE: 75" x .75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. | TRS-5-8A-7075-T6 | U8861613 | RT5-75-7075T6-020-100 | . | |
AFNDT-2075/AL-2 | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM .PAD SIZE: 75" x .75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. | TRS-5-8A-2024-T3 | . | . | . | |
AFNDT-2075/INC | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 718 INCONEL. PAD SIZE: 75" x .75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2075/TI | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM . PAD SIZE: 75" x .75" .Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. |
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AFNDT-2075CS | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 4340 CARBON STEEL . PAD SIZE:75"x.75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2075SS | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 304 STAINLESS. PAD SIZE: 75" x .75". Supplied with Delrin Holding Block. Includes Test Report traceable to NIST and Certificate of Conformance. |
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AFNDT-2076AL | 10 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. Hole Sizes: 1/8", 5/32", 3/16", 7/32" ,1/4", 9/32", 5/16", 3/8", 7/16", 1/2", .030" X. 030" x.005" +/- .001" WIDE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2076TI | 10 HOLE REFERENCE STANDARD 6AL-4v TITANIUM. Hole Sizes: 1/8", 5/32", 3/16", 7/32" ,1/4", 9/32", 5/16", 3/8", 7/16", 1/2", .030" X. 030" x.005" +/- .001" WIDE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2077/7075T6 | 5 STEP WEDGE .040", .080", .120", .160", .200" +/-.001", 7075-T6 ALUMINUM .75" x .75" STEP FACE | . | . | . | . | |
AFNDT-2078/7075T6 | 5 STEP WEDGE .240", .280", .320", .360", .400" +/-.001", 7075-T6 ALUMINUM 1.0" x 1.0" STEP FACE | . | . | . | . | |
AFNDT-2079/2024T3 | 6 STEP CALIBRATION BLOCK, STEP SIZES .030", .100", .250", .500", .750", 1.0" in 2024-T3 Aluminum | RT6-2024T3-.030/1.0 | . | . | . | |
AFNDT-2080/AL | MINI ANGLE BEAM BLOCK ALUM | . | . | . | . | |
AFNDT-2080AL | 2024-T3 ALUMINUM 6 STEP WEDGE 0.075", 0.100", 0.125, 0.150", 0.175", 0.200" +/-.001 TOLERANCE. Includes Test Report ancd Certificate of Conformance. | . | . | . | . | |
AFNDT-2081 | CUSTOM BOLT HOLE BLOCK, 7075-T6, 1/4" THICK, 3 SURFACE NOTCHES .008 / .020 / .040 DEEP, .020 THRU NOTCH FOR EACH HOLE, HOLE Ø 15/32, 1/2 , 9/16 , 5/8, 11/16, 3/4, 1/8, 7/16, 13/32, 3/8, 11/32, 5/16, 9/32, 1/4, 7/32, 3/16, 5/32, 7/8 | . | . | . | . | |
AFNDT-2082 | CUSTOM FOUR STEP BLOCK, 2205SS, 5.0MM, 10.0MM, 15.0MM, 20.0MM. 3/4"X3/4" | . | . | . | . | |
AFNDT-2083 | 10 HOLE REFERENCE STANDARD 2024-T3, HOLE SIZES, 1/8,5/32, 3/16 , 1/4, 5/16, 3/8, 7/16, 1/2, 5/8, 3/4, .030X.030 CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .75L X.010,.020,.040 DEEP | ECRS-218/AL | . | . | ||
AFNDT-2084 | CUSTOM 3 STEP BLOCK, CARBON STEEL, 1 1/8X5X1.75 | . | . | . | . | |
AFNDT-2085/7075-T6 | 6 STEP CALIBRATION BLOCK,STEP SIZES 1.0" X1.0"(500",.600",.700",.800",.900" and 1.0") +/- .001" 7075-T6 ALUMINUM . Includes certification Report Traceable to NIST, Meets tolerance for ASTM E797.. | . | . | . | . | |
AFNDT-2086CS | 4 STEP CALIBRATION BLOCK. STEP SIZES: .050", .075", .100", .125" ±.001, 3/4" X 3/4" PAD SIZE. MATERIAL: 1018 CARBON STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2086SS | 4 STEP CALIBRATION BLOCK. STEP SIZES: .050", .075", .100", .125" ±.001, 3/4" X 3/4" PAD SIZE. MATERIAL: 304 STAINLESS STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2087/CS | 5 STEP CALIBRATION BLOCK, .100, .200, .300, .400, .500, ± .001, 3/4X3/4 FACE, CARBON STEEL | . | . | . | . | |
AFNDT-2087/SS | 5 STEP CALIBRATION BLOCK, .100, .200, .300, .400, .500, ± .001, 3/4X3/4 FACE, STAINLESS STEEL | . | . | . | . | |
AFNDT-2088/2024-T3 | METRIC 10 STEP CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 20mm X 20mm. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2088/7075-T6 | METRIC 10 STEP CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 20mm X 20mm. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2089/7075T6 | 2 STEP WEDGE. STEP SIZE: .500", 1.0", +/-.001". MATERIAL: 7075-T6 ALUMINUM 2.0" x 2.0" PAD SIZE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2090AL | 5 STEP WEDGE, 11mm, 12mm, 13mm, 14mm, 15mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square. Includes Delrin Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2091/AL | 6 STEP CALIBRATION BLOCK, CUSTOM, .040, .080, .160 , .250, .300, .400, 2024-T3 | . | . | . | . | |
AFNDT-2091/MAG | 5 STEP CALIBRATION BLOCK, STEP THICKNESSES: .050, .100, .150 , .200, .250. STEP PAD SIZE: 1.0" x 1.0", MATERIAL: MAGNASESIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2091/S | 6 STEP CALIBRATION BLOCK, CUSTOM, .040, .080, .160 , .250, .300, .400, 4340 STEEL | . | . | . | . | |
AFNDT-2091/SS | 6 STEP CALIBRATION BLOCK, CUSTOM, .040, .080, .160 , .250, .300, .400, 300 STAINLESS STEEL | . | . | . | . | |
AFNDT-2091/TI | 6 STEP CALIBRATION BLOCK, CUSTOM, .040, .080, .160 , .250, .300, .400, 6AL-4V | . | . | . | . | |
AFNDT-2093/7075-T6 | 5 STEP CALIBRATION BLOCK,STEP SIZES 1.0" X1.0"(1.100", 1.200", 1.300", 1.400", 1.500" ) +/- .001" 7075-T6 ALUMINUM. Includes certification Report Traceable to NIST, Meets tolerance for ASTM E797 | . | . | . | . | |
AFNDT-2094/6.2 | EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 6.2 | . | . | . | . | |
AFNDT-2094/7.8 | EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 7.8 | . | . | . | . | |
AFNDT-2094/8.2 | EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 8.2 | . | . | . | . | |
AFNDT-2094AL | 5 STEP WEDGE .550", .600", .650", .700", .750". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2094SS | 5 STEP WEDGE .550", .600", .650", .700", .750". TOLERANCE +/-.001". MATERIAL: 304 STAINLESS STEEL. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2094TI | 5 STEP WEDGE .550", .600", .650", .700", .750". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | .. | |
AFNDT-2095 | 5 STEP WEDGE W/ BASE, .016, .020, .040 , .050, 2024-T3 | . | . | . | . | |
AFNDT-2096 | 5 STEP WEDGE, .063, .072, .080, .100, .125. 2024-T3 | . | . | . | . | |
AFNDT-2097AL | 7 STEP WEDGE. STEP SIZES: .030", .040", .050", .060", .070", .080", and .090" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2098/2024-T3 | 5 STEP WEDGE 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 25mm x 25mm. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2098/7175 | 5 STEP WEDGE 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 25mm x 25mm. Material: 7175-T73 Aluminum Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2099/2219-T8 | 5 STEP WEDGE 2219-T851 Aluminum 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 25mm x 25mm | . | . | . | . | |
AFNDT-2099/S | 5 STEP STANDARD .050, .100, .200, .300, .400, 1018 STEEL | . | . | . | . | |
AFNDT-2100/AL | 6 STEP STANDARD, .500, .600, .700, .800, .900, 1.00, ALUMINUM 2024-T351 | . | . | . | . | |
AFNDT-2100/S | 6 STEP STANDARD, .500, .600, .700, .800, .900, 1.00, 1018 STEEL | . | . | . | . | |
AFNDT-2100AL | 6 STEP STANDARD, 1MM, 2MM, 4MM, 6MM, 8MM, 10MM, ALUMINUM 2024-T351 | . | . | . | . | |
AFNDT-2100TI | 6 STEP WEDGE TITANIUM, 1MM, 2MM, 4MM, 6MM, 8MM, 10MM, 6AL-4V, 1.0" x 1.0" SQUARES, AMS 4928 | . | . | . | . | |
AFNDT-2101/AL | 5 STEP STANDARD, 1.00, 1.50, 2.00, 2.50, 3.0, ALLUMINUM | . | . | . | . | |
AFNDT-2101/S | 5 STEP STANDARD, 1.00, 1.50, 2.00, 2.50, 3.0, STEEL | . | . | . | . | |
AFNDT-2102/2219-T8 | 5 STEP WEDGE 2219-T851 Aluminum 0.5mm, 1.0mm,1.5mm, 2.0mm, 2.5mm +/- 0.05mm, Pad Size: 25mm x 25mm | . | . | . | . | |
AFNDT-2103AL | METRIC 5 STEP CALIBRATION BLOCK, 7075-T6 ALUMINUM. STEP SIZES: 2.5mm, 5.0mm, 7.5mm, 10.0mm, 12.5mm. PAD SIZE: 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | 2213M | . | . | . | |
AFNDT-2103CS | METRIC 5 STEP CALIBRATION BLOCK, 1018 CARBON STEEL. STEP SIZES: 2.5mm, 5.0mm, 7.5mm, 10.0mm, 12.5mm. Includes Test Report and Certificate of Conformance. | 2214M | . | . | . | |
AFNDT-2103SS | METRIC 5 STEP CALIBRATION BLOCK, 304 STAINLESS STEEL. STEP SIZES: 2.5mm, 5.0mm, 7.5mm, 10.0mm, 12.5mm. Includes Test Report and Certificate of Conformance. | 2211M | . | . | . | |
AFNDT-2103SS/E | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 304 STAINLESS STEEL. PAD SIZE: .75" x .75" TOLEREANCE = +/- .001. Includes Test Report Traceable to NIST and Certificate of Conformance. | 2211E | . | . | . | |
AFNDT-2104/15MM | CUSTOM 5 STEP WEDGE, 7075-T6 , 9MM, 7MM, 5MM, 3MM, 1MM, STEP FACE 15MMX15MM | . | . | . | . | |
AFNDT-2104/AL | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM .PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2105/360 | 5 STEP BLOCK, .100, .250, .500, .750, 1.00. 360BRASS, 3/4X3/4 STEP SIZE | . | . | . | . | |
AFNDT-2105/6061 | 5 STEP BLOCK, .100, .250, .500, .750, 1.00. 6061 ALUMINUM, 3/4X3/4 STEP SIZE | . | . | . | . | |
AFNDT-2105/COP | 5 STEP BLOCK, .100, .250, .500, .750, 1.00. COPPER, 3/4X3/4 STEP SIZE | . | . | . | . | |
AFNDT-2105AL | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 2024-T3 ALUMINUM. PAD SIZE: .75" x .75" TOLEREANCE = +/- .001. Includes Test Report Traceable to NIST and Certificate of Conformance. | UT-RC-5S2024-AL | . | . | . | |
AFNDT-2105TI | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 6AL-4V TITANIUM. PAD SIZE: .75" x .75" TOLEREANCE = +/- .001. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2106 | 3 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM.. HOLE SIZES: 5/32", 3/16", 1/4" TOTAL OF 3 EDM CORNER NOTCHES .030" x .030".N Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2106/2024 | 5 STEP WEDGE .020", .060", .150", .300", .600". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM . PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance. | TRS-5-12A/2024-T3 | TRS-5-12A/2024-T3 | . | ||
AFNDT-2106/7075 | 5 STEP WEDGE .020", .060", .150", .300", .600". TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM . PAD SIZE: 1.0" x 1.0" . Includes Test Report traceable to NIST and Certificate of Conformance. | TRS-5-12A/7075-T6 | TRS-5-12A/7075-T6 | . | ||
AFNDT-2107/4340 | EDDY CURRENT SURFACE REFERENCE STANDARD. EDM FLAWS: .008", .020", .040" (.005" Maximum Width). MATERIAL: 4340 STEEL. SIZE: 1.0"W x 4.0"L x .25"H. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2107/6AL4V | EDDY CURRENT SURFACE REFERENCE STANDARD. EDM FLAWS: .008", .020", .040" (.005" Maximum Width). MATERIAL: 6AL-4V TITANIUM. SIZE: 1.0"W x 4.0"L x .25"H. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2107/7075T6 | EDDY CURRENT SURFACE REFERENCE STANDARD. EDM FLAWS: .008", .020", .040" (.005" Maximum Width). MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25"H. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2108 | CUSTOM DEPTH METER BASE, BOTH PARTS PER SPEC | . | . | . | . | |
AFNDT-2108-1 | CUSTOM DEPTH METER BASE, PER FL TECHNICS SPEC. | . | . | . | . | |
AFNDT-2108-2 | CUSTOM DEPTH METER BASE, PER FL TECHNICS SPEC. | . | . | . | . | |
AFNDT-2109 | 15 Hole aluminum reference standard, material 7075-T6, hole sizes: 1/8, 5/32, 11/64, 3/16, 13/64, 7/32, 15/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64, 11/32, 23/64. With .030 x .030 and .020 x .020 Corner EDM Notches | . | . | . | . | |
AFNDT-2110 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (SELECTED RIVETS) | . | . | . | . | |
AFNDT-2110-.201 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.201" DIAMETER HOLE) | . | . | . | . | |
AFNDT-2110-.500D | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.500" DIAMETER HOLE D SHAPE) | . | . | . | . | |
AFNDT-2110-.812 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.812" DIAMETER HOLE) | . | . | . | . | |
AFNDT-2110-.950 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (.950" DIAMETER HOLE) | . | . | . | . | |
AFNDT-2110-1.06 | CUSTOM EDDY CURRENT TEMPLATE.2024-T3 ALUMINUM .063" THICK PLATE. (1.06" DIAMETER HOLE) | .. | . | . | . | |
AFNDT-2111 | CUSTOM CALIBRATION TEST STANDARD. PER CUSTOMER SPECS | . | . | . | . | |
AFNDT-2112 | CUSTOM EC CORROSION EVALUATION BLOCK ART72 FIG 617 | . | . | . | . | |
AFNDT-2114AL | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.006W +/- .001). BLOCK SIZE:3.156 "L x 1.375"W x .312"H. MATERIAL: 2024-T3 ALUMINUM. | . | . | . | . | |
AFNDT-2115 | 10 STEP REFERENCE BLOCK .025", .030", .040", .050", .063", .071", .080", .090", .100", .120" +/-.001" 2024-T6 ALUMINUM .75" x .75" STEP PAD. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2116 | CUSTOM EC REFERENCE STANDARD BRT189-080 REV A, STEEL 15-5PH | . | . | . | . | |
AFNDT-2117AL | 6 STEP THICKNESS STANDARD. STEP SIZES: .050", .100", .200", .300", .400, .500" +/-.001". PAD SIZE 1.0" x 1.0". MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2118 | CUSTOM 6 STEP BLOCK, 0.5mm, 1mm,2mm, 3mm, 4mm, 5mm +/- .05mm . Pad Size: .750" x .750" Material- 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2119AL | 5 STEP WEDGE, 11mm, 12mm, 13mm, 14mm, 15mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 20mm x 20mm square. Includes Delrin Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2120 | CUSTOM EDDY CURRENT BLOCK, 4340, 4X1X.250, EDM .2MM, .5MM, 1.0MM X .005±.002. ADD.003 NON-CONDUCTIVE SHIMS | . | . | . | . | |
AFNDT-2121AL | 5 STEP WEDGE .300", .350", .400", .450", .500". TOLERANCE +/-.001". MATERIAL: 2024-T3 ALUMINUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2121SS | 5 STEP WEDGE .300", .350", .400", .450", .500". TOLERANCE +/-.001". MATERIAL: 304 STAINLESS STEEL. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-2121TI | 5 STEP WEDGE .300", .350", .400", .450", .500". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | |||
AFNDT-2122/C/1.5/.050 | BEECHCRAFT STANDARD CURVED, 1.5Ø, .050 | . | . | . | . | |
AFNDT-2122/C/1.5/.100 | BEECHCRAFT STANDARD CURVED, 1.5Ø, .100 | . | . | . | . | |
AFNDT-2122/C/2.5/.050 | BEECHCRAFT STANDARD CURVED, 2.5Ø, .050 | . | . | . | . | |
AFNDT-2122/C/2.5/.100 | BEECHCRAFT STANDARD CURVED, 2.5Ø, .100 | . | . | . | . | |
AFNDT-2122/F.050 | BEECHCRAFT STANDARD FLAT .050 | . | . | . | . | |
AFNDT-2122/F.100 | BEECHCRAFT STANDARD FLAT .100 | . | . | . | . | |
AFNDT-2123AL | 12 HOLE REFERENCE STANDARD 7075-T6, 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", .005" +/-.001" THROUGH NOTCH ON EACH HOLE and A .030" x .030" x .005+/- .001" CORNER NOTCH IN EACH HOLE. SURFACE NOTCHES: .008", .020"... | . | . | . | . | |
AFNDT-2123S | 12 HOLE REFERENCE STANDARD 4340 STEEL, 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", .005" +/-.001" THROUGH NOTCH ON EACH HOLE and A .030" x .030" x .005+/- .001" CORNER NOTCH IN EACH HOLE. SURFACE NOTCHES: .008", .0... | . | . | . | . | |
AFNDT-2123TI | 12 HOLE REFERENCE STANDARD 6AL-4v TITANIUM, 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", .005" +/-.001" THROUGH NOTCH ON EACH HOLE and A .030" x .030" x .005+/- .001" CORNER NOTCH IN EACH HOLE. SURFACE NOTCHES: .008... | . | . | . | . | |
AFNDT-2124 | CUSTOM REFERENCE STANDARD PER SPEC, 2024-T42 | . | . | . | . | |
AFNDT-2125/AL | CUSTOM MULTI HOLE ET STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 3/16", 7/32", 1/4", 5/16", 3/8", 7/16", 1/2", 9//16", 5/8", 3/4". EDM NOTCH: .030" x .030" x .005" +/-.002" and .020" x .020" x .005" +/-.002" | . | . | . | . | |
AFNDT-2125/S | CUSTOM MULTI HOLE ET STANDARD. MATERIAL: 4130 STEEL. HOLE SIZES: 3/16", 7/32", 1/4", 5/16", 3/8", 7/16", 1/2", 9//16", 5/8", 3/4". EDM NOTCH: .030" x .030" x .005" +/-.002" and .020" x .020" x .005" +/-.002" | . | . | . | . | |
AFNDT-2125/TI | CUSTOM MULTI HOLE ET STANDARD. MATERIAL: 6AL-4V TITANIUM. HOLE SIZES: 3/16", 7/32", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4". EDM NOTCH: .030" x .030" x .005" +/-.002" and .020" x .020" x .005" +/-.002". 3 SURFACE EDM NOTCHES: .008", .020"... | . | . | . | . | |
AFNDT-2126 | BOEING DC-9/MD80 3-2 PAGE 5 | . | . | . | . | |
AFNDT-2127 | SAFRAN MESSIER -BUGATTI-DOWTY REFERENCE STANDARD 32-09-01-041-006-A01 | . | . | . | . | |
AFNDT-2128 | 12 HOLE REFERENCE STANDARD 2024-T3, .156, .187, .199, .218, .250, .281, .312, .343, .375, .406, .437, .500, .020X.020 CORNER NOTCH, .030X.030 CORNER NOTCH, EDM PER 737 PT 6 51-00-00 IFG 3 | . | . | . | . | |
AFNDT-2129 | 10 STEP WEDGE .008", .020", .050", .080", .100", .150", .220", .300", .400", .500" +/-.005" INCONEL 718 .75" x .75" STEP FACE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2129/BASE | 6 STEP BLOCK, 4130 STEEL, .050, .060, .070, .080, .090, .100. .750"X.750", ±.001, WITH BASE .250" 3/4X3/4 | . | . | . | . | |
AFNDT-2129CS | LEONDRO CALIBRATION BLOCK PAGE 18 FIGURE 3 S.B. N°169-165. 2 STEP BLOCK, MATERIAL: LOW CARBON STEEL SUCH AS 1018, 4130 or 4340. Step Size: 2-3mm and 10-11mm. ±.0.1mm, PAD SIZE: 20mm X 20mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2130AL | 9 HOLE REFERENCE STANDARD 7075-T6, HOLE SIZES, 1/2",, 9/16" , 5/8", 11/16, 3/4", 13/16", 7/8", 15/16", 1.0", .030X.030 CORNER NOTCH .005+/-.001 | . | . | . | . | |
AFNDT-2130S | 9 HOLE REFERENCE STANDARD 4130 STEEL, HOLE SIZES, 1/2",, 9/16" , 5/8", 11/16, 3/4", 13/16", 7/8", 15/16", 1.0", .030X.030 CORNER NOTCH .005+/-.001 | . | . | . | . | |
AFNDT-2130TI | 9 HOLE REFERENCE STANDARD 6Al-4V Titanium , HOLE SIZES, 1/2",, 9/16" , 5/8", 11/16, 3/4", 13/16", 7/8", 15/16", 1.0", .030X.030 CORNER NOTCH .005+/-.001 | . | . | . | . | |
AFNDT-2131 | CUSTOM 6 STEP BLOCK : (1mm, 2mm, 4mm, 6mm, 8mm, 10mm, +/- .05mm thick. total of 6 steps. Material- 2024-T6 Aluminum | . | . | . | . | |
AFNDT-2132/2024-T3 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16",19/32", 5/8", 21/32", 11/16", 23/32", 3/4". TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x ... | RH20-C30M20-2024T3 | . | . | . | |
AFNDT-2133/304L | 20 HOLE REFERENCE STANDARD 304L STAINLESS STEEL. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001 | RH20-C30-304L | . | . | . | |
AFNDT-2133/4130 | 20 HOLE REFERENCE STANDARD 4130 CARBON STEEL. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001 | RH20-C30-4130 | . | . | . | |
AFNDT-2133/6AL4V | 20 HOLE REFERENCE STANDARD 6AL-4V TITANIUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001 | RH20-C30-6AL4V | . | . | . | |
AFNDT-2133/7075T6 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001 | RH20-C30-7075T6 | . | . | . | |
AFNDT-2133AL-1 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001 NOTCHES .008", .020", .040" (.004"W +/- .002), 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2136 | 12 HOLE REFERENCE STANDARD 6061-T6. HOLE SIZES: 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4". .030" x .030" x .005" +/- .001" W CORNER NOTCH IN EACH HOLE. SURFACE NOTCHES: .008", .020", .040" . .005" +/-.001" | . | . | . | . | |
AFNDT-2137/6AL4V | 3 HOLE REFERENCE STANDARD 6AL-4V TITANIUM. HOLE SIZES: 7/32, 1/4, 9/32 TOTAL OF 3 EDM THROUGH NOTCHES .020 DEEP | RCH3-T20-6AL4V | . | . | . | |
AFNDT-2138/6AL-4V | 3 HOLE COUNTERSINK REFERENCE STANDARD 6AL-4V TITANIUM. HOLE SIZES: 7/32, 1/4, 9/32 TOTAL OF 3 EDM THROUGH NOTCHES .020 DEEP | RCH3-T20-6AL4V | . | . | . | |
AFNDT-2140/304L | 11 HOLE REFERENCE STANDARD IN 304L STAINLESS STEEL; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH .030"x.030" CORNER EDM NOTCH IN EACH HOLE. | . | . | . | . | |
AFNDT-2140/4130 | 11 HOLE REFERENCE STANDARD IN 4130 CARBON STEEL; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16,5/8,11/16, 3/4), WITH .030"x.030" CORNER EDM NOTCH IN EACH HOLE. | . | . | . | . | |
AFNDT-2140/6AL4V | 11 HOLE REFERENCE STANDARD IN 6AL-4v Ti; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH .030"x.030" CORNER EDM NOTCH IN EACH HOLE. | . | . | . | . | |
AFNDT-2140/7075 | 11 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH .030"x.030" CORNER EDM NOTCH IN EACH HOLE. | . | . | . | . | |
AFNDT-2141AL | 12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER EDM NOTCH and .020" MID-WALL EDM NOTCH IN EACH HOLE. Tolerance: .005" +/-.001". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2142 | 6 STEP WEDGE .200", .300",. 400", .500", .650" , .800" MATERIAL: 7075-T6 ALUMINUM. LENGTH: 0.8" x 4.8". TOLERANCE = +/- .001. Includes Test Report and Certificate of Conformance | . | . | . | . | |
AFNDT-2143 | 6 STEP WEDGE .024", .040",. 060", .080", .100" , .150" MATERIAL: 7075-T6 ALUMINUM. LENGTH: 0.8" Wide x 1.1" Long for the first and last step. 0.8" x 1.1" long for the 4 inside steps. Total Length = 5.4" Long. TOLEREANCE = +/- .001. Includes Hold... | . | . | . | . | |
AFNDT-2144 | 13 HOLE REFERENCE STANDARD 7075-T6 Auminum. Hole Sizes: (5/32",3/16", 7/32" ,1/4", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 1.0"), . 040" DEEP x .005" WIDE +0.00/-.002" THROUGH EDM NOTCH in EACH HOLE | . | . | . | . | |
AFNDT-2145AL | Custom calibration standard containing 4 hole sizes of 5mm, 6mm, 8mm and 10mm. Each hole has a .100" x .100" x .005" W +/- .002". Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2145MG | Custom calibration standard containing 4 hole sizes of 5mm, 6mm, 8mm and 10mm. Each hole has a .100" x .100" x .005" W +/- .002". Material: Mgnesium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2146AL | ALUMINUM CHEM MILL MEASURING STEP WEDGE. MATERIAL: 2024-T3 ANODISED ALUMINUM. STEPS: .024, .028, .031, .035, .039, .044, .048, .052, .056, .059 +/-.002". Includes Test eport and Certificate of Conformance. | . | . | . | . | |
AFNDT-2146S | STEEL CHEM MILL MEASURING STEP WEDGE. MATERIAL: 4340 STEEL CHROME COATED. STEPS: .024, .028, .031, .035, .039, .044, .048, .052, .056, .059 +/-.002". Includes Test eport and Certificate of Conformance. | . | . | . | . | |
AFNDT-2147/2024-T3 | Step Wedge: 2024-T3 Aluminium, 5 Steps total (2.5mm, 5.0mm, 7.5mm, 10.0mm and 12.5mm). Step pad size: .75” x .75”. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2147/7075-T6 | Step Wedge: 7075-T6 Aluminium, 5 Steps total (2.5mm, 5.0mm, 7.5mm, 10.0mm and 12.5mm). Step pad size: .75” x .75”. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2147/TI | Step Wedge: 6AL-4V TITANIUM, 5 Steps total (2.5mm, 5.0mm, 7.5mm, 10.0mm and 12.5mm). Step pad size: .75” x .75”. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2148AL | Step Wedge: 7075-T6 Aluminium, 5 Steps total (0.5mm, 5mm, 7.5mm, 10mm and 12.5mm). Step pad size: 1” x 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2148S | Step Wedge: 4340 Steel, 5 Steps total (0.5mm, 5mm, 7.5mm, 10mm and 12.5mm). Step pad size: 1” x 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2148SS | Step Wedge: 304 Stainless Steel, 5 Steps total (0.5mm, 5mm, 7.5mm, 10mm and 12.5mm). Step pad size: 1” x 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2149AL | 13 HOLE REFERENCE STANDARD 7075-T7 Auminum. Hole Sizes: (5/32",3/16", 7/32" ,1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.0"), . 020" DEEP x .005" MAX WIDTH THROUGH EDM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2149AL-1 | 13 HOLE REFERENCE STANDARD 7075-T7 Auminum. Hole Sizes: (5/32",3/16", 7/32" ,1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.0"), . 040" DEEP x .005" MAX WIDTH THROUGH EDM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2149SS | 13 HOLE REFERENCE STANDARD 304 Stainless Steel. Hole Sizes: (5/32",3/16", 7/32" ,1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.0"), . 020" DEEP x .005" MAX WIDTH THROUGH EDM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2150AL | 9 HOLE REFERENCE STANDARD 7075-T6, HOLE SIZES, 3/16",, 7/32" , 9/32", 5/16, 11/32", 3/8", 7/16", 5/8", 3/4", CORNER EDM NOTCH .030X.030 +/- 10%; WIDTH: .005+/-.001. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2151AL | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.005"W + .001"), MATERIAL: 5086 H32 ALUMINUM. (29.0% IACS. SIZE: 80mm(3.15") L +5mm(.197") x 30mm(1.18") W +5mm(.197") x 8mm(.315") THICK +3mm(.118"). Includes Mill Certifica... | . | . | . | . | |
AFNDT-2157AL | 10 STEP REFERENCE BLOCK .025", .030", .040", .050", .063", .071", .080", .090", .100", .120" +/-.001" 7075-T6 ALUMINUM .75" x .75" STEP PAD. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2160/19MM | Custom ASME ultrasonic phased array PAUT Calibration Block per customer supplied drawing. 270mm x 150mm x 19mm. Material: 1018 Carbon Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2160/38MM | Custom ASME ultrasonic phased array PAUT Calibration Block per customer supplied drawing. 330mm x 150mm x 38mm. Material: 1018 Carbon Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-2161/4130 | 10 STEP CARBON STEEL WEDGE. STEP THICKNESS OF: 1.10", 1.20", 1.30", 1.40", 1.50", 1.60", 1.70", 1.80", 1.90" 2.00" +/-.001". 0.75" x 0.75" Step Pad Face. Material: 4130 Carbon Steel, Nickel Plated. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-21-6-9 | CUSTOM REFERENCES STANDARD PER AMSS5561 | . | . | |||
AFNDT-2227Ti | CUSTOM TITANIUM EDDY CURRENT MULTI HOLE STANDARD WHICH COMBINES BOEING PART NUMBERS NDT1022-NDT1027 STANDARDS INTO ONE PART..HOLE SIZES ( 0.188", 0.250", 0.313", 0.375",0.438", 0.500" ) | . | . | . | . | |
AFNDT-2227Ti-1 | 8 Hole Calibration Standard, Hole Sizes; 1/8" 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", EDM NOTCH: .050" x .050" x .005" +0.000/-.002" BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, 737 PT 6 51-00-00 FIG 3 PROCEDURE 17, PG.8 MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3001 | Embraer 170 reference standard with a .473" diameter hole. Per NDTM PT1 51-00-00-916-802-A , 1.4mm x 1.4mm +/-.05mm long x 0.1mm +/-.05 wide corner EDM notch. Material: 7050-T7 Aluminum. Block size 2.0" x 2.0" x .375" | . | . | . | . | |
AFNDT-3002/2024-T3 | 6 STEP WEDGE .030", .040", .060", .080", .100", .150" +/-.001", 2024-T3 ALUMINUM 0.75" x 0.75" STEP FACE. 6.0" X 1.0" LENGTH INCLUDES HOLDER | TRS-6-8A-2024-T3 | . | . | . | |
AFNDT-3002/7075-T6 | 6 STEP WEDGE .030", .040", .060", .080", .100", .150" +/-.001", 7075-T6 ALUMINUM 0.75" x 0.75" STEP FACE. 6.0" X 1.0" LENGTH INCLUDES HOLDER | TRS-6-8A-7075-T6 | . | . | . | |
AFNDT-3003INC | 2 STEP WEDGE. MATERIAL: INCONEL 718 Dimension: 1.37” L x 1.0” W x Step thickness 0.016” & 0.050 +/- .001". Step Pad Size: .685” x 1.0" Includes Certification Report... | . | . | .. | . | |
AFNDT-3003SS | 2 STEP WEDGE. MATERIAL: 304 STAINLESS STEEL, Dimension: 1.37” L x 1.0” W x Step thickness 0.016” & 0.050 +/- .001". Step Pad Size: .685” x 1.0". Includes Certification Report. | . | . | . | . | |
AFNDT-3003TI | 2 STEP WEDGE. MATERIAL: 6AL-4V Titanium - AMS 4919 Dimension: 1.37” L x 1.0” W x Step thickness 0.016” & 0.035 +/- .001". Step Pad Size: .685” x 1.0". Includes Certification Report... | . | . | . | . | |
AFNDT-3004S | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .020 THRU NOTCH and 3 SURFACE NOTCHES .020", .030", .040" DEEP x .750" LONG.) 4340 STEEL | . | . | . | . | |
AFNDT-3006AL | Step Wedge: Material: 2024-T3 Aluminium, 5 Steps total (12mm, 14mm, 16mm, 18mm and 20mm). Tolerance = +/-0.05mm. Step pad size: 1.0” x 1.0". Includes Mill Test Report, Calibration Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3007 | SURFACE NOTCH REFERENCE STANDARD 15-5 PH STEEL. EDM NOTCH SIZE: FULL WIDTH OF PART x .20mm(.008") WIDE x .50mm(.020") DEEP +/- .05mm(.002"). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3008AL | 5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: ANODIZED 2024-T4 ALUMINUM .PAD SIZE: 75" x .75" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3009 | CUSTOM BOLT HOLE STANDARD 6AL-4V TITANIUM. HOLE SIZES: 7/32", 7/4", 9/32" CONTAINING 0.020" DEEP x .005" WIDE edm NOTCHES IN THE COUNTERSINK OF EACH HOLE | RCH3-T20-6AL4V | . | . | . | |
AFNDT-3010/2024 | 11 STEP WEDGE STEP THICKNESS OF .050", .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001" 2024-T3 ALUMINUM | . | . | . | . | |
AFNDT-3010/304 | 11 STEP WEDGE. STEP THICKNESS OF , .050", .100", .200", .300", .400", .500", .600", .700", .800" .900", 1.0" +/-.001". Pad Size: .75" x 75" . Material: 304 Stainless Steel. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3010/4340 | 11 STEP WEDGE STEP THICKNESS OF .050", .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001" 4340 STEEL | . | . | . | . | |
AFNDT-3010/7075-T6 | METRIC 10 STEP CALIBRATION BLOCK, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, 20mm ± .05mm. Pad Size: 20mm X 20mm. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3010/7075-T7 | 11 STEP WEDGE. STEP THICKNESS OF , .050", .100", .200", .300", .400", .500", .600", .700", .800" .900", 1.0" +/-.001". Pad Size: .75" x 75" . Material: 7075-T7 ALUMINUM. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3010/MAG | 11 STEP WEDGE. STEP THICKNESS OF , .050", .100", .200", .300", .400", .500", .600", .700", .800" .900", 1.0" +/-.001". Pad Size: .75" x 75" . Material: AZ31B MAGNESIUM. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3011AL | 4 HOLE REFERENCE STANDARD 7075-T6,1/8"(3.2mm),5/32"(3.9mm),1/4"(6.5mm),9/32"(7.1mm), .005" +/-.001" THROUGH NOTCH ON EACH HOLE and .030" x .030" x .005+/- .001" CORNER NOTCH IN EACH HOLE. .005" +/-.001". Includes Test Report and Certificate of Confor... | . | . | . | . | |
AFNDT-3012AL | 9 HOLE REFERENCE STANDARD PER BOEING 737 NTM 51-00-00 PG 9 FIGURE 3 SPECIFICATION. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES, 1.0",1.125",1.250", 1.375", 1.500"", 1.625", 1.750", 1.875", 2.00", .030"x.030" and .020"x.020" CORNER NOTCH .005+/-.002. Includ... | NDT1084 | . | . | . | |
AFNDT-3013/2024 | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 2024 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013/301 | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 301 Stainless Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013/304 | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 304 Stainless Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | |||||
AFNDT-3013/4340 | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 4340 Cres Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013/7075 | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 7075 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013/INC | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 718 Inconel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013/TI | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 6AL-4V Titanium. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013AL | 6 STEP WEDGE, 0.5mm,1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013CS | 6 STEP WEDGE, 0.5mm 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 4340 Carbon Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3013TI | 5 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: 6AL-4V Titanium. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3014AL | 8 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3014CS | 8 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm +/- .05mm. Material: 4340 Carbon Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3014SS | 8 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm +/- .05mm. Material: 304 Stainless Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3014TI | 8 STEP WEDGE, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm +/- .05mm. Material: 6AL-4V Titanium. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3015 | EMBRAER 170/190 SERIES EDDY CURRENT SURFACE REFERENCE STANDARD 50-00-00 PT 1 PAGE 4, Aluminum(7075-T6) 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05mm WIDE). Includes Test Report and Certificate of Conformance. | GSE206 | . | . | . | |
AFNDT-3016-2024T3 | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 Corner EDM Notch and 3 Surface EDM Notches .010", .020", .040" Deep x .750" Long.) Material: 2024-T3 Aluminum | RM120-C30 2024T3 | RM120-C30-2024T3 | . | . | |
AFNDT-3017/7175 | 5 STEP WEDGE, 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 19mm x 19mm. Material: 7175-T73 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3017AL | 5 STEP WEDGE 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 19mm x 19mm. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | , | , | , | |
AFNDT-3017CS | 5 STEP WEDGE 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 19mm x 19mm. Material: 4340 Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3018TI | CUSTOM TITANIUM BORE HOLE STANDARD WITH 2.200" BORE with 2 EDM FLAWS .030" CORNER NOTCH, .060"x.030" MID-BORE NOTCH. MATERIAL: 6AL-4V. SIZE 3.0" X 3.0" X 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3019S | CUSTOM AIR FORCE EDDY CURRENT BOLT HOLE STANDARD PER CUSTOMER SUPPLIED DRAWING, 1/4" 8630 STEEL PLATE (4130 EQUIVALENT ALTERNATIVE). EDM: 0.030 x 0.030 CORNER NOTCH. HOLE DIAMETER= 0.437Ø. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3020AL | 8 STEP THICKNESS STANDARD. STEP SIZES: .015", .025", .040", .060", .080", .100", .150", .200" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | TRS-8-9A-7075-T6 | . | . | . | |
AFNDT-3020CS | 8 STEP THICKNESS STANDARD. STEP SIZES: .015", .025", .040", .060", .080", .100", .150", .200" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 1018 CARBON STEEL. Includes Test Report and Certificate of Conformance. | TRS-8-9S-1018 | U8862920 | . | . | |
AFNDT-3020TI | 8 STEP THICKNESS STANDARD. STEP SIZES: .015", .025", .040", .060", .080", .100", .150", .200" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | TRS-8-9T | U8880197 | . | . | |
AFNDT-3021AL | Custom Metric 6 Step Block. Step Thicknesses of 0.5mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm. (Tolerance: +/- 0.2mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 2024-T3 Aluminum. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3022 | BOMBARDIER SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL 7075-T6 ALUMINUM. SIZE: 1.5"W x 3.75"L x .25". Includes Test Report and Certificate of Conformance. ( Similar to Specification BD-700 PT 6 ... | . | . | . | ||
AFNDT-3023 | BOMBARDIER SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL 7050-T74 ALUMINUM. SIZE: 1.5"W x 3.75"L x .25". Includes Test Report and Certificate of Conformance. ( Similar to Specification BD-700 PT 6... | . | . | . | ||
AFNDT-3024AL | 12 HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .004" +/- .002" WIDE THROUGH EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010"... | VM89A-1 | . | . | . | |
AFNDT-3024SS | 304 STAINLESS STEEL AWS RESOLUTION BLOCK 1.0" x 3.0" x 6.0". WITH A QUANTITY OF (9) .062" DIAMETER HOLES. | . | . | . | . | |
AFNDT-3025AL | Eddy Current Surface Standard 7075-T6 Aluminum. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W x... | . | . | . | . | |
AFNDT-3025CS | Eddy Current Surface Standard 4340 Carbon Steel. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W ... | . | . | . | . | |
AFNDT-3025INC | Eddy Current Surface Standard 718 Inconel. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W x (25m... | . | . | . | . | |
AFNDT-3025SS | Eddy Current Surface Standard 304 Stainless Steel. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)... | . | . | . | . | |
AFNDT-3025TI | Eddy Current Surface Standard 6AL-4V Titanium. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W x ... | . | . | . | . | |
AFNDT-3026AL | EDDY CURRENT SURFACE REFERENCE STANDARD Leonardo Helicopters SB No. 109EP-158. MATERIAL: 7475-T7 ALUMINUM. SIZE: 1.0" x 3.0" x .25" EDM SLOT (0.5mm DEEP) x (0.05-0.25mm WIDE) +/-.03mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3027AL | MHS style Multi-Hole reference standard (Aluminum 7075-T6 with certifications). 12 Holes 3/16", 7/32", 1/4" ,9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 11/16" ( .030 x .030 x .006 +/- .001) Corner Notches and .010, .020, .040 Surface notch... | . | . | . | . | |
AFNDT-3028AL | 3i-Hole reference standard (Aluminum 7075-T6 with certifications). Hole Sizes , 7/16", 1/2" and 11/16" ( .030 x .030 x .006 +/- .001) Corner Notches | . | . | . | . | |
AFNDT-3029/2024 | 6 STEP WEDGE .100", .200",. 300", .400", .500" , .600". MATERIAL: 2024-T3 ALUMINUM. STEP PAD SIZE: .787" x .787". TOLERANCE = +/- .001. Includes Test Report and Certificate of Conformance | . | . | . | . | |
AFNDT-3029/7075 | 6 STEP WEDGE .100", .200",. 300", .400", .500" , .600". MATERIAL: 7075-T6 ALUMINUM. STEP PAD SIZE: .787" x .787". TOLERANCE = +/- .001. Includes Test Report and Certificate of Conformance | . | . | . | .. | |
AFNDT-3030 | Step Wedge: 7075-T6 Aluminium, 5 Steps total (.010", .016", .020", .030", .040"). Step pad size: 1” x 1”. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3031 | 4 STEP WEDGE 2mm, 3mm, 4mm, 5mm, +/- .05mm. Material: Magnesium RZ5. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3032 | 3 HOLE 100° COUNTERSINK REFERENCE STANDARD 2024-T3 ALUMINUM, PLATE SIZE: 3.0" x 2.0" x 1/4" . HOLE SIZES: 5/32", 3/16" and 1/4" TOTAL OF 3 EDM NOTCHES .040" +0.004"/-0.000" Long x .007" Max Width Through the Depth of the Countersink. | . | . | . | . | |
AFNDT-3032-1 | 3 HOLE 100° COUNTERSINK REFERENCE STANDARD 7075-T6 ALUMINUM, PLATE SIZE: 3.0" x 2.0" x 1/4" . HOLE SIZES: 3/16", 7/32" and 1/4" TOTAL OF 3 CORNER EDM NOTCHES: .030" +0.004"/-0.000" Long x .007" Max Width Through the Depth of the Countersink. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3033/17-4 | 5 STEP WEDGE, .100", .200",. 300", .400", .500" MATERIAL: 17-4PH STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .002 | . | . | . | . | |
AFNDT-3033/718 | 5 STEP WEDGE, .100", .200",. 300", .400", .500" MATERIAL: 718 inconel. PAD SIZE: .75" X .75" TOLEREANCE = +/- .002 | . | . | . | . | |
AFNDT-3034AL | Custom Bolt Hole / Countersink Reference Standard Combination Containing 6 Bolt Hole Sizes of .171", .218", .281", .343", .406", .500". EDM Slot Size: .030" x .030" x .005" Wide +/- .001". 5 Holes with 100° Countersinks, Hole Sizes: .218", .312", .37... | . | . | . | . | |
AFNDT-3035SS | EDDY CURRENT SURFACE REFERENCE STANDARD. EDM NOTCHES: .005", .010", .020", .060" (.005"W +/- .002, MAX.007" WIDE). MATERIAL: 301 1/2 HARD STAINLESS STEEL(MIL-S-5059) 1.0"W x 4.0"L x .125", NOTE: .750" DISTANCE BETWEEN EACH NOTCH. Includes Test Repor... | . | . | . | . | |
AFNDT-3036AL | CUSTOM 2 HOLE EDDY CURRENT REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES: .250" and .875" WITH a .030" x .030" x .007" MAX WIDTH CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3037 | CUSTOM EDDY CURRENT HOLE REFERENCE STANDARD. MATERIAL: 718 INCONEL. HOLE SIZE: .256"Ø WITH a 0.1" x 0..1" x .010" +/- .002" EDM NOTCH IN THE BOTTOM RADIUS OF THE HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3038 | CUSTOM BOND LINE STANDARD. 3.0" x 6.0" LONG, 2024-T351 ALUMINUM. BOEING BMS 5-101 ADHESIVE. QUANTITY OF 2 0.5" x 0.5" DISBOND VOIDS. | . | . | . | . | |
AFNDT-3039 | CUSTOM SURFACE CALIBRATION BLOCK. MATERIAL: 7075-T73 ALUMINUM. EDM NOTCH SIZE: 1.52mm(.060") LONG x 0.13mm(.0051") WIDE x 0.76mm(.030") DEEP. +/- .05mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3045-2024T3 | 10 STEP REFERENCE BLOCK .010", .020", .030", .040", .050", .060", .070", .080", .090", .100", +/-.001" . Material: 7075-T6 ALUMINUM, Pad Size: .75" x 75" with Acetal( Delrin) holding block . Includes Test Report and Certificate of Conformance. | . | ... | . | . | |
AFNDT-3045-7075T6 | 10 STEP REFERENCE BLOCK .010", .020", .030", .040", .050", .060", .070", .080", .090", .100", +/-.001" . Material: 7075-T6 ALUMINUM, Pad Size: .75" x 75" with Acetal( Delrin) holding block. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-304AWSDS | DISTANCE / SENSITIVITY (DS) CALIBRATION BLOCK 304 STAINLESS STEEL AWS type DS | . | . | . | . | |
AFNDT-304DAA19 | ASTM DISTANCE AMPLITUDE SET OF 19 304 STAINLESS STEEL (CASE INCL) 3/34", 5/64" and 8/64" FLAT BOTTOM HOLES | 200129-0 | . | . | . | |
AFNDT-3051AL | (Aluminum Multi-hole reference standard with certificate. Contains 2 rows of 6 hole sizes. The first row has no flaws or side drilled holes. The second row includes side drilled holes. Hole Sizes: 3/16", 1/4", 5/16", 3/8", and 1/2". Material: 7075-T6 ... | ATB005 | . | . | . | |
AFNDT-3052AL | (Aluminum Multi-hole reference standard with certificate. Contains 2 rows of 29 hole sizes. The first row has no flaws or side drilled holes. The second row includes side drilled holes. Hole Sizes: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32"... | ATB004 | . | . | . | |
AFNDT-3053AL | 11 STEP THICKNESS STANDARD. STEP SIZES: .010", .020", .030", .040", .050", .060", .070", .080", .090", ..100", .110" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | TRS-11-4A-2024 | U8863168 | . | . | |
AFNDT-3054/CS | 5 STEP WEDGE .100", .125",. 150", .175", .200" MATERIAL: 4340 CARBON STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 | . | . | . | . | |
AFNDT-3055 | EDDY CURRENT SURFACE REFERENCE STANDARD. Low Hydrogen Embrittlement Cadmium-Titaniium Alloy Plating per BAC5804. 3 EDM FLAWS ON BOTH SIDES. ONE SIDE UNPLATED(BARE). NOTCH DEPTHS : .010", .020", .050". NOTCH WIDTH: (.007" +/- .002"). MATERIAL: 4330 STE... | . | . | . | . | |
AFNDT-3056AL | 10 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. Hole Sizes: 3/16", 7/32" ,1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16', 5/8". Corner EDM Notches: .020" x .020" x .005" +/- .001" Wide and Mid-Wall EDM Notches .020" x .020" x .005" +/- .001" Wide in Each... | . | . | . | . | |
AFNDT-3057AL | Custom 3 Step Thin Wedge with Holder. Step Thicknesses: 0.015", 0.030" and 0.070". Pad Size: 1.0" x 1.0" x 3.0" Total Length. Step ThicknessTolerence +/- .001. Material: 7075-T6 Aluminum Also Contains 2 EDM Flaws .010" and .020" Deep x .005" Wide x .3... | . | . | . | . | |
AFNDT-3057ST | Custom 3 Step Thin Wedge with Holder. Step Thicknesses: 0.015", 0.030" and 0.070". Pad Size: 1.0" x 1.0" x 3.0" Total Length. Step ThicknessTolerence +/- .001. Material: 4340 Cres Steel. Also Contains 2 EDM Flaws .010" and .020" Deep x .005" Wide x .... | . | . | . | . | |
AFNDT-3057TI | Custom 3 Step Thin Wedge with Holder. Step Thicknesses: 0.015", 0.030" and 0.070". Pad Size: 1.0" x 1.0" x 3.0" Total Length. Step ThicknessTolerence +/- .001. Material: 6AL-4V Titanium Also Contains 2 EDM Flaws .010" and .020" Deep x .005" Wide x .30... | . | . | . | . | |
AFNDT-3058/INC | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .5mm, 1.0mm, 2.0mm x (.006"Wide +/- .001). MATERIAL: 718 Inconel. SIZE: 1.0" Wide x 4.0" Long x 0.25" Thick. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3059 | Custom Eddy Current 2 Hole Calibration Standard per Customer Supplied Drawing. Material: 7050-T7451. Hole Sizes: .516"Ø and .812"Ø with a total of 4 EDM Notches 0.021" x 0.021" x .004" Wide Max. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3060 | Custom Eddy Current 2 Hole Calibration Standard per Customer Supplied Drawing. Material: 7050-T7451. Hole Sizes: .252"Ø and .516"Ø with a total of 4 EDM Notches 0.021" x 0.021" x .004" Wide Max. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3061AL | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005", .010", .020" (.004"W +/- .002), 7075-T7 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3062/13-8PH | 8 STEP CALIBRATION BLOCK, PAD SIZE 1.0" x1.0", STEP SIZE: .250", .400", .600", .800", 1.00" +/- .010" 13-8PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3062/15-5PH | 5 STEP CALIBRATION BLOCK, PAD SIZE 1.0" x1.0", STEP SIZE: .250", .400", .600", .800", 1.00" +/- .010" 15-5PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3062/17-4PH | 5 STEP CALIBRATION BLOCK, PAD SIZE 1.0" x1.0", STEP SIZE: .250", .400", .600", .800", 1.00" +/- .010" 17-4PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3063/13-8PH | 5 STEP CALIBRATION BLOCK, INCLUDES ACETAL(DELRIN) HOLDING BLOCK. PAD SIZE 1.0" x1.0", STEP SIZE: .020", .040", .060", .080", .100", .150, .200, .300 +/- .010" 13-8PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3063/15-5PH | 8 STEP CALIBRATION BLOCK, INCLUDES ACETAL(DELRIN) HOLDING BLOCK. PAD SIZE 1.0" x1.0", STEP SIZE: .020", .040", .060", .080", .100", .150, .200, .300 +/- .010" 15-5PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | ||||
AFNDT-3063/17-4PH | 8 STEP CALIBRATION BLOCK, INCLUDES ACETAL(DELRIN) HOLDING BLOCK. PAD SIZE 1.0" x1.0", STEP SIZE: .020", .040", .060", .080", .100", .150, .200, .300 +/- .010" 17-4PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3064/2024AL | 7 STEP REFERENCE BLOCK WITH ACETAL( DELRIN ) HOLDING BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 2024-T3 ALUMINUM. STEP RANGE:.020", .040", .060", .080", .100", .150", .200" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3064/6061AL | 7 STEP REFERENCE BLOCK WITH ACETAL( DELRIN ) HOLDING BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 6061-T6 ALUMINUM. STEP RANGE:.020", .040", .060", .080", .100", .150", .200" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3064/7075AL | 7 STEP REFERENCE BLOCK WITH ACETAL( DELRIN ) HOLDING BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 7075-T6 ALUMINUM. STEP RANGE:.020", .040", .060", .080", .100", .150", .200" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3065/2024AL | 6 STEP REFERENCE BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 2024-T3 ALUMINUM. STEP RANGE:.100", .250", .400", .600", .800", 1.00" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3065/6061AL | 6 STEP REFERENCE BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 6061-T6 ALUMINUM. STEP RANGE:.100", .250", .400", .600", .800", 1.00" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3065/7075AL | 6 STEP REFERENCE BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 7075-T6 ALUMINUM. STEP RANGE:.100", .250", .400", .600", .800", 1.00" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3066/4130 | 5 STEP REFERENCE BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 4130 STEEL. STEP RANGE: .200", .400", .600", .800", 1.00" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3066/6AL4V | 5 STEP REFERENCE BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 6AL-4V TITANIUM. STEP RANGE: .200", .400", .600", .800", 1.00" +/- .002". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3067/6AL4V | 8 STEP CALIBRATION BLOCK, INCLUDES ACETAL(DELRIN) HOLDING BLOCK. PAD SIZE 1.0" x1.0", STEP SIZE: .015", .030", .050", .080", .120", .160, .200, .300 +/- .005" 15-5PH STAINLESS STEEL. Includes certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3068/4130 | 7 STEP REFERENCE BLOCK WITH ACETAL( DELRIN ) HOLDING BLOCK. STEP PAD SIZE: 1.0" X 1.0". MATERIAL: 4130 STEEL. STEP RANGE:.020", .050", .080", .120", .160", .200", .300" +/- .010". Includes certification report traceable to NIST. | . | . | . | . | |
AFNDT-3070/7475 | 6 STEP THICKNESS STANDARD. STEP SIZES: .030", .050", .100", .150", .300", .500" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 7475-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3070AL | 6 STEP THICKNESS STANDARD. STEP SIZES: .030", .050", .100", .150", .300", .500" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | TRS-6-10A7075-T6 | U8862594 | . | . | |
AFNDT-3071 | Custom designed eddy current multi-layer aircraft aluminum skin test specimen, drawing 2, sheets 1-4. reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3072 | Custom designed eddy current aircraft calibration standard, Drawing 3, Sheets 1-3, for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3073 TYPE 1 | Custom designed eddy current reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3073 TYPE 2 | Custom designed eddy current reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3073 TYPE 3 | Custom designed eddy current reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3074AL | 12 Hole reference standard. Material: 2024-T3 Aluminum. Contains 12 hole sizes; 3/16 inch (4.74mm) 7/32 inch (5.53mm) 1/4 inch (6.35mm) 9/32 inch (7.13mm) 5/16 inch (7.92mm) 11/32 inch (8.71mm) 3/8 inch (9.52mm) 7/16 inch (11.09mm) 1/2 inch (12.7mm) 9/16 inch (14.27mm) 5/8 inch (15.87mm) 3/4 inch (19.05mm); Each hole contains 0.030 x 0.030 (+/-10%) corner EDM notch and a .040" Long x .020" Deep x .005" Wide Mid-Wall EDM Notch. Includes Test Report and Certificate of Conformance. | RM12-C30M20-2024T3 | . | . | . | |
AFNDT-3076AL | 7 STEP WEDGE, STEP SIZES OF .120", .150", .200", .250", .300", .350", and .400" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 2024-T3 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-2024T3-.120/.400 | . | . | . | |
AFNDT-3076AL-1 | 7 STEP WEDGE, STEP SIZES OF .120", .150", .200", .250", .300", .350", and .400" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 7075-T7 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-7075T7-.120/.400 | . | . | . | |
AFNDT-3076AL-2 | 7 STEP WEDGE, STEP SIZES OF .120", .150", .200", .250", .300", .350", and .400" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 7050-T7 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-7050T7-.120/.400 | . | . | . | |
AFNDT-3077AL | 7 STEP WEDGE, STEP SIZES OF .450", .500", .550", .600", .650", .700", and .750" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 2024-T3 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-2024T3-.450/.750 | . | . | ||
AFNDT-3077AL-1 | 7 STEP WEDGE, STEP SIZES OF .450", .500", .550", .600", .650", .700", and .750" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 7075-T7 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-7075T7-.450/.750 | . | . | . | |
AFNDT-3077AL-2 | 7 STEP WEDGE, STEP SIZES OF .450", .500", .550", .600", .650", .700", and .750" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 7050-T7 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-7050T7-.450/.750 | . | . | . | |
AFNDT-3078AL | 7 STEP WEDGE, STEP SIZES OF .800", .850", .900", .950", 1.00", 1.50", and 2.00" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 2024-T3 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT7-2024T3-.800/2.0 | . | . | . | |
AFNDT-3079AL | 9 STEP WEDGE, STEP SIZES OF: .020", .030", .040", .050", .060", .070", .080", .090" and .100" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 7075-T7 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT9-7075T7-.020/.100 | . | . | . | |
AFNDT-3079AL-1 | 9 STEP WEDGE, STEP SIZES OF: .020", .030", .040", .050", .060", .070", .080", .090" and .100" +/- .001". PAD SIZE: 1.0" x 1.0", MATERIAL: 7050-T7 ALUMINUM. CLEAR ANODIZED FOR CORROSION PROTECTION. Includes Test Report and Certificate of Conformance. | RT9-7050T7-.020/.100 | . | . | . | |
AFNDT-3080 | UT Flawed Specimen Set - Carbon Steel | FS-CS-01 | . | . | . | |
AFNDT-3081AL | 3 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM.. HOLE SIZES: 5/16", 3/8", 7/16" TOTAL OF 3 EDM CORNER NOTCHES .030" x .030". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3082 | MT Flawed Specimen Set - Carbon Steel | FS-CS-03 | . | . | . | |
AFNDT-3083/2205 | 5 STEP WEDGE 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 20mm x 20mm. Material: 2205 Duplex Stainless Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3083SS | 5 STEP WEDGE 2.5mm, 5.0mm,7.5mm, 10.0mm, 12.5mm +/- 0.05mm, Pad Size: 20mm x 20mm. Material: 304 Stainless Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3084AL | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: AMS4144 2219-T851 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001. Clear Anodized for corrosion protection. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-30CTI | REFERENCE STANDARD, 30 CORNER NOTCHES, 12" X 4" , 6AL-4V TI | . | . | |||
AFNDT-3100/2024 | CUSTOM THICKNESS STANDARD, 2024-T3 or 2024-T4 ALUMINUM. SIZE: 50mm X 50mm X 10mm +/- 1mm or 1.97" x 1.97" x .397" +/- .039". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3100/304 | CUSTOM THICKNESS STANDARD, 304 STAINLESS STEEL. SIZE: 50mm X 50mm X 10mm +/- 1mm or 1.97" x 1.97" x .397" +/- .039". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3100/6061 | CUSTOM THICKNESS STANDARD, 6061-T3 or 6061-T4 ALUMINUM. SIZE: 50mm X 50mm X 10mm +/- 1mm or 1.97" x 1.97" x .397" +/- .039". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3100/7075 | CUSTOM THICKNESS STANDARD, 7075-T6 or 7075-T7 ALUMINUM. SIZE: 50mm X 50mm X 10mm +/- 1mm or 1.97" x 1.97" x .397" +/- .039". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3100/TI | CUSTOM THICKNESS STANDARD, 6-2-4-2 TITANIUM. SIZE: 50mm X 50mm X 10mm +/- 1mm or 1.97" x 1.97" x .397" +/- .039". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3100/WAS25 | CUSTOM THICKNESS STANDARD, WASPALOY 25. SIZE: 50mm X 50mm X 10mm +/- 1mm or 1.97" x 1.97" x .397" +/- .039". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3101 | Thin Material Step Wedge: 7075-T6 Aluminium, 5 Steps total (0.5mm, 1.00mm, 1.5mm, 2.00mm and 2.5mm). Step pad size: 20mm x 20mm. Anodized. Includes Test Report and Certificate of Conformance. | 10183 | . | . | . | |
AFNDT-3102AL/7075 | 9 STEP WEDGE .500", .625",. 750", .875", 1.0" , 1.125", 1.250", 1.375", 1.50". MATERIAL: 7075-T6 ALUMINUM WITH GRAIN DIRECTION. STEP PAD SIZE: 1.0" x 1.0". TOLERANCE = +/- .001. Includes Test Report and Certificate of Conformance | RT9-7075T6-.5/1.5 | . | . | . | |
AFNDT-3104 | The VMA.01-0-07 reference standard is ..3 ½” long x 3.0” wide x 1/4” thick...• The tapered notch on both standards is 0.080” deep at the edge of the standard and tapers to 0.000” deep...• The tapered notch has scribe marks every 0.010” deep from 0.000”... | VMA.01-0-07 | . | . | . | |
AFNDT-3105CS | 5 STEP WEDGE 12.5mm, 15.0mm,17.5mm, 20.0mm, 25.0mm +/- 0.05mm, Pad Size: 19mm x 19mm. Material: 1018 Carbon Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3106TI | 7 STEP CALIBRATION BLOCK. MATERIAL: 6AL-4V TITANIUM. STEP THICKNESS: 0.035", 0.070", 0.105", 0.140", 0.175", .210" 0.250" +/- .001". STEP PAD SIZE: .75" x .75". Includes certification Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3108CS | CUSTOM 7 STEP BLOCK, 0.5mm, 1mm,2mm, 3mm, 4mm, 5mm, 6mm +/- .05mm . Pad Size: .750" x .750" Material- 4340 Carbon Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3108TI | CUSTOM 7 STEP BLOCK, 0.5mm, 1mm,2mm, 3mm, 4mm, 5mm, 6mm +/- .05mm . Pad Size: .750" x .750" Material- 6AL-4V Titaniuml. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3110A | Custom Multi-Hole Standard made to the Specifications of 99A53003001101. Material: 2024-T351. 48 Total Hole Sizes: 33/64, 17/32, 35/64, 9/16, 37/64, 19/32, 39/64, 5/8, 41/64, 21/32,43/64, 11/16. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3110B | Custom Multi-Hole Standard made to the Specifications of 99A53003001101. Material: 2024-T351. 36 Total Hole Sizes: 45/64, 23/32, 47/64, 3/4, 49/64, 25/32, 51/64, 13/16, 53/64. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3110C | Custom Multi-Hole Standard made to the Specifications of 99A53003001101. Material: 2024-T351. 24 Total Hole Sizes: 27/32, 55/64, 7/8, 57/64, 29/32, 59/64. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3110D | Custom Multi-Hole Standard made to the Specifications of 99A53003001101. Material: 2024-T351. 20 Total Hole Sizes: 15/16, 61/64, 31/32, 63/64, 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3112 | Custom Bolt hole Standard, Hole Sizes; 1/8", 5/32", 3/16", 1/4", inch diameter Holes. .020" Thru EDM notches .005" Wide(+/- .001"). Material: 2024-T3 Aluminum. Plate Size: 2.0" x 4.0" x 0.250". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3112/2014-T6 | Custom Bolt hole Standard, Hole Sizes; 1/8", 5/32", 3/16", 1/4", inch diameter Holes. .020" Thru EDM notches .005" Wide(+/- .001"). Material: 2014-T6 Aluminum. Plate Size: 2.0" x 5.0" x 0.250". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3112/2024-T6 | Custom Bolt hole Standard, Hole Sizes; 1/8", 5/32", 3/16", 1/4", inch diameter Holes. .020" Thru EDM notches .005" Wide(+/- .001"). Material: 2024-T6 Aluminum. Plate Size: 2.0" x 5.0" x 0.250". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3113 | Custom Bolt hole Standard, Hole Size; 5/8"Ø inch diameter Hole. .020" Thru EDM notch .005" Wide(+/- .001"). Material: 7075-T6 Aluminum. Plate Size: 2.0" x 2.0" x 0.250". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3114 | 16 HOLE REFERENCE STANDARD 6AL-4V TITANIUM. 2 OF EACH HOLE SIZES: 3/16", 13/64" 7/32" , 1/4", 17/64", 9/32", 7/16", 9/16". .030" x .030" CORNER NOTCH IN 1st HOLE SET and .060" x .020" MID-WALL NOTCH IN 2nd HOLE SET. Tolerance: .006" +/-.001". Includ... | . | . | . | . | |
AFNDT-3115 | 16 HOLE REFERENCE STANDARD 4340 CRES STEEL. 2 OF EACH HOLE SIZES: 3/16", 13/64" 7/32" , 1/4", 17/64", 9/32", 7/16", 9/16". .030" x .030" CORNER NOTCH IN 1st HOLE SET and .060" x .020" MID-WALL NOTCH IN 2nd HOLE SET. Tolerance: .006" +/-.001". Includ... | . | . | . | . | |
AFNDT-3116 | 16 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. 2 OF EACH HOLE SIZES: 3/16", 13/64" 7/32" , 1/4", 17/64", 9/32", 7/16", 9/16". .030" x .030" CORNER NOTCH IN 1st HOLE SET and .060" x .020" MID-WALL NOTCH IN 2nd HOLE SET. Tolerance: .006" +/-.001". Inclu... | . | . | . | . | |
AFNDT-3117/15-5PH | Custom EC 14 Hole Standard. Hole sizes: 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.EDM NOTCH: .050" x .050" CORNER NOTCH IN EACH HOLE. 3 SURFACE EDM NOTCHES .010", .020", .040" DEEP x .750" LONG.) Material: 15-5PH Stainless Steel. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3117/7075-T6 | Custom EC 14 Hole Standard. Hole sizes: 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.EDM NOTCH: .050" x .050" CORNER NOTCH IN EACH HOLE. 3 SURFACE EDM NOTCHES .010", .020", .040" DEEP x .750" LONG.) Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | RM140-C50-7075T6 | . | . | . | |
AFNDT-3117/TI | Custom EC 14 Hole Standard. Hole sizes: 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.EDM NOTCH: .050" x .050" CORNER NOTCH IN EACH HOLE. 3 SURFACE EDM NOTCHES .010", .020", .040" DEEP x .750" LONG.) Material: 6AL-4V Titanium. Includes Test Report and Certificate of Conformance. | RM140-C50-6AL4V | . | . | . | |
AFNDT-3118TI | 5 STEP WEDGE .100"(2.54mm), .200"(5.08mm),. 300"(7.62mm), .400"(10.16mm), .500"(12.7mm) MATERIAL: 6AL-4V TiTANIUM. PAD SIZE: 1.0" X 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3119AL | Aluminum Dynamic Split Hole Reference Block. Material: 7075-T651 aluminum. 16 Holes with 1/16" Cross Drilled Holes on both sides. Hole Sizes: 4.5mm, 5.0mm, 6.0mm, 6.5mm, 7.0mm, 7.5mm, 8.0mm, 9.0mm, 10mm, 12mm, 14mm, 16mm, 20mm, 22mm, 24mm. Tolerance +/... | . | . | . | . | |
AFNDT-3119TI | Titanium Dynamic Split Hole Reference Block. Material: 6Al-4v Titanium. 16 Holes with 1/16" Cross Drilled Holes on both sides. Hole Sizes: 4.5mm, 5.0mm, 6.0mm, 6.5mm, 7.0mm, 7.5mm, 8.0mm, 9.0mm, 10mm, 12mm, 14mm, 16mm, 20mm, 22mm, 24mm. Tolerance +/- .... | . | . | . | . | |
AFNDT-3120AL | 11 hole Reference Standard 7075-T6 Aluminum. Contains 10 hole sizes; 7/64, 1/8, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 5/8, 3/4 and 1.0 inch diameters.( .030X.030 Corner EDM Notch and 3 Surface EDM Notches at .010", .020", .040" DEEP x .750" LONG.) Includes T... | MHS-11-4A-0 | . | . | . | |
AFNDT-3121S | 10 hole Reference Standard 4340 or 4130 Carbon Steel. Contains 10 hole sizes; 1/8, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4 inch diameters.( .030" x .030" +/- 10% x .006" +/- .001" Wide Corner EDM Notch and 3 Surface EDM Notches at .010", .020", ... | MHS-10-1S-2 | . | . | . | |
AFNDT-3122T-0 | 10 hole Reference Standard 6AL-4v Titanium. Contains 10 hole sizes; 1/8, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4 inch diameters.( .030" x .030" +/- 10% x .006" +/- .001" Wide Corner EDM Notch and 3 Surface EDM Notches at .010", .020", .040" Dee... | MHS-10-1T-0 | . | . | . | |
AFNDT-3122T-4 | 10 hole Reference Standard 6AL-4v Titanium. Contains 10 hole sizes; 1/8, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4 inch diameters.( .050" x .050" +/- 10% x .006" +/- .001" Wide Corner EDM Notch and 3 Surface EDM Notches at .010", .020", .040" Dee... | MHS-10-1T-4 | . | . | . | |
AFNDT-3123AL | 7 STEP REFERENCE BLOCK ..STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 2024-T3 ALUMINUM. STEP RANGE:.030", .040", .050", .0600", .070", .080", .090" +/- .001". Includes certification report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3124/6061 | Custom Ultrasonic Calibration Block. Material: 6061 Al. Size: 6.0" x 1.5" x 5mm Thick. EDM slot depths 0.118"(0.3mm), .0197"(0.5mm), .0394"(1.0mm), .0787"(2.0mm), .0984"(2.5mm) x .005"W +/-.001"Wide. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3125AL | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) MATERIAL: 2024-T3 ALUMINUM. Includes Certification Repo... | . | , | . | . | |
AFNDT-3125CS | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.( .030X.030 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) MATERIAL: 4130 or 4340 CARBON STEEL. Includes Certificat... | . | . | . | . | |
AFNDT-3125SS | Contains 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters.( .030" X .030" CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) MATERIAL: 304 STAINLESS STEEL. Includes Certificatio... | . | . | . | . | |
AFNDT-3126CS | 12 hole sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters, .030" Deep Mid-bore EDM Notches .005"(+/- .001") wide and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.). Material: 4340 Carbon Steel. Incl... | . | . | . | . | |
AFNDT-3128AL | BOEING ALL AIRCRAFT MODELS 51-00-16 PT 6 FIG 3. MULTIHOLE STANDARD WITH 11 HOLES SIZES: 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.00". EDM NOTCHES: .020 x .020 X .005" +/-0.002 wide on one side and .030 x .030 .005" +/-0.002 wi... | . | . | . | . | |
AFNDT-3129CS | BOEING ALL AIRCRAFT MODELS 51-00-17 PT 6 FIG 3. MULTIHOLE STANDARD WITH 11 HOLES SIZES: 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.00". EDM NOTCHES: .030 x .030 .005" +/-0.002. MATERIAL: 4340 STEEL. Includes Test Report Traceab... | . | . | . | . | |
AFNDT-3130TI | BOEING ALL AIRCRAFT MODELS 51-00-14 PT 6 FIG 3. MULTIHOLE STANDARD WITH 11 HOLES SIZES: 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.00". EDM NOTCHES: .050 x .050(+/-.005") x .005" (+0.00/-.002). MATERIAL: 6AL-4V TITANIUM. Includ... | . | . | . | . | |
AFNDT-3131AL | 5 STEP WEDGE. STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 2024-T3 ALUMINUM. STEP RANGE: .100", .110", .120", .130", .140", +/- .001". Includes certification report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3132AL | 5 STEP WEDGE. STEP PAD SIZE: 1.0" X 1.0" MATERIAL: 2024-T3 ALUMINUM. STEP RANGE: .150", .160", .170", .180", .190", +/- .001". Includes certification report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3134AL | 8 STEP WEDGE, STEP SIZES OF .110", .120",.130", .140", .150", .160", .170", and .180" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3135AL | 7 STEP WEDGE, STEP SIZES OF .190", .200", .210", .220", .230", .240", and .250" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3136/2024T3 | 12 Hole Calibration Standard, Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 and .020 x .020 Corner EDM Notches in each Hole. Material: 2024-T3 Aluminum | RH120-C30C20-2024T3 | . | . | . | |
AFNDT-3136-7075T6 | 12 Hole Calibration Standard, Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 and .020 x .020 Corner EDM Notches in each Hole. Material: 7075-T6 Aluminum | RH120-C30C20-7075T6 | . | . | .. | |
AFNDT-3137AL | 14 Hole Calibration Standard, Hole Sizes; 1/8" 5/32", 3/16", 7/32", 1/4", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 11/16" and 3/4 inch diameters. ( .030 x .030 and .020 x .020 Corner EDM Notches in each Hole Per Boeing B737 PT 6 51-00-00 Prodedure 16 Fig.3, 1 Surface EDM Notch .020" Deep X .750" Long .005" MAX Width. Material: 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3138MAG | 7 STEP REFERENCE BLOCK. MATERIAL: MAGNESIUM STEP PAD SIZE: .75" X .75". STEP RANGE:.040", .080", .160", .250", .300", .400", .500" +/- .001". Includes certification report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3139AL | 11 HOLE REFERENCE STANDARD in 7075-T6 Aluminum; Hole Sizes: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), With a .020" x .020" x .005" and a .030"x.030" x .005" +/-.002" Corner EDM Notch in each hole Per BOEING Proceedure 51-00-16 PT 6... | . | . | . | . | |
AFNDT-3139CS | 11 HOLE REFERENCE STANDARD in 4130 Carbon Steel; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16,5/8,11/16, 3/4), With a .020" x .020" x .005" and a .030"x.030" x .005" +/-.002" Corner EDM Notch in each hole Per BOEING Proceedure 51-00-16 PT 6... | . | . | . | . | |
AFNDT-3139TI | 11 HOLE REFERENCE STANDARD in 6AL-4V Titanium; Hole Sizes: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), With a .020" x .020" x .005" and a .030"x.030" x .005" +/-.002" Corner EDM Notch in each hole Per BOEING Proceedure 51-00-16 PT 6 ... | . | . | . | . | |
AFNDT-3140AL | 7 HOLE REFERENCE STANDARD in 7075-T6 Aluminum; Hole Sizes: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2), With a .020" x .020" x .005" and a .030"x.030" x .005" +/-.002" Corner EDM Notch in each hole Per BOEING Proceedure 51-00-16 PT 6 FIG 3, 14 Notches Tota... | . | . | . | . | |
AFNDT-3141AL | Custom McDonnell Douglas 12 bolt hole reference standard 7075-T6 Aluminum with a .060"L x .030Dx .005" max width mid-wall notch, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (.125, .156", .187", .250", .281", ..312", .375", .4... | . | . | . | . | |
AFNDT-3141AL-1 | Custom McDonnell Douglas 12 bolt hole reference standard 7075-T6 Aluminum with .005" max width through EDM notch in holes #1-#6 and a .060"L x .030"D x .005" max width mid-wall notch in holes #7-12, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (109",.125", .1406", .1562", .1718" .1874", .203", .2186", ..2342", .2498", .2654", .281" NDT 06-20-01 FIG.4. Sheet 1 Page 8. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3141AL-2 | Custom McDonnell Douglas 12 bolt hole reference standard 7075-T6 Aluminum with a .060"L x .030Dx .005" max width mid-wall notch, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (.2966, .3122", .3278", .3434", .359", ..3746", .3902", .4058", .4214", .437", .4526", .4682" NDT 06-20-01 FIG.4. Sheet 1 Page 8. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3142AL | CUSTOM 4 STEP REFERENCE BLOCK. MATERIAL: 7075-T6. STEP SIZE .0100",.400",.700", 1.00" +/-.001. PAD SIZE: 1"X4". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3143 | 5 STEP ACRYLIC WEDGE. STEP SIZES: .200", .300",. 400", .500", .600" MATERIAL: CAST ACRYLIC. PAD SIZE: 1.0" x 1.0" TOLEREANCE = +/- .002". Includes Certification and Certificate of Conformance. | . | . | . | . | |
AFNDT-3144AL | 7 STEP WEDGE, STEP SIZES OF .280", .350", .450", .550", .650", .750", and .850" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3145S | 12 HOLE REFERENCE STANDARD 4340 STEEL, 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", .020" x .005" +/-.001" THROUGH NOTCH ON EACH HOLE, A .030" x .030" x .005+/- .001" CORNER NOTCH IN EACH HOLE. SURFACE NOTCHES: .01... | . | . | . | . | |
AFNDT-3146AL | 12 hole Reference Standard. Hole sizes: 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters, .030" x .030" x .005" +/-.002" Wide Corner EDM Notches and .020" x .020" x .005" +/-.002" Wide Mid-Wall EDM Notches. Materia... | . | . | . | . | |
AFNDT-3147AL | 7 HOLE 100° COUNTERSINK REFERENCE STANDARD 2024-T3 ALUMINUM, PLATE SIZE: 3.0" x 2.5" x 3/8" . HOLE SIZES: 5/32", 3/16", 7/32",1/4", 5/16",3/8", 7/16". TOTAL OF 7 EDM NOTCHES .030" +0.002"/-0.002" Long x .007" Max Width Through the Depth of the Countersink. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3148AL | 13 HOLE REFERENCE STANDARD, 7075-T6 ALUMINUM. HOLE SIZES: 5/32", 3/16", 7/32", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8" & 1". THRU EDM NOTCHES IN EACH HOLE, Depth: 0.040" +/- 0.001 x Width : 0.005" + 0 - 0.002". Includes Certification R... | . | . | . | . | |
AFNDT-3149 | 5 STEP ACRYLIC WEDGE. STEP SIZES: .600", .700",. 800", .900", 1.00" MATERIAL: CAST ACRYLIC. PAD SIZE: 1.0" x 1.0" TOLEREANCE = +/- .002". Includes Certification and Certificate of Conformance. | . | . | . | . | |
AFNDT-3150CS | 4 STEP WEDGE .020, .030, .040, .050 +/-.001 4340 CARBON STEEL . PAD SIZE:75"x.75". Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3151AL | 10 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM, HOLE SIZES: 1/8, 5/32, 3/16, 7/32 ,1/4, 9/32, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4,,7/8,1.0" .030" x .030" CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .750"L x .010",.020",.040" DEEP. Includes Test Report a... | HRS-15A | . | . | . | |
AFNDT-3151AL | 15 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM, HOLE SIZES: 1/8, 5/32, 3/16, 7/32 ,1/4, 9/32, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4,,7/8,1.0" .030" x .030" CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .750"L x .010",.020",.040" DEEP. Includes Test Report and Certificate of Conformance. | HRS-15A | . | . | . | |
AFNDT-3152CS | 5 Step Wedge Manufactured in Accordance with ASTM E797/E797M-15.Step Sizes: .100", .200",. 350", .500", 1.000" MATERIAL: 1018 Carbon Steel. Pad Size: 0.750" X 0.750" TOLEREANCE = +/- .002. NICKEL PLATED CORROSION RESISTANT COATING. Includes measure... | . | . | . | . | |
AFNDT-3152SS | 5 Step Wedge Manufactured in Accordance with ASTM E797/E797M-15.Step Sizes: .100", .200",. 350", .500", 1.000" MATERIAL: 304 Stainless Steel. Pad Size: 0.750" X 0.750" TOLEREANCE = +/- .002. Includes measurement Certification for the .750" Block wi... | . | . | . | . | |
AFNDT-3153/7075T6 | 11 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 3/8, 7/16, 1/2, 9/16), WITH .050"x.050" .005±.001 CORNER EDM NOTCH IN EACH HOLE. | . | . | . | . | |
AFNDT-3154CS | Eddy Current Surface Standard Carbon Steel. 0.5mm, 1.0mm,2.0mm Deep x .15mm Wide +/- .05mm. Block Size: 5.0"(127mm)L x 2.0"(50.8mm)W x .25"(6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3154SS | Eddy Current Surface Standard 316 Steel. 0.5mm, 1.0mm,2.0mm Deep x .15mm Wide +/- .05mm. Block Size: 5.0"(127mm)L x 2.0"(50.8mm)W x .25"(6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3155AL | • Each standard is 6” long x 3” wide x 1/2” thick. Contains14 holes with diameters of: 1/8”, 5/32”, 3/16”, 7/32”, 1/4”, 9/32”, 5/16”, 11/32”, 3/8”, 7/16”, 1/2”, 9/16”, 5/8” & 3/4”..• Each hole contains a 0.050” x 0.050” corner notch at the bottom of th... | VM650CIT-3A | . | . | . | |
AFNDT-3156 | Tapered Aluminum Standard. Material: 2024-T351 Aluminum. Taper: 0.039"-0.164". Dimensions: 1" x 4" x .25". Slot width = 0.75". Includes Test Report. | SPO-4304 | U8860197 | 1916914 | . | |
AFNDT-3157 | Liquid Penetrant Standard. Meets the ASME Boiler Pressure Code, Section V & III, and MIL-I-23135-C. The cracked aluminum block is made from 2024 aluminum and is 3” x 2” x 3/8” thick. A 1/8" wide groove separates the blocks two sides to facilitate side-... | . | . | . | . | |
AFNDT-3158 | 3 HOLE REFERENCE STANDARD. MATERIAL: 4130 CRES STEEL. HOLE SIZES: 3/16, 1/4, 5/16 TOTAL OF 3 EDM THROUGH NOTCHES .020 DEEP x .006" WIDE. Includes Certification Report. | . | . | . | . | |
AFNDT-3159AL | 8 HOLE REFERENCE STANDARD, MATERIAL: 2024-T3 ALUMINUM., HOLE SIZES: 1/8", 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", .020" THROUGH NOTCH .005+/-.001. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3159AL | 8 HOLE REFERENCE STANDARD, MATERIAL: 2024-T3 ALUMINUM., HOLE SIZES: 1/8", 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", .020" THROUGH NOTCH .005+/-.001. Includes Test Report and Certificate of Conformance. | RH80-T20-2024T3 | . | . | . | |
AFNDT-3159TI | 8 HOLE REFERENCE STANDARD 6AL-4v TITANIU., HOLE SIZES: 1/8", 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", .020" THROUGH NOTCH .005+/-.001. Includes Test Report and Certificate of Conformance. | RH80-T20-T6AL4V | . | . | . | |
AFNDT-3160AL | BOMBARDIER EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), DEPTH TOLERANCE = +/- .001"(+/- .003mm). MATERIAL 2024-T3 ALUMINUM. SIZE: 1.5"W x 3.75"L x .25". Includes Test Report and Certificate of... | . | . | . | . | |
AFNDT-3160AL-1 | BOMBARDIER EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), DEPTH TOLERANCE = +/- .001"(+/- .003mm). MATERIAL 6061-T6 ALUMINUM, IACS 40.00-44.80. SIZE: 1.5"W x 3.75"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3160CS | BOMBARDIER EDDY CURRENT SURFACE REFERENECE STANDARD. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), DEPTH TOLERANCE = +/- .001"(+/- .003mm). MATERIAL 4130/4340 CRES STEEL. SIZE: 1.5"W x 3.75"L x .25". Includes Test Report and Certificat... | . | . | . | . | |
AFNDT-3161/321S | 6 STEP REFERENCE BLOCK WITH HOLDER. MATERIAL: 321 CRES STEEL. STEP SIZES: .008",.020",.050", .080", .100" , .125" +/-.005". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3161/INC | 6 STEP REFERENCE BLOCK WITH HOLDER. MATERIAL: INCONEL. STEP SIZES: .008",.020",.050", .080", .100" , .125" +/-.005". PAD SIZE = 1.0" x 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3162CS | 5 STEP WEDGE .200", .300", .400", .500", .600". TOLERANCE +/-.001". ..MATERIAL: 4340 or 4130 CARBON STEEL . PAD SIZE:75"x.75". Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3163CS | 8 STEP WEDGE, STEP SIZES: 0.35mm 1mm, 2mm, 3mm, 4mm, 5mm, 7mm, 9mm +/- .02mm. Material: 1018 Carbon Steel. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3164AL | Custom NDI standard for F-15C/D inspection. Material: 2124-T8 Aluminum. Includes Certification Report Traceable to NIST. | . | . | . | . | |
AFNDT-3165MG | 5 STEP WEDGE .050", .070", .090", .110", .130". TOLERANCE +/-.001". ..MATERIAL: MAGNESIUM. PAD SIZE:75"x.75". Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3166 | CUSTOM 2 HOLE REFERENCE STANDARD. MATERIAL: 718 INCONEL, BLOCK SIZE: .500" x 1.0" x 4.0" . HOLE SIZES: 5/16", 9/32" WITH -3( .030" x .060" x .005" W MID-WALL NOTCH ' | . | . | . | .. | |
AFNDT-3166AL | CUSTOM 13 HOLE REFERENCE 3 PLATE STANDARD, 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, 7/8, 1.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3167CS | CUSTOM HOLE REFERENCE STANDARD in 4130 OR 4340 STEEL; HOLE SIZES: 2 OF EACH SIZE HOLE FOR A TOTAL OF 4 HOLES. 2.5mm(.098"), ,3.5mm(.137") , WITH A .030"x.030" x .005" +/-.002" CORNER EDM NOTCH AND .020" x .005" THRU NOTCHES. | . | . | . | . | |
AFNDT-3168CS | Eddy Current Surface Calibration Standard.Alloy: 4340 Steel, bare..Size: .250” thick x 1.00” wide x 3.00” long.. - 0.05mm deep x 0.05mm wide (±0.025) x 1.00” long (full-width).. - 0.05mm deep x 0.05mm wide (±0.025) x 3mm long .... | . | . | . | . | |
AFNDT-3169 | 8 Step Wedge, Material: 2219 Aluminium per AMS4144.8 Steps: 0.5mm, 1mm, 2mm, 3mm, 4mm, 5mm, 7mm, 9mm. (Tolerance: ± 0.02mm). Pad Size: 15mm x 15mm (Tolerance: ± 0.5mm).Surface Finish: Ra 0.8 µm (32 µin.)max. Includes Test Report and Certificate of Conf... | . | . | . | . | |
AFNDT-3170AL | Thin Material Step Wedge: 7075-T6 Aluminium, 5 Steps total (0.5mm, 1.00mm, 1.5mm, 2.00mm and 2.5mm). Step pad size: 19mm x 19mm. Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
AFNDT-3171AL | 17 HOLE REFERENCE STANDARD 7075-T6 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 5/8, 11/16 and 3/4 diameters. Includes 15 Thru EDM Notches .040" +/- 10% x .005" +/- .001" Wide. Includes Test Report and Certificate ... | RM171-T40-7075 | . | . | . | |
AFNDT-3171AL-1 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .055", .063", .071", .080", .090", .100", .110", .115", .120" .125" +/-.001" Pad Size: .75" x 75" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3171CS | 17 HOLE REFERENCE STANDARD 4130/4340 Carbon Steel, 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 5/8, 11/16 and 3/4 diameters. Includes 15 Thru EDM Notches .040" +/- 10% x .005" +/- .001" Wide. Includes Test Report ... | RM171-T40-4130 | . | . | . | |
AFNDT-3171SS | 17 HOLE REFERENCE STANDARD 304 Stainless Steel, 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 5/8, 11/16 and 3/4 diameters. Includes 15 Thru EDM Notches .040" +/- 10% x .005" +/- .001" Wide. Includes Test Report and... | RM171-T40-303 | . | . | . | |
AFNDT-3172AL-1 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .012", .016", .020", .025", .032", .036", .040", .045", .050" .055" +/-.001" Pad Size: .75" x 75" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3172AL-2 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .012", .016", .020", .025", .032", .036", .040", .045", .050" .055" +/-.001" Pad Size: .75" x 75" . Material: 7075-T6 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3172CS | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .012", .016", .020", .025", .032", .036", .040", .045", .050" .055" +/-.001" Pad Size: .75" x 75" . Material: 4130 Carbon Steel. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3173AL-1 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .055", .063", .071", .080", .090", .100", .110", .115", .120" .125" +/-.001" Pad Size: .75" x 75" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | .. | |
AFNDT-3173AL-2 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .055", .063", .071", .080", .090", .100", .110", .115", .120" .125" +/-.001" Pad Size: .75" x 75" . Material: 7075-T6 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3173CS | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .055", .063", .071", .080", .090", .100", .110", .115", .120" .125" +/-.001" Pad Size: .75" x 75" . Material: 4130 Carbon Steel. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3174AL-1 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .125", .135", .145", .150", .160", .170", .180", .190", .200" .225" +/-.001" Pad Size: .75" x 75" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3174AL-2 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .125", .135", .145", .150", .160", .170", .180", .190", .200" .225" +/-.001" Pad Size: .75" x 75" . Material: 7075-T6 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3174CS | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .125", .135", .145", .150", .160", .170", .180", .190", .200" .225" +/-.001" Pad Size: .75" x 75" . Material: 4340M Carbon Steel. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3175AL | 8 Step Calibration Block, Material 7075-T6 Aluminum. Steps: 0.5mm, 1mm, 2mm, 3mm, 4mm, 5mm, 7mm, 9mm. (Tolerance: +/-0.02mm)...- Pad Size: 19mm x 19mm (Tolerance: +/- 0.5mm)...- Surface Finish: Ra 0.8 µm (32 µin) max...- Includes Certification Report a... | . | . | . | . | |
AFNDT-3175CS | 8 Step Calibration Block, Material 1018 Steel. Steps: 0.5mm, 1mm, 2mm, 3mm, 4mm, 5mm, 7mm, 9mm. (Tolerance: +/-0.02mm)...- Pad Size: 19mm x 19mm (Tolerance: +/- 0.5mm)...- Surface Finish: Ra 0.8 µm (32 µin) max...- Includes Certification Report and Cer... | . | . | . | . | |
AFNDT-3175TI | 8 Step Calibration Block, Material 6AL-4V Titanium. Steps: 0.5mm, 1mm, 2mm, 3mm, 4mm, 5mm, 7mm, 9mm. (Tolerance: +/-0.02mm)...- Pad Size: 19mm x 19mm (Tolerance: +/- 0.5mm)...- Surface Finish: Ra 0.8 µm (32 µin) max...- Includes Certification Report an... | . | . | . | . | |
AFNDT-3176AL-1 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .250", .300", .350", .400", .500", .600", .700", .800", .900" 1.000" +/-.001" Pad Size: .75" x 75" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3176AL-2 | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .250", .300", .350", .400", .500", .600", .700", .800", .900" 1.000" +/-.001" Pad Size: .75" x 75" . Material: 7075-T6 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3177AL | BOMBARDIER 10 STEP ALUMINUM WEDGE, PT 4 FIG. 2 PAGE 8. STEP THICKNESSES:, .024", .028", .031", .035", .039", .044", .048", .052", .056" .059" X.XXX +/-0.002, X.XX +/-0.010". PAD SIZE: 1.0" x 1.0", Material: 2024-T3 Aluminum. Chromic anodize and 1 coat of CMS 565-01 primer on chem mill side only. Chemical mill from stock thickness 0.063” (1.60 Includes certification Report Traceable to NIST and Certificate of Conformance(COC). | . | . | . | . | |
AFNDT-3178AL | Contains 12 hole sizes: 3mm, 5mm, 7mm, 9mm, 11mm, 13mm, 14mm,15mm, 16mm 17mm,18mm and 19mm diameters. (1mm x 1mm x 0.15mm ± 0.03mm) Corner EDM Notches. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3178AL-1 | Contains 12 hole sizes: 3mm, 5mm, 7mm, 9mm, 11mm, 13mm, 14mm,15mm, 16mm 17mm,18mm and 19mm diameters. (1mm x 1mm x 0.15mm ± 0.03mm) Corner EDM Notches. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3179AL | 100° Countersink Multi Hole Standard. Contains 12 hole sizes: 3mm, 5mm, 7mm, 9mm, 11mm, 13mm, 14mm,15mm, 16mm 17mm,18mm and 19mm diameters. (1mm x 1mm x 0.15mm ± 0.03mm) Corner EDM Notches. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3180 | 6 FLAT BOTTOM HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. Hole Sizes: 5/16", 3/8", 7/16", 1/2", 9/16", 5/8" .060" LONG X. 020" x DEEP x .005" WIDE +/- .001" WIDE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3181AL | 8 Step Calibration Block, Material 2024-T3 Aluminum. Step Sizes: 0.5mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 5.0mm, 7.5mm, 10mm. (Tolerance: +/-0.02mm).- Pad Size: 20mm x 20mm (Tolerance: +/- 0.5mm). Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3182AL | 5 STEP WEDGE. STEP SIZES: .040", .100", .150", .250", .350". TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM . PAD SIZE: .75" x .75" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3187AL | METRIC 10 STEP CALIBRATION BLOCK, 0.6mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm ± .05mm. Pad Size: 20mm X 20mm. Per Airbus Procedure A 51-10-04. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3187TI | METRIC 10 STEP CALIBRATION BLOCK, 0.6mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm ± .05mm. Pad Size: 20mm X 20mm. Material: 6AL-4V Titanium. Per Airbus Procedure A 51-10-04. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3188 | 6 STEP WEDGE, 625 INCONEL. PAD SIZE: .787" x .787". STEP SIZES: 0.015", 0.020", 0.040", 0.063", 0.071", 0.100" +/-.001 TOLERANCE. Includes Test Report ancd Certificate of Conformance. | . | . | . | . | |
AFNDT-3189AL | 11 HOLE REFERENCE STANDARD IN 2024-T3 ALUMINUM; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH .020" x .020" x .005" +/-.001" CORNER EDM NOTCH IN EACH HOLE. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3190AL | 7 STEP WEDGE. STEP SIZES: .030", .115", .200", .285", .370", .455", and .540" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | UT-CI-7S2024-C | . | . | . | |
AFNDT-3191AL | 7 STEP WEDGE. STEP SIZES: .030", .115", .200", .285", .370", .455", and .540" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | UT-CI-7S7075-C | . | . | . | |
AFNDT-3192AL | 10 STEP REFERENCE BLOCK .020", .040", .060", .080", .100", .120", .140", .160", .180", .200" +/-.001" 7075-T6 ALUMINUM .75" x .75" STEP PAD With Delrin Holding Block. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3193AL | 10 STEP REFERENCE BLOCK .020", .040", .060", .080", .100", .120", .140", .160", .180", .200" +/-.001" 2024-T3 ALUMINUM .75" x .75" STEP PAD With Delrin Holding Block. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3194TI | 10 STEP REFERENCE BLOCK .020", .040", .060", .080", .100", .120", .140", .160", .180", .200" +/-.001" 6AL-4V TITANIUM .75" x .75" STEP PAD With Delrin Holding Block. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3195S | 10 STEP REFERENCE BLOCK .020", .040", .060", .080", .100", .120", .140", .160", .180", .200" +/-.001" CARBON STEEL .75" x .75" STEP PAD With Delrin Holding Block. Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
AFNDT-3196AL | CUSTOM 4 STEP WEDGE. MATERIAL: 7075-T6 ALUMINUM. STEP SIZES: .250",.500",.750", 1.000" +/-.001. PAD SIZE: .75" x .75". Includes Test Report Traceable to NIST. | . | . | . | . | |
AFNDT-3197AL | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8. HOLE SIZES: 1.000", 1.250" . Includes Test Report and Certificate of Conformance. | NDT1084 | . | . | . | |
AFNDT-3198TI | 10 HOLE REFERENCE STANDARD 6AL-4V Titanium.Hole Sizes: (3/16", 7/32" ,1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.005" +/-.002" WIDE & .020" X. 020" x.005" +/-.002" WIDE CORNER EDM NOTCH EACH HOLE and 3 SURFACE EDM NOTCHES .500... | . | . | . | .. | |
AFNDT-3199AL | 7 STEP REFERENCE BLOCK. STEP SIZES: .025",.040", .063", .071", .100",.125",.200" +/-.001". MATERIAL: 2024-T6 ALUMINUM. PAD SIZE: .75"x.75" .Includes Test Report and Certificate of Conformance | . | . | . | . | |
AFNDT-3200/321 | 7 STEP CALIBRATION BLOCK. STEP SIZES: .020", .040", .060", .080", .100", .150", and .200" +/- .010". PAD SIZE: 1.0" x 1.0", MATERIAL: 321 CRES. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3201/321SS | EDDY CURRENT SURFACE REFERENCE STANDARD, 321SS 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3201A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 11.3mm(.445")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA113C | . | . | . | |
AFNDT-3201CS | 4 STEP CALIBRATION BLOCK. STEP SIZES: .250", .500", .750", 1.00" ±.002, 3/4" X 3/4" PAD SIZE. MATERIAL: 1018 CARBON STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3202A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 14.3mm(.563")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA143C | . | . | . | |
AFNDT-3203A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 15.1mm(.594")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA151C | . | . | . | |
AFNDT-3204/4130 | 8 HOLE REFERENCE STANDARD IN 4130 CARBON STEEL; HOLE SIZES: (1/8, 5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2), WITH .020"x.020" CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3204/7075 | 8 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (1/8, 5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2), WITH .020"x.020" CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3204A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 15.9mm(.626")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA159C | . | . | . | |
AFNDT-3205A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 16.0mm(.630")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA160C | . | . | . | |
AFNDT-3206A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 16.3mm(.642")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA163C | . | . | . | |
AFNDT-3207A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 16.7mm(.657")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA167C | . | . | . | |
AFNDT-3207CS | 5 Step Block. Material: 1018 Steel. Steps: 0.45mm, 0.50mm, 1.0mm, 2.5mm, 5.0mm. Tolerance: ± 0.02mm. Pad Size: 15.0mm x 15.0mm. Tolerance: ± 0.5mm. Surface Finish: Ra 0.8 µm (32 µin.) max. Supplied with Delrin Holding Block. Includes Test Report and Certificate of Conformance. | .. | . | . | . | |
AFNDT-3208A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 17.5mm(.689")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA175C | . | . | . | |
AFNDT-3209A | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameter = 2 Holes 19.3mm(.760")Ø each. Hole 1 = No EDM Flaws, Hole 2 = .030" x .030" x .004" +/- .001" EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Co... | ATBRA193C | . | . | . | |
AFNDT-3210 | SURFACE REFERENCE STANDARD, ONE EDM NOTCH .030" Deep x .040" wide x .060 long ( +/- .002), MATERIAL: 2024-T3 ALUMINUM. SIZE: 2.0"L x 2.0"W x .25". Includes Test Report and Certificate of Conformance. | RS0824-2024T3 | . | . | . | |
AFNDT-3211 | ALUMINUM TO ALUMINUM BONDED STANDARD. MATERIAL: 2024-T3 ALUMINUM, .063"/.040" WITH A 1.0" DISBOND. SIZE: 4.0" X 4.0". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3212AL | 13 HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 23/32". EACH HOLE CONTAINS A CORNER EDM NOTCH 030" x .030" x Width : 0.005" +/- 0.002". Includes Certif... | . | . | . | . | |
AFNDT-3212ST | 13 HOLE REFERENCE STANDARD. MATERIAL: 4130 or 4340 CRES STEEL. HOLE SIZES: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 23/32". EACH HOLE CONTAINS A CORNER EDM NOTCH 030" x .030" x Width : 0.005" +/- 0.002". Includes... | . | . | . | . | |
AFNDT-3212TI | 13 HOLE REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 23/32". EACH HOLE CONTAINS A CORNER EDM NOTCH 030" x .030" x Width : 0.005" +/- 0.002". Includes Certifi... | . | . | . | . | |
AFNDT-3213AL | 2024-T3 Aluminum hole standard, hole diameter 5/32", notch type .030 x .030" Coner Notch". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3214AL | 10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.000" +/-.001" Pad Size: .75" x 75" . Material: 2024-T3 Aluminum. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3215AL | BOEING REFERENCE STANDARD. PT 6 51-0-00. 13 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 5/32", 3/16", 1/4", 7/32", 9/32" 5/16" , 11/32", 3/8" ,7/16", 1/2", 9/16", 5/8", 3/4". EACH HOLE CONTAINS A CORNER EDM NOTCH: 0.030" x 0.030" a... | . | . | . | . | |
AFNDT-3216/TI | 4 STEP WEDGE .125", .250", .500", .750". TOLERANCE +/-.001". MATERIAL: 6AL-4V TITANIUM. PAD SIZE: 750" x .750" . Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3217AL | BOEING REFERENCE STANDARD. PT 6 51-0-00. 29 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", ... | . | . | . | . | |
AFNDT-3218AL | CUSTOM HOLE STANDARD IN 2024-T351 ALUMINUM PER BOEING PART NUMBER NDT1084. EDM CORNER NOTCH SIZES: .020" x .020" x .005" +/- .002 " and .030" x .030" x .005" +/- .002" HOLE SIZES: 9/64,10/64,11/64,12/64,13/64, 14/64, 15/64, 16/64, 17/64, 18/64, 19/64... | NDT1084 | . | . | . | |
AFNDT-3219AL | CUSTOM HOLE STANDARD IN 2024-T351 ALUMINUM PER BOEING PART NUMBER NDT1084. EDM CORNER NOTCH SIZES: .020" x .020" x .005" +/- .002 " and .030" x .030" x .005" +/- .002" HOLE SIZES: 37/64,38/64,39/64,40/64,41/64, 42/64, 43/64, 44/64, 45/64, 46/64, 47/6... | NDT1084 | . | . | . | |
AFNDT-3220ST | CUSTOM HOLE STANDARD IN 4340 OR 4340M STEEL PER BOEING PART NUMBER NDT1084. EDM CORNER NOTCH SIZES: .030" x .030" x .005" +/- .002" HOLE SIZES: 9/64,10/64,11/64,12/64,13/64, 14/64, 15/64, 16/64, 17/64, 18/64, 19/64, 20/64, 21/64, 22/64, 23/64, 24/64, ... | NDT1083 | . | . | . | |
AFNDT-3221ST | CUSTOM HOLE STANDARD IN 4340 OR 4340M STEEL PER BOEING PART NUMBER NDT1083. EDM CORNER NOTCH SIZES: .030" x .030" x .005" +/- .002" HOLE SIZES: 37/64,38/64,39/64,40/64,41/64, 42/64, 43/64, 44/64, 45/64, 46/64, 47/64, 48/64, 49/64, 50/64, 51/64, 52/64... | NDT1083 | . | . | . | |
AFNDT-3222TI | CUSTOM HOLE STANDARD IN 6AL-4V TITANIUM PER BOEING PART NUMBER NDT1027. EDM CORNER NOTCH SIZES: .050" x .050" x .005" + 0.000 / - 0.002" HOLE SIZES:9/64,10/64,11/64,12/64,13/64, 14/64, 15/64, 16/64, 17/64, 18/64, 19/64, 20/64, 21/64, 22/64, 23/64, 24/... | NDT1027 | . | . | . | |
AFNDT-3223TI | CUSTOM HOLE STANDARD IN 6AL-4V TITANIUM PER BOEING PART NUMBER NDT1027. EDM CORNER NOTCH SIZES: .050" x .050" x .005" +0.000 / - 0.002" HOLE SIZES: 37/64,38/64,39/64,40/64,41/64, 42/64, 43/64, 44/64, 45/64, 46/64, 47/64, 48/64, 49/64, 50/64, 51/64, 5... | NDT1027 | . | . | . | |
AFNDT-3224TI | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005", .010", .020", .040", .060" (.005"W +/- .002, MAX .007"). MATERIAL: 6AL-4v TITANIUM@2.2IACS. SIZE: 1.0"W x 6.0"L x .500". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3225AL | 12 HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .004" +/- .002" WIDE THROUGH EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010"... | VM89A-1 | . | . | . | |
AFNDT-3225I | 12 HOLE REFERENCE STANDARD. MATERIAL: 718 INCONEL.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .004" +/- .002" WIDE THROUGH EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020... | VM89I-1 | . | . | . | |
AFNDT-3225S | 12 HOLE REFERENCE STANDARD. MATERIAL: 4130 or 4340 CRES STEEL. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .004" +/- .002" WIDE THROUGH EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LON... | VM89S-1 | . | . | . | |
AFNDT-3225TI | 12 HOLE REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM.Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .004" +/- .002" WIDE THROUGH EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", ... | VM89T-1 | . | . | . | |
AFNDT-3226AL | Custom Metric 6 Step Block. Step Thicknesses of 2mm, 4mm, 6mm, 8mm, 10mm, 12.5mm. (Tolerance: +/- 0.02mm). Pad Size: 20mm x 20mm. Material: 7075-T6 ALUMINUM. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-3227/7175 | Custom Metric 7 Step Block. Step Thicknesses of 12.5mm, 14mm, 16mm, 18mm, 20mm, 22.mm, 25mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm x 19mm. Material: 7175-T73 ALUMINUM. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-3227AL | Custom Metric 7 Step Block. Step Thicknesses of 12.5mm, 14mm, 16mm, 18mm, 20mm, 22.mm, 25mm. (Tolerance: +/- 0.02mm). Pad Size: 19mm x 19mm. Material: 7075-T6 ALUMINUM. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-3228AL-1 | 8 STEP WEDGE, 0.5mm, 1.0mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, +/- .05mm. Material: 2024-T3 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3228AL-2 | 8 STEP WEDGE, 0.5mm, 1.0mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3229AL | BOEING REFERENCE STANDARD. PT 6 51-0-00. 13 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 3/16", 1/4", 7/32", 9/32" 5/16" , 11/32", 3/8" ,7/16", 1/2", 9/16", 5/8", 3/4". EACH HOLE CONTAINS A CORNER EDM NOTCH: 0.030" x 0.030" and 0.02... | . | . | . | . | |
AFNDT-3230A | Custom Bolt Hole Calibration Block, 2024-T3 Aluminum. Hole Diameter 5/16" (.312")Ø Contains one EDM Corner Notch .050" x .050" +/- .001", and one EDM Surface Notch .750" long x .020 deep +/- .001 . Block Size = 2.0" x 2.0" x .25". Includes Test Rep... | . | . | . | . | |
AFNDT-3231 | Custom McDonnell Douglas Low Frequency Eddy Current reference standard, 06-20-01 Figure 9 sheets 1-4. Material: 2024-T3 or 7075-T6 Aluminum. Fasteners: (NAS1097AD6-5 & BACB30NW6K3). Includes Test Report and Certificate of Confromance. | . | . | . | . | |
AFNDT-3231-1 | Custom McDonnell Douglas Low Frequency Eddy Current reference standard, 06-20-01 Figure 9 sheets 1-4. Material: 2024-T3 or 7075-T6 Aluminum.Fasteners: (CR3223-5 & MS21141-5). Includes Test Report and Certificate of Confromance. | . | . | . | . | |
AFNDT-3232F | Custom Hole Standard 2.0" x 2.0" x .25" Square. Material: Forged Aluminum. Hole Size: 16.5mm. EDM Corner Notch: .05mm x .05mm x .1mm Wide +/- 0.05mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3233F | Custom Eddy Current Surface Standard. Size: 80mm x 35mm x 7mm. Material: Forged Aluminum. EDM Notch: .060" Long x .004" Wide x .030" Deep +/- 0.002". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3235 | BOEING REFERENCE STANDARD PT 6 32-11-11. 4340M. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3236CS | Custom Thin 4-Step Calibration Block, 1018 Carbon Steel (0.040, 0.060, 0.080 and 0.100"). Includes Test Report and Certificate of Conformance. | UT-RC-4-TS-CS | . | . | . | |
AFNDT-3236SS | Custom Thin 4-Step Calibration Block, 304 Stainless Steel (0.040, 0.060, 0.080 and 0.100"). Includes Test Report and Certificate of Conformance. | UT-RC-4-TS-SS | . | . | . | |
AFNDT-3237AL | Custom Thin 8-Step Calibration Block, 7075 Aluminum (.030, .040, .050, .060, .070, .080, .090 .100"). Includes Test Report and Certificate of Conformance. | UT-RC-8-TS-AL | . | . | . | |
AFNDT-3238AL | Contains 13 hole sizes; 1/8, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. EDM: ( .030 X .030 X .005 +/- .002) CORNER NOTCH and ( .020 X .005 +/- .002) THRU NOTCH. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | MHS-13-8A-2 | . | . | . | |
AFNDT-3239AL | 3 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM. HOLE SIZES: 1/4", 5/16", 3/8" TOTAL OF 3 EDM CORNER NOTCHES .030" x .030". 3 EDM SURFACE NOTCHES 0.008", 0.020", 0.040". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3240AL | Aluminum multi-hole reference standard. Contains 5 hole sizes; 1/8, 5/32, 3/16, 7/32 and 1/4" inch hole diameters.( .030" x.030" corner EDM notch in each hole). Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3241AL | Aluminum Multi-hole reference standard. Material: 7075-T6 Aluminum. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains on the top layer contains Corner EDM corner notches; 0.030" x 0.030" x .005" +/- .001". The Middle layer contains 0.060" x 0.030" x .005" +/-.001" Mid -Bore Notch. The third layer contains a .020" x 0.020" x .005" +/-.001" Corner EDM notch. Includes Test Certificate traceable to NIST and Certificate of Conformance (COC). | . | . | . | . | |
AFNDT-3243AL | 8 STEP WEDGE, 2mm, 4mm, 6mm, 8mm, 10mm, 12mm, 14mm, 16mm +/- .05mm. Material: 2024-T3 Aluminum. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3244AL | 8 STEP WEDGE, 2mm, 4mm, 6mm, 8mm, 10mm, 12mm, 14mm, 16mm +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3245AL | 8 STEP WEDGE, 14mm, 16mm, 18mm, 20mm, 22mm, 24mm, 26mm, 28mm +/- .05mm. Material: 2024-T3 Aluminum. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3246AL | 8 STEP WEDGE, 14mm, 16mm, 18mm, 20mm, 22mm, 24mm, 26mm, 28mm +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3247AL-1 | 8 STEP WEDGE, 1mm (.0394), 3mm (.1181), 5mm (.1968), 8mm (.3149), 10mm (.3937), 15mm (.5905), 20mm (.7874), 25mm (.9842) +/- .01mm. Material: 7075-T6 Aluminum. Material Thickness: .984, Steps: .984x.984, Length: 7.874 Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3248AL | Custom Metric 6 Step Block. Step Thicknesses of 0.4mm, 0.7mm, 1.0mm, 1.3mm, 1.6mm, 2.0mm. (Tolerance: +/- 0.05mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3250/2024T3 | 12 Hole Calibration Standard, Hole Sizes; 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" inch diameters. ( .030 x .030 Corner and .020 x .020 Midwall EDM Notches in each Hole. Material: 2024-T3 Aluminum | RH12-C30M20-2024T3 | ||||
AFNDT-3251AL | 12 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM. HOLE SIZES: 1/8", 3/16" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8",11/16", 3/4", 13/16" .030" x .030" CORNER NOTCH and .020" x .020" CORNER NOTCH IN EACH HOLE. Tolerance: .005" +/-.001", 4 SURFACE EDM NOTCHES: .010", .020", .030" and .040" DEEP x .750" LONG. Inclludes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3251TI | 12 HOLE REFERENCE STANDARD 6AL-4V TITANIUM. HOLE SIZES: 1/8", 3/16" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8",11/16", 3/4", 13/16" .030" x .030" CORNER NOTCH and .020" x .020" CORNER NOTCH IN EACH HOLE. Tolerance: .005" +/-.001", 4 SURFACE EDM NOTCHES: .010", .020", .030" and .040" DEEP x .750" LONG. Inclludes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3252AL | 9 STEP THICKNESS STANDARD. STEP SIZES: .015", .025", .035", .045", .055", .065", .075", .085", .095" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 7075-T6 ALUMINUM.Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3252CS | 9 STEP THICKNESS STANDARD. STEP SIZES: .015", .025", .035", .045", .055", .065", .075", .085", .095" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 4340 or 4130 Carbon Steel.Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3252TI | 9 STEP THICKNESS STANDARD. STEP SIZES: .015", .025", .035", .045", .055", .065", .075", .085", .095" +/-.001". PAD SIZE 0.75" x 0.75". MATERIAL: 6AL-4V TITANIUM. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3253AL | 9 STEP WEDGE, 0.38mm, 0.64mm, 0.89mm, 1.14mm, 1.40mm, 1.65mm, 1.91mm, 2.16mm, 2.41mm +/- .05mm. Material: 7075-T6 Aluminum. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3253CS | 9 STEP WEDGE, 0.38mm, 0.64mm, 0.89mm, 1.14mm, 1.40mm, 1.65mm, 1.91mm, 2.16mm, 2.41mm +/- .05mm. Material: 4340 or 4130 Carbon Steel. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3253TI | 9 STEP WEDGE, 0.38mm, 0.64mm, 0.89mm, 1.14mm, 1.40mm, 1.65mm, 1.91mm, 2.16mm, 2.41mm +/- .05mm. Material: 6Al-4v Titanium. Pad Size: 19mm x 19mm square. Supplied with a PTFE Holding Block. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3254AL | Custom Bolt Hole Calibration Block, 7075-T651 Aluminum. Hole Diameters = 2 Holes 22.23mm(.875")Ø, and 25.4mm(1.0")Ø. EDM Flaws:.030" x .030" x .005" +/- .001" Corner EDM Notch. Block Size = 3.0" x 1.5" x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3255AL | 11 HOLE REFERENCE STANDARD in 7075-T6 Aluminum; Hole Sizes: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), With a .020" x .020" x .005" +/-.002" Corner EDM Notch in each hole. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3256/2024-T3 | 8 STEP WEDGE, 0.51mm (.020"), 0.64mm (.025"), 0.76mm (..030"), 0.91mm (.036"), 1.02mm (.040"), 1.14mm (.045"), 1.27mm (.050"), 1.42mm (.056") +/- .01mm. Material: 2024-T3 Aluminum. Step Pad Size: .25mm x .25mm, Overall Length: 7.874 Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3256/7075-T6 | 8 STEP WEDGE, 0.51mm (.020"), 0.64mm (.025"), 0.76mm (..030"), 0.91mm (.036"), 1.02mm (.040"), 1.14mm (.045"), 1.27mm (.050"), 1.42mm (.056") +/- .01mm. Material: 7075-T6 Aluminum. Step Pad Size: .25mm x .25mm, Overall Length: 7.874 Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3257/2024-T3 | 8 STEP WEDGE, 1.60mm (.063"), 1.80mm (.071"), 2.03mm (..080"), 2.31mm (.091"), 2.54mm (.100"), 3.0mm (.118"), 3.18mm (.125"), 3.56mm (.140") +/- .01mm. Material: 2024-T3 Aluminum. Step Pad Size: .25mm x .25mm, Overall Length: 7.874 Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3257/7075-T6 | 8 STEP WEDGE, 1.60mm (.063"), 1.80mm (.071"), 2.03mm (..080"), 2.31mm (.091"), 2.54mm (.100"), 3.0mm (.118"), 3.18mm (.125"), 3.56mm (.140") +/- .01mm. Material: 7075-T6 Aluminum. Step Pad Size: .25mm x .25mm, Overall Length: 7.874 Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3259/INC | 10 STEP WEDGE .008", .020", .050", .080", .000", .150", .220", .300", .400", .500" +/-.002" INCONEL 718 .75" x .75" STEP FACE | . | . | . | . | |
AFNDT-3260AL | Olympus Style Aluminum multi-hole reference standard. Contains 5 hole sizes; 2.0mm, 2.5mm, 3.0mm, 3.5 and 4.0mm hole diameters. EDM notch 0.5mm deep in each hole, length is half of the material thickness. Material: 7075-T76 Aluminum 15mm Thick. Includes Test Report and Certificate of Conformance Traceable to NIST. | . | . | . | . | |
AFNDT-3261AL | Olympus Style Aluminum multi-hole reference standard. Contains 11 hole sizes; 16.5mm, 17.0mm, 17.5mm, 18.0mm, 18.5mm, 19.0mm, 19.5mm, 20.0mm, 20.5mm, 21.0mm, and 21.5mm hole diameters. EDM notch = 0.5mm corner EDM notch and 0.5mm deep in each hole, length is half of the material thickness. Material: 7075-T76 Aluminum 15mm Thick. Includes Test Report and Certificate of ConformanceTraceable to NIST.. | . | . | . | . | |
AFNDT-3262TI | Olympus Style Aluminum multi-hole reference standard. Contains 21 hole sizes; 4.0mm, 4.5mm 5.0mm, 5.5mm, 6.0mm, 6.5mm, 7.0mm, 7.5mm, 8.0mm, 8.5mm, 9.0mm, 9.5mm, 10.0mm, 10.5mm, 11.0mm, 11.5mm, 12.0mm, 13.0mm, 14.0mm, 15.0mm and 16.0mm hole diameters. EDM notch = 0.5mm corner EDM notch and 0.5mm deep in each hole, length is half of the material thickness. Material: 6AL-4V Titanium 15mm Thick. Includes Test Report and Certificate of ConformanceTraceable to NIST.. | |||||
AFNDT-3262TI | Olympus Style Aluminum multi-hole reference standard. Contains 21 hole sizes; 4.0mm, 4.5mm 5.0mm, 5.5mm, 6.0mm, 6.5mm, 7.0mm, 7.5mm, 8.0mm, 8.5mm, 9.0mm, 9.5mm, 10.0mm, 10.5mm, 11.0mm, 11.5mm, 12.0mm, 13.0mm, 14.0mm, 15.0mm and 16.0mm hole diameters. EDM notch = 0.5mm corner EDM notch and 0.5mm deep in each hole, length is half of the material thickness. Material: 6AL-4V Titanium 15mm Thick. Includes Test Report and Certificate of ConformanceTraceable to NIST.. | . | . | . | . | |
AFNDT-3264 | Custom Reference Standard for the Boeing Lead Screw inspection, equivalent to 7903385. Material: 4150 Alloy Steel, 1.5 Outside Diameter and 1.069" Inside Diameter with 3 EDM Flaws per BSS 7048 page 2 Table 1. Includes Test Report and Certificate of Conformance. | 7903385 | . | . | ||
AFNDT-3265I | 6 Step Wedge .015", .020", .025", .030" ,0.035", 0.040" +/-.001", . Pad Size: 1.0" x 1.0". Material: 625 Inconel. Includes Certification. | . | . | . | . | |
AFNDT-3266I | 6 Step Wedge .050", .100", .200", .300" ,.400", .500" +/-.001", . Pad Size: 1.0" x 1.0". Material: 625 Inconel. Includes Certification. | . | . | . | . | |
AFNDT-3269AL | Custom Multi-Hole Standard manufactured to the Specifications of Airbus part number 99A53003001101. Material: 2024-T351. 8 Total Hole Sizes: 6.0mm, 7.0mm, 8.0mm, 9.0mm, 10.0mm, 11.0mm, 12.0mm, 13mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3270AL | Aluminum Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 x .005" (+/-.002) and 0.020 x 0.020 x .005" (+/-.002) corner EDM notch. Three Surface EDM Notches, 1.0" long: 0.010+0/-0.002, 0.010+0/-0.002, 0.020 ± 0.002. Material: 2024-T3 Aluminum Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3271AL | Aluminum Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 x .005" (+/-.002) and 0.020 x 0.020 x .005" (+/-.002) corner EDM notch. Three Surface EDM Notches, 1.0" long: 0.010+0/-0.002, 0.010+0/-0.002, 0.020 ± 0.002. Material: 2024-T3 Aluminum Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3272CS | Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 x .005" (+/-.002) corner EDM notch. Three Surface EDM Notches, 1.0" long: 0.010+0/-0.002, 0.010+0/-0.002, 0.020 ± 0.002. Material: 4340 Cres Steel Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3272SS | Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 x .005" (+/-.002) corner EDM notch. Three Surface EDM Notches, 1.0" long: 0.010+0/-0.002, 0.010+0/-0.002, 0.020 ± 0.002. Material: 303 Stainless Steel Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3273TI | Aluminum Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.050 x 0.050 x .005" (+/-.002) corner EDM notch. Three Surface EDM Notches, 1.0" long: 0.010+0/-0.002, 0.010+0/-0.002, 0.020 ± 0.002. Material: 6AL-4V Titanium Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3274SS | Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 x .005" (+/-.002) corner EDM notch. Three Surface EDM Notches, 1.0" long: 0.010+0/-0.002, 0.010+0/-0.002, 0.020 ± 0.002. Material: 301 1/2 Hard Stainless Steel Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3275 | Custom Metric 7 Step Block Per ASTM E797/E797M-15. Step Thicknesses of .50mm, 1.00mm, 2.00mm, 4.00mm, 6.00mm, 8.00mm, 10.00mm. (Tolerance: +/- 0.02mm). Pad Size: 20mm x 20mm. Material: 7075-T6 ALUMINUM. Includes Certification Report for step thickness, Anodizing and Certificate of Conformance. | . | . | . | . | |
AFNDT-3276 | Custom Metric 7 Step Block Per ASTM E797/E797M-15. Step Thicknesses of .50mm, 1.00mm, 2.00mm, 4.00mm, 6.00mm, 8.00mm, 10.00mm. (Tolerance: +/- 0.02mm). Pad Size: 20mm x 20mm. Material: 2024-T3 ALUMINUM. Includes Certification Report for step thickness, Anodizing and Certificate of Conformance. | . | . | . | . | |
AFNDT-3277 | Custom 2 Layer 12 Hole Calibration Standard, Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. 36 Total EDM Notches.1.) EDM Notch Specifications: .030 x .030 Corner EDM Notches in each Hole. 2.) Faying Surface EDM = .030 x .030 Corner EDM Notches in each Hole. 3.) Mid-Wall EDM Motches in Second Layer 0.060" x 0.030". Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3279/15-5PH | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .010", .020", .050" .007" ,MAX WIDTH, 15-5PH STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | SRS-125/15-5 | . | . | . | |
AFNDT-3279/Ti | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .010", .020", .050" .007" ,MAX WIDTH, 6AL-4V TITANIUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | SRS-125T | . | . | . | |
AFNDT-3280 | Surface reference standard, 4340 Steel, with EDM notch depths of 0.5mm", 1.0" and 2.0mm +/-1.3mm, Notch Width: .18mm Max. Depth: +/- .03mm. Reference standard overall dImensions 25.4mm X 101.6mm X 6.4mm). Includeds .020" thick shim and Key Ring. Supplied with Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3281 | 5 STEP WEDGE .100", .200",. 300", .400", .500" +/- .001. MATERIAL: 2219-T851 ALUMINUM. PAD SIZE: .75" L +/- .002 x .75" W +/- .005 TOLEREANCE. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3282 | Custom Metric 7 Step Block Per ASTM E797/E797M-15. Step Thicknesses of .50mm, 1.00mm, 2.00mm, 4.00mm, 6.00mm, 8.00mm, 10.00mm. (Thickness Tolerance: +/- 0.02mm). Pad Size: 20mm x 20mm.Width Tolerance ±1.0mm and Length Tolerance ± 0.5mm. Material: 15-5PH STEEL. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-3284SS | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005"(0.127mm), .010"(0.254mm), .020"(0.508mm), .050"(1.27mm) (.004"W +/- .001), 304 STAINLESS STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. REFERENCE P/N:29A049 | . | . | . | . | |
AFNDT-3285/17-4 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005"(0.127mm), .010"(0.254mm), .020"(0.508mm) (.004"W +/- .002). Material: 17-4PH Steel Condition to TH1050. SIZE: 1.0"W x 3.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3285/17-7 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005"(0.127mm), .010"(0.254mm), .020"(0.508mm) (.004"W +/- .002). Material: 17-7PH Steel Condition to TH1050. SIZE: 1.0"W x 3.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3285/304 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005"(0.127mm), .010"(0.254mm), .020"(0.508mm) (.004"W +/- .002). Material: Non-Magnetic 304 Stainless Steel. SIZE: 1.0"W x 3.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3286 | 12 HOLE REFERENCE STANDARD 7075-T6 (Hole Sizes 3/8", 7/16", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 15/16", 1.0", 1-1/8",) .020"x.020" and .030"x.030" x .005"W +/-.002" CORNER EDM NOTCH PER BOEING SPECIFICATION 747 PART 6 51-00-00 PAGE 8 FIGURE 3 | NDT1084 | . | . | . | |
AFNDT-3287AL | Custom multi-hole 100° countersink reference standard Material: 7075-T6 Aluminum. Hole sizes: 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2". Countersink holes opposite side. Thru hole EDM notches in each hole, .020" Deep x .005" Wide +/-.001". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3288AL | 5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: ASTM E 797 7075 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001. Clear Anodized for corrosion protection. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3289AL | Custom Metric 6 Step Block. Step Thicknesses of 1.0mm, 1.2mm, 1.4mm, and1.6mm. (Tolerance: +/- 0.02mm). Pad Size: 15mm X 15mm, (Tolerance: +/- 0.5mm) Material: 7075-T6 Aluminum with Delrin Holding Block. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3290AL | Custom ST Aerospace Engineering Multi-Hole Standard 2 Plate Assembly, Manufactured to the Customer Supplied Drawing Specifications . Material: 7075-T6 Aluminum. 6 Total Hole Sizes to be determined. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3291AL | BOMBARDIER 15 HOLE METRIC REFERENCE STANDARD. CL-215T PART 6 PAGE 8 FIGURE 5 GENERAL. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES: 4MM, 5MM, 6MM, 7MM, 8MM, 9MM, 10MM, 11MM, 12MM, 13MM, 14MM, 15MM, 16MM, 17MM, 18MM diameters. Includes 15 Thru EDM Notches 0.040 ± 0.001 Deep x .005" + 0.000/- 0.002" Wide. Includes certification Report Traceable to NIST and Certificate of Conformance(COC). | . | . | . | . | |
AFNDT-3291CS | BOMBARDIER 15 HOLE METRIC REFERENCE STANDARD. CL-215T PART 6 PAGE 8 FIGURE 5 GENERAL. MATERIAL: 4340 CARBON STEEL. HOLE SIZES: 4MM, 5MM, 6MM, 7MM, 8MM, 9MM, 10MM, 11MM, 12MM, 13MM, 14MM, 15MM, 16MM, 17MM, 18MM diameters. Includes 15 Thru EDM Notches 0.040 ± 0.001 Deep x .005" + 0.000/- 0.002" Wide. Includes certification Report Traceable to NIST and Certificate of Conformance(COC). | . | . | . | . | |
AFNDT-3292AL | CUSTOM 20 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .(1/8", 5/32",3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8",13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1"), MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3293/400 | 6 STEP WEDGE, .025", .050",. 100", .150", .200", 300" MATERIAL: MONEL 400. PAD SIZE: 1.50" X 1.50" TOLEREANCE = +/- .001. Includes Delrin Holding Block and Certification Report. | . | . | . | . | |
AFNDT-3293/625I | 6 STEP WEDGE, .025", .050",. 100", .150", .200", 300" MATERIAL: 625 inconel. PAD SIZE: 1.50" X 1.50" TOLEREANCE = +/- .001. Includes Delrin Holding Block and Certification Report. | . | . | . | . | |
AFNDT-3293/718I | 6 STEP WEDGE, .025", .050",. 100", .150", .200", 300" MATERIAL: 718 inconel. PAD SIZE: 1.50" X 1.50" TOLEREANCE = +/- .001. Includes Delrin Holding Block and Certification Report. | . | . | . | . | |
AFNDT-3294/718I | 6 STEP WEDGE, .050", .100", .150", .200", .250", 300" MATERIAL: 718 inconel. PAD SIZE: 1.50" X 1.50" TOLEREANCE = +/- .001. Includes Delrin Holding Block and Certification Report. | . | . | . | ||
AFNDT-3295 | CUSTOM HOLE STANDARD IN 4340 OR 4340M STEEL PER BOEING PART NUMBER NDT1083 PART 6 51-00-00 PROCEDURE 19. EDM CORNER NOTCH SIZES: .030" x .030" x .005" +/- .002". 13 HOLE SIZES: 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 17/32, 9/16. Includes Test Report and Certificate of Conformance. | NDT1083 | . | . | . | |
AFNDT-3296/316L | 12 Hole Calibration Standard, Hole Sizes; 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters, .020 x .005" ± .002" Thru EDM Notches in each Hole. Material: 316L Stainless Steel. Includes Test Report and Certificate of Conformance. | RH12-T20-316L | . | . | . | |
AFNDT-3297CS | Custom Metric 7 Step Block. Step Thicknesses of 2.5mm, 5.00mm, 5.05mm, 7.5mm, 7.55mm, 10.00mm, 10.05mm. (Thickness Tolerance: +/- 0.02mm). Pad Size: 20mm x 20mm, (Tolerance: ± 0.5mm) Material: 1018 Steel. Includes Certification Report for step thickness and Certificate of Conformance. | . | . | . | . | |
AFNDT-3298CS | 10 STEP CARBON STEEL WEDGE. STEP THICKNESS OF: 100", .310", 520", 730", .940", 1.150", 1.360", 1.570", 1.780" 2.00" +/-.001". Pad Size: 1.00" x 1.00" . Material: 1018 Carbon Steel. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3299/4340 | 12 HOLE REFERENCE STANDARD . HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .002" WIDE MID-WALL EDM NOTCH. Material: 4340 Steel. Includes Test Report and Certificate of Conformance. | RH121-M20-4340 | . | . | . | |
AFNDT-3299/6AL-4V | 12 HOLE REFERENCE STANDARD . HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .002" WIDE MID-WALL EDM NOTCH. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3299/7075-T6 | 12 HOLE REFERENCE STANDARD . HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .002" WIDE MID-WALL EDM NOTCH. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | RH121-M20-7075T6 | . | . | . | |
AFNDT-3301/2024-T3 | 8 STEP WEDGE, Step Sizes: 0.6mm,1.2mm,1.4mm,1.6mm,1.8mm, 2.0mm,2.2mm,2.4mm; MATERIAL: 2024-T3 ALUMINUM. LENGTH: 20mm Wide x 28mm Long for the first and last step. 20mm x 20mm long for the 6 inside steps. Total Length=176mm Long. TOLERANCE = +/- 0.05mm. Supplied with Holder. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3301/7075-T6 | 8 STEP WEDGE, Step Sizes: 0.6mm,1.2mm,1.4mm,1.6mm,1.8mm, 2.0mm,2.2mm,2.4mm; MATERIAL: 7075-T6 ALUMINUM. LENGTH: 20mm Wide x 28mm Long for the first and last step. 20mm x 20mm long for the 6 inside steps. Total Length=176mm Long. TOLERANCE = +/- 0.05mm. Supplied with Holder. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3302//7075-T6 | 8 STEP WEDGE:3.0mm,3.5mm, 4.0mm, 4.5mm, 5.0mm, 5.5mm,6.0mm,7.0mm; MATERIAL: 7075-T6 ALUMINUM. LENGTH: 20mm x 160mm. TOLERANCE = +/- 0.05mm. Supplied with Holder. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3302/2024-T3 | 8 STEP WEDGE:3.0mm,3.5mm, 4.0mm, 4.5mm, 5.0mm, 5.5mm,6.0mm,7.0mm; MATERIAL: 2024-T3 ALUMINUM. LENGTH: 20mm x 160mm. TOLERANCE = +/- 0.05mm. Supplied with Holder. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3303AL | SINGLE HOLE REFERENCE STANDARD 2024-T3 ALUMINUM, HOLE SIZE 3/8"( .375) EDM CORNER NOTCHES .030" x .030". BLOCK SIZE: 2.0" x 2.0" x 1/4" Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3304/7075-T6 | 12 Hole reference standard. Material: 7075-T6 Aluminum. Contains 12 hole sizes; 3/16 inch (4.74mm) 7/32 inch (5.53mm) 1/4 inch (6.35mm) 9/32 inch (7.13mm) 5/16 inch (7.92mm) 11/32 inch (8.71mm) 3/8 inch (9.52mm) 7/16 inch (11.09mm) 1/2 inch (12.7mm) 9/16 inch (14.27mm) 5/8 inch (15.87mm) 3/4 inch (19.05mm); Each hole contains 0.030" x 0.030" (+/-.002") corner EDM notch and a .040" Long x .020" Deep x .005" Wide Mid-Wall EDM Notch. Includes Test Report and Certificate of Conformance. | RH12-C30M20-7075-T6 | . | . | . | |
AFNDT-3305AL | Custom 2 Hole Standard. Material: 7075-T6 Aluminum, Block Size: ..250" x 2.0" x 4.0" . HOLE SIZES:.098" and .188" Diameter with Type A% EDM Notch: .035" x .035" x .004" W ±.001". Includes Test Report and Certificate of Conformance Traceable to NIST. | . | . | . | . | |
AFNDT-3306/2024T3 | EDDY CURRENT SURFACE REFERENCE STANDARD, METRIC NOTCHE SIZES: 0.2mm, 0.5mm &1.0mm. WIDTH = .005" +/- .002" MATERIAL: 2024-T3 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | RS02051M-2024T3 | . | . | . | |
AFNDT-3306/7075T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, METRIC NOTCHE SIZES: 0.2mm, 0.5mm &1.0mm. WIDTH = .005" +/- .002" MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | RS02051M-7075T6 | . | . | . | |
AFNDT-3307 | Custom 8 Hole Standard Manufactured to the Specifications of ATR Part Number 98S51605001-218, Part 6 51-60-00 Figure 616 Sheet 1. Material: 2024-T3 Aluminum, Block Size: .390" x 4.4" x 4.4"(10mm x 111.8mm x 111.8mm) . HOLE SIZES: 2.5mm and 3.2mm. Includes Test Report and Certificate of Conformance Traceable to NIST. | . | . | . | . | |
AFNDT-3308AL | Eddy Current Calibration Standard 3/8” diameter hole standard. Material: 2024-T3 standard with a .030”x .030" corner notch. Includes Certification Report traceable to NIST. | . | . | . | . | |
AFNDT-3309AL | Custom Thin Plate Surface Standard. 7075-T76 Aluminum 10.0" x 10.0" x .050". 3 Surface EDM Notches ±.001" on Width. 1.) 0.010" x 0.200" x .004"W 2.) 0.015" x 0.200" x .004"W 3.) 0.020" x 0.200" x .004"W. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3312AL | 12 HOLE REFERENCE STANDARD, 7075-T6 Aluminum. HOLE SIZES: 3/16", 7/32" 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .004" +/- .001" Wide Thru EDM Notch. A Total of 4 Surface EDM Notches .005", .010" .020", .040" Tolerance: .005" +/-.001". Manufactured in accordance to UASF T.O 33-B-1-1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3313TI | 5 STEP WEDGE, 1mm, 1.5mm, 2mm, 3mm, 4mm, +/- .05mm. Material: 6AL-4V Titanium. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3314TI | 12 HOLE REFERENCE STANDARD, 6AL-4V TITANIUM. HOLE SIZES: 3/16", 7/32" 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .004" +/- .001" Wide Thru EDM Notch. A Total of 4 Surface EDM Notches .005", .010", .020", .050" Tolerance: .005" +/-.001". Manufactured in accordance to UASF T.O 33-B-1-1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3315AL | EDDY CURRENT SURFACE REFERENCE STANDARD, 4 EDM NOTCHES .005", .010", .020" and .050" x (.004"W +/- .002). MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3316AL | Custom Bolt Hole Calibration Block, 2024-T3 Aluminum. Hole Diameter 3/8" (.375")Ø Contains one EDM Corner Notch .030" x .030" +/- .001", and one EDM Radius Thumbnail Notch .120" long x .030 deep +/- .001 . Block Size = 2.0" x 2.0" x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3317/7075 | 6 STEP WEDGE, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm +/- .05mm. Material: 7075 Aluminum. Pad Size: 19mm x 19mm square. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
AFNDT-3318/7075-T6 | 5 STEP WEDGE .500", .600",. 700", .800", 1.00" MATERIAL: 7075-T6 ALUMINUM. PAD SIZE: .75" X .75" TOLERANCE = +/- .001. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3319SS | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .020"(0.5mm), .040"(1.0mm), .079"(2.0mm) (.005"W +/- .002), 304 STAINLESS STEEL. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3320AL | 6 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-02 Part 6 Procedure 1 or 2. Hole Sizes: 15/32", 17/32", 9/16", 11/16", 5/8", 3/4" ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002) Corner EDM Notches. Includes Test Report and Certificate of Conformance. | NDT1084 | . | . | . | |
AFNDT-3321AL | 5 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Hole Sizes: 11.5mm, 14.4mm, 14.6mm, 17.4mm and 17.5mm. Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3340CS | CUSTOM 4 STEP CALIBRATION BLOCK. MATERIAL: 4340 CARBON STEEL. STEP SIZES: .040",.090",.180", .250". PAD SIZE: .750" x .750", Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | |||
AFNDT-3340SS | CUSTOM 4 STEP CALIBRATION BLOCK. MATERIAL: 304 STAINLESS STEEL. STEP SIZES: .040",.090",.180", .250". PAD SIZE: .750" x .750", Includes Test Report traceable to NIST and Certificate of Conformance. | . | . | |||
AFNDT-3390AL | CUSTOM 10 HOLE FLAT BOTTOM REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .218", .250", 312", .375" .437" .500",.562", .625", .750" Ø MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 51-00-00 | . | . | . | |
AFNDT-3391AL | CUSTOM 10 HOLE FLAT BOTTOM HOLE REFERENCE STANDARD ASSEMBLY PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .875", 1.00", 1.125", 1.250" 1.375", 1.500", 1.625", 1.750" 1.875", 2.000Ø Ø MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 51-00-16 | . | . | . | |
AFNDT-3392TI | Custom Titanium multi-hole reference standard. Contains 9 hole sizes; 2.0mm, 2.5mm 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm, 5.5mm and 6.0mm hole diameters. EDM notch 0.5mm X 7.5mm deep in each hole (half of the material thickness). Material: 6AL-4V Titanium 15mm Thick. Includes Test Report and Certificate of ConformanceTraceable to NIST. | . | . | . | . | |
AFNDT-3393TI | Custom Titanium multi-hole reference standard. Contains 9 hole sizes; 2.0mm, 2.5mm 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm, 5.5mm and 6.0mm, 6.5mm. 7.0mm, 7.5mm, 8.0mm, 8.5mm, 9.0mm, 9.5mm, 10.0mm, 10.5mm, 11.0mm, 11.5mm, 12.0mm, 12.5mm, 13.5mm, 14.0mm, 14.5mm, 15.0mm, 15.5mm, and 16.0mm hole diameters. EDM notch 0.5mm X 7.5mm deep in each hole (half of the material thickness). Material: 6AL-4V Titanium 15mm Thick. Includes Test Report and Certificate of ConformanceTraceable to NIST. | . | . | . | . | |
AFNDT-3394AL | 8 STEP WEDGE, STEP SIZES OF .015", .025",.040", .060", .080", .100", .150", and .200" +/- .001". PAD SIZE: .75"x.75", MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3395 | CUSTOM EC SKIN INSPECTION REFERENCE STANDARD. Contains various EDM Nothes in the Upper and Lower Skin. Upper Skin Thickness of .080" and Lower Skin Thickness of .100" Thick. Standard Physical Size = 13.5" Long x 5.15" Wide. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-3396CS | SURFACE NOTCH REFERENCE STANDARD 4130 or 4340 CARBON STEEL. EDM NOTCH SIZE: FULL WIDTH OF PART x .51mm(.020") DEEP +/- .05mm(.002"). BLOCK SIZE: 1.0" WIDE x 3.0" LONG. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-4010/2024T3 | 6 STEP WEDGE: 0.030 in. (0.762 mm), 0.050 in. (1.27 mm), 0.100 in.(2.54 mm), 0.150 in (3.81 mm), 0.300 in. (7.62 mm), and 0.500 in. (12.70 mm) +/-.001", Material: 2024-T3 Aluminum. Pad Size: 0.75" x 0.75" , BLOCK SIZE: 4.50" L x .750"W SUPPLIED WITH DELRIN HOLDING BLOCK. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-4010/7075T6 | 6 STEP WEDGE: 0.030 in. (0.762 mm), 0.050 in. (1.27 mm), 0.100 in.(2.54 mm), 0.150 in (3.81 mm), 0.300 in. (7.62 mm), and 0.500 in. (12.70 mm) +/-.001", Material: 7075-T6 Aluminum. Pad Size: 0.75" x 0.75" , BLOCK SIZE: 4.50" L x .750"W SUPPLIED WITH DELRIN HOLDING BLOCK. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-40244 | CUSTOM ETHER NDE TEST BLOCK, PER SPEC | . | . | . | . | |
AFNDT-7075DAA19 | ASTM DISTANCE AMPLITUDE SET OF 19 7075-T6 ALUMINUM (CASE INCL) 3/34", 5/64" and 8/64" FLAT BOTTOM HOLES | 200129-1 | . | . | . | |
AFNDT-AL-6061 | CUSTOM REFERENCES STANDARD PER AMS4083 | . | . | |||
AFNDT-CHOKE BLOCK-70/30 | CALIBRATION BLOCK 70/30 COPPER-NICKEL | NDE005 | . | . | . | |
AFNDT-CHOKE BLOCK-C | CALIBRATION BLOCK 1018 CARBON STEEL | NDE005 | . | |||
AFNDT-CHOKE BLOCK-DUP | CALIBRATION BLOCK 2205 SS (DUPLEX) | NDE005 | . | . | . | |
AFNDT-CHOKE BLOCK-S | CALIBRATION BLOCK 303 STAINLESS STEEL | NDE005 | . | |||
AFNDT-CRJ200/CRS | SURFACE REFERENCE STANDARD, ALUMINUM, .005W x .008", .020", .040" EDM NOTCH DEPTHS . MATERIAL 2024-T3 AL...CRJ200 PART1 51-20-06 PG.9 | . | . | . | . | |
AFNDT-DELRIN BLOCKS | DELRIN BLOCKS W/ TOE CLAMPS .500-.030 STEP BLOCKS | . | . | |||
AFNDT-ECRC82040 | Eddy Current Crack Standard Magnesium AZ-31 | . | . | . | . | |
AFNDT-FBH30AL | Used for determining resolution and sensitivity capabilities and for producing area amplitude and distance amplitude plots for normal beam transducers. Contains ten flat-bottom holes at 3/64” diameter, ten at 5/64”, and ten at 8/64”. Metal travel dista... | . | . | . | . | |
AFNDT-FBH30CS | Used for determining resolution and sensitivity capabilities and for producing area amplitude and distance amplitude plots for normal beam transducers. Contains ten flat-bottom holes at 3/64” diameter, ten at 5/64”, and ten at 8/64”. Metal travel dista... | . | . | . | . | |
AFNDT-IIW-01AL | ALUM. IIW TYPE 1 TEST BLOCK.. Aluminum Ultrasonic IIW Type 1 Test Block 7075-T6 Aluminum. 1 "x 4"x 12". Contains 2" diameter hole and 4" radius. Also, 1/8" x 1" radius alternate reflector and 1/16" deep on echo side. Meets ASTM-E-164, MIL-STD-2154 a... | CB-01-AL | 802048A | . | ||
AFNDT-IIW-01CS | IIW TYPE 1 TEST BLOCK.. Aluminum Ultrasonic IIW Type 1 Test Block 1018 Carbon Steel. 1 "x 4"x 12". Contains 2" diameter hole and 4" radius. Also, 1/8" x 1" radius alternate reflector and 1/16" deep on echo side. Meets ASTM-E-164, MIL-STD-2154 and AW... | . | . | . | . | |
AFNDT-PLUG | PLUG - 54-10-33 | . | . | |||
AFNDT-PR-T-2521/22 | CUSTOM EDDY CURRENT SURFACE CALIBRATION BLOCK. PER CUSTOMER SUPPLIED DRAWING. MATERIAL: 7075-T6 Aluminum. EDM Notch size 1mm (.040') , .76mm(.030"), .2mm(.008") deep x .1mm(.004") wide +/- .002". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFNDT-PSM-5/S | The PSM-5 Panel is manufactured to Pratt-Whitney P/N TAM 146040 specifications. Smooth Type - the chrome plated strip of the second version is not grit blasted...Sherwin Incorporated is an authorized manufacturer of TAM 146040 panels...PSM-5 Panel pro... | . | . | . | . | |
AFNDT-ROMPAS-7075-T6 | ROMPAS BLOCK, 7075-T6 ALUMINUM ½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version). SPECIFICATION: ASTM E-164. (Includes wooden case) | . | . | . | . | |
AFNDT-SA227 | FAIRCHILD REFERENCE STARDARD FOR THE SA227 DOOR use fastener MS2042AD4-10 | 304 | . | . | ||
AFNDT-SRS-082A-1 | EDDY CURRENT SURFACE BLOCK 7075-T6 ALUMINUM. 2 EDM SLOTS ( 0.2mm deep +/-0.05mm & 0.12mm wide +/- 0.01mm). EDM NOTCH#1 ( 0.5mm deep +0.06/-0.04 & 0.12 wide +0.01/-0.02 ), and EDM NOTCH #2 ( 1.0mm deep +0.06mm/-0.04mm & 0.12mm wide +0.01mm/-0.02mm). Inc... | SRS-082A-1 | . | . | . | |
AFNDT-SRS-082S-1 | EDDY CURRENT SURFACE BLOCK 4130 STEEL. 2 EDM SLOTS ( 0.2mm deep +/-0.05mm & 0.12mm wide +/- 0.01mm). EDM NOTCH#1 ( 0.5mm deep +0.06/-0.04 & 0.12 wide +0.01/-0.02 ), and EDM NOTCH #2 ( 1.0mm deep +0.06mm/-0.04mm & 0.12mm wide +0.01mm/-0.02mm). Includes ... | SRS-082S-1 | . | . | . | |
AFNDT-SRS-4A | SURFACE STANDARD ALUMINUM(2024-T351) 1 EDM SLOT (0.040 DEEP) | SRS-4A | SRS-4A | . | . | |
AFNDT-SRS-4S | SURFACE STANDARD STEEL 4340 1 EDM SLOT (0.40 DEEP) | SRS-4S | SRS-4S | . | . | |
AFNDT-SRS-4T | SURFACE STANDARD TITANIUM 1 EDM SLOT (0.40 DEEP) | SRS-4A | . | . | ||
AFNDT-SS304 | CUSTOM REFERENCES STANDARD PER AMSS5564 | . | . | |||
AFNDT-VL769-1A | TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(.800"THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES) | . | . | . | . | |
AFNDT-VL769-2A | TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(1.500" THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES) | . | . | . | . | |
AF-NEC-6112-1/Ti | Custom multi-hole reference standard Material: 6AL-4v Titanium. Hole sizes: 1/8", 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8",11/16" and 3/4". Countersink holes opposite side. Thru hole EDM notches in each hole .005" +/-.001". 3 Surface... | NEC-6112-1 | . | . | . | |
AFS-0504-70ST | 70° ANGLE BEAM TRANSDUCER in STEEL, 5MHz .25" x .25" ELEMENT, CASE SIZE( .550"L x .310"W x .675" H) SUPPLIED WITH A TOP MOUNT MICRODOT CONNECTOR. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AFW37-32-TI | WEDGE 32° REFRACTED IN TI | . | . | . | . | |
AFW37-39-TI | WEDGE 39° REFRACTED IN TI | W37-39-TI | . | . | . | |
AGE-02321-401 | Embraer 170 Reference Standard. Material: 2024-T351 Clad. Top skin = 0.040, Lower skin = 0.080. Rivet - MS2047AD-5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AHS29-1A-0 | (Aluminum Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/... | MHS-29-1A-0 | . | . | . | |
AHS29-1A-2 | (Aluminum Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/... | MHS-29-1A-2 | . | . | .. | |
AHS29-1S-0 | Carbon Steel(4340) Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 2... | MHS-29-1S-0 | . | . | . | |
AHS29-1SS-0 | (304 Stainless Steel Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16",... | MHS29-1SS-0 | . | . | . | |
AHS29-1SS-1 | (Stainless Steel Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/... | MHS-29-1SS-1 | . | . | . | |
AHS29-C2-A1 | CUSTOM 29 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM WITH 0.015" THRU EDM NOTCH AND 0.030X0.030 CORNER NOTCH. Includes Test Report Traceable to NIST and Certificate of Conformance. | MHS-29-1A-3 | . | |||
AHS29-C30304 | 304 Stainless Steel Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 (+/-10%) corner EDM notch. . Includes Test Report and Certificate of Conformance. | RM290C30-304 | . | . | . | |
AHS29-C30INC | Inconel 718 Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 (+/-10%) corner EDM notch. . Includes Test Report and Certificate of Conformance. | RM290C30I718 | . | . | . | |
AHS29-C30TI | 6AL-4V Titanium Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 31/32", 1.0" inch. Each hole contains 0.030 x 0.030 (+/-10%) corner EDM notch. . Includes Test Report and Certificate of Conformance. | RM290C30-6AL4V | . | . | . | |
AL 29-32 | BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-20-001. Also in 53-30-19 PART 6 PAGE 6 FIGURE 2. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL 2024-T3 ALUMINUM. SIZE: 1.5"W x 3.75"L x .25" | . | . | . | . | |
AL 35-45 | BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-70-001. ALSO IN 53-10-01 PART 6 PAGE 5 FIGURE 1. EDM Notches: .008", .020", .040" ( .005" Wide +0.00, - .002" and +/- .001" Depth), MATERIAL: 2124-T8 or 7075-T7 ALUMINUM. SIZE: 1.5"W x 3.75"L... | . | . | . | . | |
AL2024-016-063 | CUSTOM 4 STEP REFERENCE BLOCK. MATERIAL: 2024-T3. STEP SIZE 0.016", 0.032", 0.056", 0.063" +/-.002". PAD SIZE: .787" x .787". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AL2024-024-125 | CUSTOM 4 STEP REFERENCE BLOCK. MATERIAL: 2024-T3. STEP SIZE 0.024", 0.071", 0.112", 0.125" +/-.002". PAD SIZE: .787" x .787". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AL7075-016-063 | CUSTOM 4 STEP REFERENCE BLOCK. MATERIAL: 7075-T6. STEP SIZE 0.016", 0.032", 0.056", 0.063" +/-.002". PAD SIZE: .787" x .787". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AL7075-024-125 | CUSTOM 4 STEP REFERENCE BLOCK. MATERIAL: 7075-T6. STEP SIZE 0.024", 0.071", 0.112", 0.125" +/-.002". PAD SIZE: .787" x .787". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AMP-39-B-53-10-00-00A-31BA-K | REFERENCE STANDARD PER AW139 IETP 33rd Issue. Material: AISI 301-1/4 HARD STEEL, 7075 AL | . | . | . | . | |
AMS2630C Custom | Custom Reference Standard Per SAE AMS2630C. material: Titanium Alloy, Ti6Al4V per AMS-4928R Annealed. Includes 2 EDM Flaws per customer supplied Drawing. Includes Test Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
ANDT1015 | BOEING REFERENCE STANDARD 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1049 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN5-2, BACR15CE5D-2, BACR15ET7D-2). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1049/.036 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5, .036 SKIN. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1050 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN5-2, BACR15CE5D-2, BACR15ET7D-2). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1051 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN6-2, BACR15CE6D-2, BACR15BB8D-2). Includes Test Report and Certificate of Conformance. | BACB30FN6-2 | . | . | ||
ANDT1052 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-2, BACR15CE8D-2, BACR15BB8D-2). Includes Test Report and Certificate of Conformance. | BACB30FN8-2 | . | . | ||
ANDT1053 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 FASTENER (BACB30FN8-3, BACR15CE8D-3, BACR15BB8D-3). Includes Test Report and Certificate of Conformance. | BACB30FN8-2 | . | . | ||
ANDT1054 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-3, BACR158D-3, BACR15BB8D-3). Includes Test Report and Certificate of Conformance. | BACB30FN8-3 | . | . | ||
ANDT1055 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | BACB30FN8-4 | . | . | ||
ANDT1056 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1057 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT-1070/4330 | 14 HOLE CALIBRATION STANDARD. Material: 4330 Steel. Hole Sizes: 5/32, 3/16, 13/64, 7/32, 15/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64, 11/32, 3/8, 1/2. EDM Flaws: .020" x .020" x .005" +/- .001" and .030" x .030" x .005" Wide +/- .001" corner notches. ... | . | . | |||
ANDT-1070/TI | 14 HOLE CALIBRATION STANDARD. Material: 6AL-4V Titanium. Hole Sizes: 5/32, 3/16, 13/64, 7/32, 15/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64, 11/32, 3/8, 1/2. 28 Total EDM Flaws: .020" x .020" x .005" +/- .001" and .030" x .030" x .005" Wide +/- .001" co... | . | . | . | . | |
ANDT1077 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN5-2, BACR15CE5D-2, BACR15ET7D-2). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1079 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. Includes Test Report and Certificate of Conformance. FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, BACR15BB7AD-4, BACR15BB8AD-4, ALL ALODINE) | . | . | . | . | |
ANDT1080 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. Includes Test Report and Certificate of Conformance. FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, BACR15BB7AD-4, BACR15BB8AD-4, ALL ALODINE) | . | . | . | . | |
ANDT1081 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENER (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT1082 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENERS: (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT-1096AL | 10 STEP REFERENCE BLOCK, .020".030",.040",.050",.063",.071",.080",.090",100",.125" MATERIAL: (7075-T651 ALUMINUM) | . | . | . | . | |
ANDT3004 | BOEING REFERENCE STANDARD 737 PT 6 53-30-12 FASTENER (BARC15CE5D5, BARC15CE5D6, BACR15CE6D5, BACR15CE6D6) | . | . | . | . | |
ANDT3006 | BOEING REFERENCE STANDARD 737 PT 6 53-30-14 FASTENER (BACR15BB8D-7, BACR15ET7D-7, BACB30FN5-3, BACC30M-5, ALL ALODINE) | . | . | . | . | |
ANDT3016-B | BOEING REFERENCE STANDARD 737 PT 6 53-10-54 FIG 2 FASTENER (BACB15BB5D-4, ALL ALODINE). Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
ANDT3019 | BOEING REFERENCE STANDARD 737 PT 6 53-30-16 FIG 1 FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, ALL ALODINE) | . | . | . | . | |
ANDT388 | BOEING 737 REFERENCE STANDARD PART 6 53-10-48, ..PAGE 11 FIGURE 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ANDT390A | BOEING REFERENCE STANDARD 737 PT 6 53-10-47 FASTENER (BACR15BB6, ALL ALODINE) | . | . | |||
ANDT390B | BOEING REFERENCE STANDARD 737 PT 6 53-10-47 FASTENER (BACR15BB6, ALL ALODINE) | . | . | |||
ANDT4126 | BOEING REFERENCE STANDARD PT 6 53-30-00 FIG 6 pg.5, FASTENER (BACR15CE6, ALL ALODINE) | . | . | . | . | |
APB-NDT001 | AVIATION PARTNERS BOEING 767 REFERENCE STANDARD 57-20-02 PG.6.. PART 6 | . | . | . | . | |
APB-NDT003 | AVIATION PARTNERS BOEING 767 REFERENCE STANDARD 57-20-02 PG.9.. PART 6 | . | . | . | . | |
APB-NDT004 | AVIATION PARTNERS BOEING 767 REFERENCE STANDARD 57-20-01.. PART 6 | . | . | . | . | |
APB-NDT005 | AVIATION PARTNERS BOEING 767 REFERENCE STANDARD 57-20-02.. PART 6 | . | . | . | . | |
APB-NDT006 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 57-20-03.. PART 6, PG. 5&6 SHEETS 1&2 | . | . | . | . | |
APB-NDT007 | BOEING-AVIATION PARTNERS REFERENCE STANDATD 767 PART 6 57-20-09 PAGE 7 FIGURE 2 SHEET 1&2 | . | . | . | . | |
APB-NDT008 | BOEING-AVIATION PARTNERS REFERENCE STANDATD 767 PART 6 57-20-09 PAGE 1 FIGURE 4 SHEET 1&2 | . | . | . | . | |
APB-NDT009 | BOEING-AVIATION PARTNERS REFERENCE STANDATD 767 PART 6 57-20-09 PAGE 5 FIGURE 6 SHEET 1&2 | . | . | . | . | |
APB-NDT010 | BOEING-AVIATION PARTNERS REFERENCE STANDATD 767 PART 6 57-20-09 PAGE 8 FIGURE 8 SHEET 1&2 | . | . | . | . | |
APB-NDT011A | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FASTENER (BACB30VU10K14,BACC30BP10). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT011B | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FASTENER (BACB30NX10K14,BACC30M10). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT011C | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FASTENER (BACB30VU10K8,BACC30BP10). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT011D | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FASTENER (BACB30VU8K7,BACC30BP8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT012 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 57-20-03 PART 4 FIGURE 3 PAGE 7. 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT013 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 57-20-03 PART 4 FIGURE 4 PAGE 9. 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT014 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 57-20-03 PART 4 FIGURE 5 PAGE 11. 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT015 | BOEING AVIATION PARTNERS REFERENCE STANDARD.PART 6 57-20-09 PAGE 21 | . | . | . | . | |
APB-NDT016 | BOEING AVIATION PARTNERS REFERENCE STANDARD.PART 6 57-20-09 PAGE 24 | . | . | . | . | |
APB-NDT3301 | AVIATION PARTNERS REFERENCE STANDARD 737 57-20-34 PT 6 FIG 2 FASTENER (BACB30NY6K8Y + BACC30R8, BACB30NW8K11 + BACC30M8) | . | . | . | . | |
APB-NDT3302 | AVIATION PARTNERS REFERENCE STANDARD 737 57-20-35 PT 6 FIG 2 FASTENER (BACB30NW8K9X + BACC10M8, BACB30MW8K9 + BACC30M8) | . | . | . | . | |
APB-NDT5201 | AVIATION PARTNERS BOEING 757 PT 6 57-20-01 | . | . | . | . | |
APB-NDT5202 | AVIATION PARTNERS BOEING 757 PT 6 57-20-01 | . | . | . | . | |
APB-NDT5203 | AVIATION PARTNERS REFERENCE STANDARD 737 57-20-02 FASTENER (BACR15FH8DD13) | . | . | . | . | |
APB-NDT5204 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 PT 6 57-20-02 FASTENER (BACR15FH10DD13) | . | . | . | . | |
APB-NDT5205 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 PT 6 57-20-02 FASTENER (BACR15FH10DD15) | . | . | . | . | |
APB-NDT5206 | AVIATION PARTNERS REFERENCE STANDARD 57-20-03 PT 6 FIG 2 FASTENER (BACB30NW10K13, BACC30BP10) | . | . | . | . | |
APB-NDT5207 | AVIATION PARTNERS REFERENCE STANDARD 57-20-03 PT 6 FIG 4 FASTENER (BACB30NW12K16, BACC30BO12) | . | . | . | . | |
APB-NDT5208 | AVIATION PARTNERS REFERENCE STANDARD 57-20-03 PT 6 FIG 6 FASTENER (BACB30NW10K13, BACC10BP10) | . | . | . | . | |
APB-NDT5209 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 57-20-03 PART 4 FIGURE 2 PAGE 9. 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
APB-NDT5301 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 PT 6 57-20-01 FASTENER (BACBYP10K14 + BACC30BP10, BACB30NY10K14Y + BACC30AC10) | . | . | . | . | |
APB-NDT5302 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 PT 6 57-20-01 FASTENER (BACBYP10K13 + BACC30BP10, BACB30N1-K14Y + BACC30AC10) | . | . | . | . | |
APB-NDT5303 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 PT 6 57-20-01 FASTENER (BACB30YP8K12 + BACC3-BP) | . | . | . | . | |
ARS-0812S | Surface reference standard, 17-4PH Steel, with EDM notch depths of 0.008", 0.010" and 0.020" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ARS-0824/2024-T3 | Surface reference standard, 2024-T3 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | . | . | . | . | |
ARS-0824/2024T6 | Surface reference standard, 2024-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ARS-0824/2024-T6 | Surface reference standard, 2024-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | ||
ARS-0824/6061T6 | Surface reference standard, 6061-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | RS-0824/6061T6 | . | . | . | |
ARS-0824/7475-T7 | Surface reference standard, 7475-T7 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | . | . | . | . | |
ARS-0824-7050 | Surface reference standard, 7050-T7 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | SRS-0824A-7050T74 | . | . | . | |
ARS-0824-7050T74 | Surface reference standard, 7050-T74 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | SRS-0824A-7050T74 | . | . | . | |
ARS-0824-7075T6 | Surface reference standard, 7075-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ARS-0824-7075T7 | Surface reference standard, 7075-T7 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | . | . | . | . | |
ARS-0824-7075T73 | Surface reference standard, 7075-T73 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ARS-0824A | Surface reference standard, 7075-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | SRS-0824A | . | . | . | |
ARS-0824I | Surface reference standard, Inconel 718, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | SRS-0824I | . | . | . | |
ARS-0824M | Surface reference standard, Magnesium, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | SRS-0824M | . | |||
ARS-0824S | Surface reference standard, 4340 Steel, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 inc... | SRS-0824S | . | |||
ARS-0824SS | Surface reference standard, 304 Stainless steel, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM NOTCHES .005" W +/-.001" | SRS-0824-304 | . | . | . | |
ARS-0824SS/316 | Surface reference standard, 316 Stainless steel, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM NOTCHES .005" W +/-.001" | . | . | . | . | |
ARS-0824T | Surface reference standard, 6AL-4v Titanium, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.2... | SRS-0824T | . | |||
ARS-1012HCS | 12 HOLE REFERENCE STANDARD 4130 OR 4340 CARBON STEEL WITH 0.020" x 0.020" and 0.030" x 0.030" CORNER EDM NOTCH. HOLE SIZES: 1/8, 5/32, 3/16, 13/64, 7/32, 5/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ARS-1012HSA | 12 HOLE REFERENCE STANDARD 7075-T6 WITH 0.020" x 0.020" and 0.030" x 0.030" CORNER EDM NOTCH. HOLE SIZES: 1/8, 5/32, 3/16, 13/64, 7/32, 5/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64. Includes Test Report and Certificate of Conformance. | . | . | |||
ARS-1018NAV | NAVSHIPS Test Block - 1018 Carbon Steel, 1 1/4" x 3" x 12", Contains six 3/64" diameter drilled holes at distances of 1/8" thru 2 3/4", With Case. | CB-20-CS | . | . | ||
ARS-304NAV | NAVSHIPS TEST S.S. BLOCK | 200124-0 | . | . | . | |
ARS-7075NAV | NAVSHIPS TEST ALUM BLOCK | 200124-1 | . | . | . | |
ASDPR-.5/500HZ-50K | REFLECTION SPOT PROBE ACETAL BODY, SHIELDED, 500Hz-50KHz, .500"Ø (12.7mm)OD, SUPPLIED WITH A RIGHT MOUNTED TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ASE-WSNDT | CUSTOM SURFACE CALIBRATION BLOCK. MATERIAL: 7075-T73 ALUMINUM. EDM NOTCH SIZE: 1.52mm(.060") LONG x 0.13mm(.0051") WIDE x 0.76mm(.030") DEEP. +/- .05mm. Includes Test Report and Certificate of Conformance. | AFNDT-3039 | . | . | . | |
ASTM E317/FIG.1 | Ultrasonic Test Block for Evaluation of Horizontal and Vertical Linearity. ASTM E317 FIG.1 | . | . | . | . | |
ASTM E317-16 FIG 1 | ASTM E317-16 Test Block for Evaluation fo Horizontal and Vertical Linearity. Material: 1018 Steel, Nickel Plated for Corrosion Resistance. ASTM E317-16 FIG.1 Pages 3-4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ASTM E317-16/FIG X1.1 | ASTM E317-16 Type RA Resolution Block. Material: 1018 Steel, Nickel Plated for Corrosion Resistance. ASTM E317-16 FIG. X1.1 Page 12. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ASTM-E317/FIG.6 | ASTM TYPE RA Resolution Block 7075-T6 Aluminum. ASTM-E317 FIG.6.. | . | . | . | . | |
ASTW-5 | 5 STEP CAST ACRYLIC STEP WEDGE, 2.0" x 2.0" PAD SIZE. STEP THICKNESSES: .100", .200", .300", .400" and .500" ± .002". Includes Test Report and Certificate of Conformance | . | . | |||
ASTW5-1 | 5 STEP ACRYLIC WEDGE, .200", .220", .240", .260", .280", Strenched Acrylic, 1" X 1" Sq, 1" x 5" LONG +/- .002. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ASTW5-2 | 5 STEP ACRYLIC WEDGE, .300", .320", .340", .360", .380", Strenched Acrylic, 1" X 1" Sq, 1" x 5" LONG +/- .002. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ASTW-8 | CUSTOM ACRYLIC CALIBRATION STANDARDS, SET OF 8, THICKNESS .921 / .818 / .559 / .504 / .275 / .248 / .157 / .134 | . | . | . | . | |
ASW5 2024-T3 | 5 STEP WEDGE - 1X1, 1.250, 1.00, .75, .500,.250 | . | . | . | . | |
AURX-1.125-1.250/100K-2MHz | ADJUSTABLE ROTARY X-PROBE. EXPANDABLE FROM 1.125"-1.250" 100KHz-2MHz 2.0" WORKING LENGTH, SUPPLIED WITH A 4 PIN FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
AWS-1000N | WHEEL REFERENCE STANDARD. INCLUDES 3 EDM NOTCHES .005"W x .030"D x .150"L. NOTCHES INSTALLED IN THE BEAD SEAT AREA OF THE WHEEL. CUSTOMER SUPPLIED PART | . | . | . | . | |
AWS-A320M | WHEEL REFERENCE STANDARD FOR AIRBUS A32 MAIN P/N: 3-1530. INCLUDES 3 EDM NOTCHES .005"W x .030"D x .150"L. NOTCHES INSTALLED IN THE BEAD SEAT AREA OF THE WHEEL. CUSTOMER SUPPLIED PART | WS-A320M | 3-1530 | . | . | |
AWS-A321M | WHEEL REFERENCE STANDARD FOR AIRBUS A321 MAIN P/N: C20500100. INCLUDES 3 EDM NOTCHES .005"W x .030"D x .150"L. NOTCHES INSTALLED IN THE BEAD SEAT AREA OF THE WHEEL. CUSTOMER SUPPLIED PART | C20500100 | . | . | . | |
AWS-A321N | WHEEL REFERENCE STANDARD FOR AIRBUS A321 NOSE P/N: 3-1531-3. INCLUDES 3 EDM NOTCHES .005"W x .030"D x .150"L. NOTCHES INSTALLED IN THE BEAD SEAT AREA OF THE WHEEL. CUSTOMER SUPPLIED PART | 3-1531-3 | . | . | . | |
AWS-B717N | WHEEL REFERENCE STANDARD FOR BOEING 717 NOSE. 3 EDM NOTCHES .005"W x .030"D x .150"L | . | . | . | . | |
AWS-B737MLG | WHEEL REFERENCE STANDARD FOR BOEING MLG WHEEL P/N: 2612311-1 . INCLUDES 3 EDM NOTCHES .005"W x .030"D x .150"L. NOTCHES INSTALLED IN THE BEAD SEAT AREA OF THE WHEEL. CUSTOMER SUPPLIED PART | 2612311-1 | . | . | . | |
AXXTPN-91-4B/500K-1MHZ | SURFACE PROBE .062" DIA TUBING 90° DEGREES .100" DROP BENT AT 1.0 ", 4.0" LONG TRIAX FISCHER CONNECTOR 500KHz-1MHz | PABM90C401 | . | . | . | |
B737NG-1 | BOEING POSITIONER CAST ACRYLIC(PLEXIGLASS) -1 | . | . | . | . | |
B737NG-2 | BOEING POSITIONER PLATE 2024-T3 ALUMINUM. -2 | . | . | . | . | |
B737NG-3 | BOEING POSITIONER RING 2024-T3 ALUMINUM. -3 | . | . | . | . | |
B737NG-4 | BOEING POSITIONER GUIDE CAST ACRYLIC(PLEXIGLASS). -4 | . | . | . | . | |
BACB30US10K47 | BOEING 767 BOLT, P/N: BACB30US10K47 PART 4 57-50-01. Includes Certification. | . | . | . | . | |
BASE PLATES 717RS2 1/4 | BOEING UT REFERENCES STANDARD | . | . | |||
BASE PLATES 717RS2 1/8 | BOEING UT REFERENCES STANDARD | . | . | |||
BH7475-T7351 | CALIBRATION STANDARD, BOMBARDIER CHALLENGER 604, 53-21-00 FIG 602. MATERIAL: 7475-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | |||
BUTTON HEAD CAL STD | BOEING BUTTON HEAD CALIBRATION STANDARD | . | . | . | . | |
C13/C33 | PEMCO REPAIR COUPON #25 FIGURE 2. MATERIAL: 2024-T3 CLAD ALUMINUM. RIVETS: MS20426DD6. EDM NOTCH LENGTH: .26"(.66mm) and .280"(.71mm) BOTH SIDES OF FASTENER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
C130-CW-012 | C-130 CALIBRATION STANDARD. MATERIAL:7075-T6 ALUMINUM 5 PIECE STACK. FASTENER (HLT114-6-8 + NUT P/N: KFN542-3) 6 PLACES. Includes Test Report and Certificate of Conformance. | PDL 1252 | BACC30X8 | |||
C130-CW-013 | C-130 CALIBRATION STANDARD. MATERIAL:7075-T6 ALUMINUM 5 PIECE STACK. FASTENER (HLT114-6-8 + NUT P/N: KFN542-3) 6 PLACES. Includes Test Report and Certificate of Conformance. | PDL 1253 | . | . | . | |
C130-CWOW-019 | LOCKHEED C-130 CALIBRATION STANDARD LOWER SURFACE PANEL. MATERIAL: 7075-T6 ALUMINUM | PDL 422J | PDL 1259 | . | . | |
C130-OW-016 | LOCKHEED C-130 CALIBRATION STANDARD FIGURE 9-4 No.1 and No. 4 Truss Mount Upper Lugs. Material: 7075-T6 Aluminum Sulfuric Acid Anodized Per MIL-A-8625 or Equivalent. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
C130-UT-17-1 | C-130 CALIBRATION STEP STANDARD. MATERIAL:7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
C-130-WR | C-130 Outer Wing Rainbow Fitting Bolt Hole Standard C-130, 2 Layers, 3 HOLES, 3/4", 7/8" and 1.0" with .004" X .030" X .030" EDM Notches in each hole. Includes Test Report and Certificate of Conformance. | ECRS-559 | . | . | . | |
C3/C29 | PEMCO REPAIR COUPON #25 FIGURE 2. MATERIAL: 2024-T3 CLAD ALUMINUM. RIVETS: MS20426DD6. EDM NOTCH LENGTH: .125"(.031mm) and .180"(.45mm) BOTH SIDES OF FASTENER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
CA12-1508A | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T7 ALUMINUM, 54-10-11 PAGE 634A FIG.603 SHEET 21B | . | . | . | . | |
CA12-1683A | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 STEEL, 54-10-11 PAGE 632C FIG.603 SHEET 20C | . | . | . | . | |
CA235-235502 | AIRBUS MILITARY REFERENCE STANDARD 53-30-10 FIG 505, PAGE 508. | . | . | . | . | |
CB-LM-532048 | REFERENCE BLOCK FIGURE 5. MATERIAL: 2024-T351 ALUMINUM WITH PRIMER. EDM NOTCH: 3mm X 3mm X .15mm ± .05mm. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
CE1331699-003 | 8 STEP THICKNESS CALIBRATION STANDARD. STEP SIZES: .025", .030", .035", .040", .045", .055", .060", .068" +/-.001". PAD SIZE 1.0" x 1.25" TYP. MATERIAL: 7475-T7351 ALUMINUM, CHROMIC ACID ANODIZED. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
CE1617528 | CALIBRATION STANDARD, BOMBARDIER TEST REFERENCE ULTRA SONIC NDI. MATERIAL: 7475-T7351 and 7040-T7451 ALUMINUM. MS90254U0805D FASTENERS. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
CE1617529 | CALIBRATION STANDARD, BOMBARDIER TEST REFERENCE ULTRA SONIC NDI. MATERIAL: 7475-T7351 and 7040-T7451 ALUMINUM. MS90254U0805D FASTENERS. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
CFM56 9970-958-579 | EDDY CURRENT SURFACE REFERENCE BLOCK. 2 EDM NOTCHES .012" Deep x .004" Wide and .020" Deep x .004" Wide. Tolerance on Width (.004" W +/- .002"), Material: Inconel 600 Series. Reference: CFM56-5B S/B 72-0620 PAGE 14. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
COMAC AL.01 | Aluminum Multi-hole reference standard with certificate. Material: 7075-T6 Aluminum. Block Thickness = .25" Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16"... | . | . | . | . | |
COMAC AL.01/2024T3 | Aluminum Multi-hole reference standard with certificate. Material: 2024-T3 Aluminum. Block Thickness = .25" Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains two EDM corner notches; 0.030 inch X 0.030 inch (0.762mm X 0.762mm) 0.020 inch X 0.020 inch (0.508mm X 0.508mm) Reference standard also contains 3 each Surface EDM notches; 0.010 inch (0.254mm), 0.020 inch (0.508mm) and 0.040 inch (1.01mm) deep). Includes Test Certificate traceable to NIST and Certificate of Conformance (COC). | . | . | . | . | |
COMAC TI.01 | Aluminum Multi-hole reference standard with certificate. Material: 6AL-4V Titanium. Block Thickness = .25" Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains two EDM corner notches; 0.030 inch X 0.030 inch (0.762mm X 0.762mm) 0.020 inch X 0.020 inch (0.508mm X 0.508mm) Reference standard also contains 3 each Surface EDM notches; 0.010 inch (0.254mm), 0.020 inch (0.508mm) and 0.040 inch (1.01mm) deep). Includes Test Certificate traceable to NIST and Certificate of Conformance (COC). | . | . | . | . | |
COMAC-20-2A-5 | Aluminum Multi-hole reference standard with certificate. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains two EDM corner... | MHS-20-2A-5 | . | . | . | |
COMAC-20-2S-5 | Steel (4130 or 4340) Multi-hole reference standard with certificate. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains tw... | MHS-20-2S-5 | . | . | . | |
COMAC-20-2SS-5 | Stainless Steel(304) Multi-hole reference standard with certificate. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains tw... | MHS-20-2SS-5 | . | . | . | |
COMAC-20-2TI-5 | Titanium(6AL-4V) Multi-hole reference standard with certificate. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains two ED... | MHS-20-2TI-5 | . | . | . | |
CONTINUITY TEST | BOEING CONTINUITY TEST REFERENCE STANDARD. PAINT REQUIRED. MATERIAL:2024-T3 CLAD OR BARE ALUMINUM. | . | . | . | . | |
COUPON 12 | PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-3. 05-30-10 PG.193. Includes Certification Report Tracable to NIST. | . | . | . | . | |
COUPON 2 | PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-4. 05-30-10 PG.190. Includes Certification Report Tracable to NIST. | . | . | . | . | |
COUPON 25 | PEMCO LOW FREQUENCY EDDY CURRENT STANDARD FOR INSPECTION UJ-1. 05-30-10 PAGE 194. EDM NOTCH: .030 MAX WIDTH x .240" LONG | . | . | . | . | |
COUPON 29 | PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-3 and ED-4. 05-30-10 PG.195. Includes Certification Report Tracable to NIST. | . | . | . | . | |
COUPON 3 | PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-3. 05-30-10 PG.191. Includes Certification Report Tracable to NIST. | . | .. | . | . | |
COUPON 31 | PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-5. 05-30-10 PG.196. Includes Certification Report Tracable to NIST. | . | . | . | . | |
COUPON 6 | PEMCO WORLD AIR SERVICES EDDY CURRENT LOW FREQUENCY STANDARD. COUPON FOR USE WITH INSPECTION ED-5. 05-30-10 PG.192. Includes Certification Report Tracable to NIST. | . | . | . | . | |
CRES 17-4PH | BOMBARDIER CHALLENGER EDDY CURRENT SURFACE BLOCK CRES 17-4PH STEEL. PART6 78-30-06 PAGE 27, 0.008", 0.020" and 0.040" EDM NOTCHES. | . | . | . | . | |
CRS 1 AL6061 | 6 STEP CALIBRATION BLOCK. STEP THICKNESS: 0.020", 0.040", 0.060", 0.100", 0.150", 0.200" +/- .001". STEP PAD SIZE: 1.0" x 1.0". MATERIAL: 6061-T6 ALUMINUM. Includes certification Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
CRS 2 AL6061 | 6 STEP CALIBRATION BLOCK. STEP THICKNESS: 0.100", 0.250", 0.400", 0.600", 0.800", 1.000" +/- .001". STEP PAD SIZE: 1.0" x 1.0". MATERIAL: 6061-T6 ALUMINUM. Includes certification Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
CRS AL2024 | 5 STEP CALIBRATION BLOCK. STEP THICKNESS: 0.200", 0.400", 0.600", 0.800", 1.000" +/- .001". STEP PAD SIZE: 1.0" x 1.0". MATERIAL: 2024-T351 ALUMINUM. Includes certification Report Traceable to NIST and Certificate of Conformance. | . | . | . | . | |
CW-23 OW-47 | C-130 CALIBRATION STANDARD. MATERIAL:7075-T7 or Equivalent Aluminum. FASTENER (NAS517-3-2) 2 Places. Includes Test Report and Certificate of Conformance For Standard and Certification for material and Fasteners. | . | . | . | . | |
D0815E1017-1001 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7050-T7451. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1003 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1005 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7075-T76,7050-T7451. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1007 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7075-T76,7050-T7451. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1009 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7075-T6, 7075-T7, 7050-T7. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1011 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7075-T6. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1013 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7075-T6. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1017-1015 | BOEING REFERENCE STANDARD ACCESSORY KIT-NDI, S48 HSTAB OPNG..MATERIAL: 2024-T3, 7075-T76,7050-T7451. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
D0815E1026-2001 | BOEING REFERENCE STANDARD HOLE PROBE KIT, EDDY CURRENT LARGE DIAMETER. MATERIAL: 6AL-4V Ti | . | . | .. | . | |
D0815E1033-2001 | BOEING REFERENCE STANDARD ACESSORY KIT-NDI, EDDY CURRENT AUTO HOLE. MATERIAL: 2024-T3..CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CALSS 1A | . | . | . | . | |
D0815E1033-2003 | BOEING REFERENCE STANDARD ACESSORY KIT-NDI, EDDY CURRENT AUTO HOLE. MATERIAL: 6AL-4V | . | . | . | . | |
D0815E1035-1001 | BOEING REFERENCE STANDARD ACESSORY KIT-NDI, HORIZONTAL STABILIZER. MATERIAL: 2024-T3, 6AL-4V. CHEMICAL CONVERSION COATING TO MIL-DTL-5541 CLASS 1A | . | . | . | . | |
DAC ETBS AL-1T 2024-T3 0.063 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5, 06-10-02.005. MATERIAL: 2024-T3 ALUMINUM 0.063". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
DAC ETBS AL-1T/ 0.032 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02, 7075-T7 ALUMINUM .032" | . | . | . | . | |
DAC ETBS AL-1T/ 0.071 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02, 2024-T3 ALUMINUM .071" | . | . | . | . | |
DAC ETBS AL-1T/ 0.090 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02, 7075-T6 ALUMINUM .090" | . | . | . | . | |
DAC ETBS AL-1T/0.080 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02, 2024-T3 ALUMINUM .080" | . | . | . | . | |
DAC ETOH AL | Multi Purpose Calibration Standard. 13 Basic Hole Sizes; 1/8, 5/32, 3/16, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 x .005 Corner EDM Notches in each Hole, .020 x .005 Thru EDM Notch in holes less than 3/16... | . | . | . | . | |
DAC ETOH FE | Multi Purpose Calibration Standard. 13 Basic Hole Sizes; 1/8, 5/32, 3/16, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 x .005 Corner EDM Notches in each Hole, .020 x .005 Thru EDM Notch in holes less than 3/16... | . | . | . | . | |
DAC ETOH TI | Multi Purpose Calibration Standard. 13 Basic Hole Sizes; 1/8, 5/32, 3/16, 1/4, 9/32, 5/16, 11/32, 3/8, 7/16, 1/2, 9/16, 5/8 and 3/4 inch diameters. ( .030 x .030 x .005 Corner EDM Notches in each Hole, .020 x .005 Thru EDM Notch in holes less than 3/16... | . | . | . | . | |
DAC ETOH-AL.04 | 717-200 OPEN HOLE REFERENCE STANDARD. FIG. 1.20, PAGE 1. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
DAC ETOH-AL-1/2 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-1/4 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-1/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-11/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-3/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-3/4 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-3/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-5/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-5/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-7/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-AL-9/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, ALULMINUM | . | . | . | . | |
DAC ETOH-FE.08 | 717-200 REFERENCE STANDARD...FIG. 1.9, PAGE 1. MATERIAL: 4340 STEEL PER MIL-S-5000. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
DAC ETOH-FE-1/2 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-1/4 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-1/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-11/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-3/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-3/4 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-3/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-5/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-5/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-7/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-FE-9/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, 4130 STEEL | . | . | . | . | |
DAC ETOH-IT-1/2 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-1/4 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-1/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-11/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-3/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-3/4 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-3/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-5/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-5/8 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-7/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC ETOH-IT-9/16 | OPEN HOLE EDDY CURRENT REFERENCE STANDARD, TI 6AL-4V | . | . | . | . | |
DAC GSET-AL | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 7075-T6 | . | . | |||
DAC GSET-AL.01 | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 7075-T6 ALUMINUM PER QQ-Q-250/12. | . | . | . | . | |
DAC GSET-FE | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 4340 | . | . | |||
DAC GSET-FE.01 | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 4340 STEEL PER MIL-S-5000 | . | . | . | . | |
DAC GSET-MG | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 ALUMINUM BRONZE | . | . | |||
DAC GSET-SS.01 | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 303SE CRES or 301 1/2 HARD CRES STEEL. | . | . | |||
DAC GSET-TI.01 | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 6AL-4V TITANIUM PER AMS 491 or MIL-T-9046 | . | . | |||
DAPT 09-0052-00 | DOWTY AEROSPACE PROPELLERS PROBE GUIDE FIXTURE, SF340-61-A42 | . | . | . | . | |
DC-10 FIG603/15C | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628B FIG.603 SHEET 15C | . | . | . | . | |
DC-10 FIG603/15E/4340 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628D FIG.603 SHEET 15E | . | . | . | . | |
DC-10 FIG603/15E/Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628D FIG.603 SHEET 15E | . | . | . | . | |
DC-10 FIG603/15G | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628F FIG.603 SHEET 15G | . | . | . | . | |
DC-10 FIG603/23 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 635 FIG.603 SHEET 23 | . | . | . | . | |
DC-10 FIG603/24-Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 636C FIG.603 SHEET 24 | . | . | . | . | |
DC-10 FIG603/24-Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 636C FIG.603 SHEET 24 | . | . | . | . | |
DC-10 FIG603/25 | DOUGLAS DC-10 WING CLEVIS REFERENCE STANDARD 6AL-6V or 6AL-4 TITANIUM, 54-10-11 PAGE 637 FIG.603 SHEET 25 | . | , | , | . | |
DC-10 FIG603/27Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 639 FIG.603 SHEET 27 | . | . | . | . | |
DC-10 FIG603/27Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 639 FIG.603 SHEET 27 | . | . | . | . | |
DC-10 FIG603/28LOWER/Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER) | . | . | . | . | |
DC-10 FIG603/28LOWERTi | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER) | . | . | . | . | |
DC-10 FIG603/28UPPER/Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER) | . | . | . | . | |
DC-10 FIG603/28UPPER/Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER) | . | . | . | . | |
DC-10 FIG603/29Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 641 FIG.603 SHEET 29 | . | . | . | . | |
DC-10 FIG603/29Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 641 FIG.603 SHEET 29 | . | . | . | . | |
DC-10 FIG603/30-AL | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 642 FIG.603 SHEET 30 | CA12-1672B | . | . | . | |
DC-10 FIG603/39-1 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #1 | . | . | . | . | |
DC-10 FIG603/39-2 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #2 | . | . | . | . | |
DC-10 FIG603/39-3 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #3 | . | . | . | . | |
DC-10 FIG603/39-4 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #4 | . | . | . | . | |
DC-10 FIG603/43 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 655 FIG.603 SHEET 43 | . | . | . | . | |
DC-10 FIG603/5 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 617 FIG.603 SHEET 5 | . | . | . | . | |
DC3-1 | DC-3 REFERENCE STANDARD ..SECTION 3 PAGE 2 FIGURE 1.1 | . | . | . | . | |
DC3-1 F | DC-3 INSTECTION FIXTURE | . | . | . | . | |
DC-9/MD-80-1 FIG 21 | Boeing DC-9/MD-80 Reference Standard Design (1- Assembly) Figure 21, Sheet 1-5 Page 31-35, 7-5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
DHC 29116-001 | deHAVILLAND DASH 8 LFEC CALIBRATION STANDARD. PART 6 53-30-31 PAGE 7 FIGURE 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
DHC 29117-001 | deHAVILLAND DASH 8 LFEC CALIBRATION STANDARD. PART 6 53-10-21 PAGE 5 FIGURE 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
DRT74469 | ALUMINUM BLOCK 2024-T3 3/64" FLAT BOTTOM HOLE, 2.0"LX2.0"HX.375"W | . | . | |||
E190 57-001 | EMBRAER 190/195 REFERENCE STANDARD, 190:00335-99999 OR POST-MOD SB 190-57-0031/02. PART 6 57-50-00, FIGURE 1-SHEET 1&2. | . | . | . | . | |
E53-002A | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler = .040"..Filler = .031"..Stringer = .063" | . | . | . | . | |
E53-002A. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler 1 = .040"..Doubler 2 = .063"..Filler = .... | . | . | . | . | |
E53-002B | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .047"..Doubler = .050"..Filler = .047"..Stringer = .063" | . | . | . | . | |
E53-002B. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .047"..Doubler 1 = .050"..Doubler 2 = .063"..Filler = .... | . | . | . | . | |
E53-002C | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .055"..Doubler = .063"..Filler = .055"..Stringer = .063" | . | . | . | . | |
E53-002C. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .055"..Doubler 1 = .063"..Doubler 2 = .063"..Filler = .... | . | . | . | . | |
E53-002D | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .071"..Doubler = .080"..Filler = .071"..Stringer = .063" | . | . | . | . | |
E53-002D. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .071"..Doubler 1 = .080"..Doubler 2 = .063"..Filler = .... | . | . | . | . | |
E53-002E | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .080"..Doubler = .098"..Filler = .080"..Stringer = .063" | . | . | .. | . | |
E53-002E. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .080"..Doubler 1 = .098"..Doubler 2 = .063"..Filler = .... | . | . | . | . | |
E53-002F | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .098"..Doubler = .110"..Filler = .098"..Stringer = .063" | . | . | . | . | |
E53-002F. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .098"..Doubler 1 = .110"..Doubler 2 = .063"..Filler = .... | . | . | . | . | |
E53-003A | EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
E53-003B | EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
E53-003C | EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
E53-003D | EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
E53-003E | EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
E53-003F | EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
E53-004 | EMBRAER 190/195 REFERENCE STANDARD PT 6 53-23-00 pages 1-13. Material: 2024-T3 Alclad Aluminum. Repair Doubler Configuration. Includes Test Report and Certificate of Conformance. Repair Doubler = .125" Fus Skin Thickness = .098" Filler = .098" Inner Doubler = .098" | . | . | . | . | |
E54-003 | EMBRAER 170/175 CALIBRATION STANDARD PT 4 54-50-00 Embraer 170 NDT 1967 Rev. 49, pages 11-13 and Embraer 175 NDT 5893 Rev. 25, pages 10-12. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
ELT TEMPLATE-1 | EDDY CURRENT CIRCLE TEMPLATE, 0.750"Ø. 3 HOLE SIZES: .749", .750",.751". MATERIAL: 2024-T351, 0.063" | . | . | . | . | |
ELT TEMPLATE-3 | EDDY CURRENT CIRCLE TEMPLATE, SELECT RIVET SIZES. 12 HOLE SIZES: .125", .156",.187", .218", .250", .281", .312", .343", .375", .437", .500", .562". MATERIAL: 2024-T351, 0.063" | . | . | . | . | |
EM145NDI540043A | EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 606 | . | . | . | . | |
EM145NDI540047A | EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 615 | . | . | . | . | |
EO13829.001/1 | Aeronautical Engineers Australia Reference Standard Fig.2 Page 5 DOC NO: MMS13829.001/1 and REF EO: EO13829.001/1 | . | . | . | . | |
ET002 | BRANTLY CALIBRATION STANDARD | MS20426-AD3 | MS20426-AD4 | . | ||
ET-55C-3 | BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024", .028", .031", .035", .039", .044", .048", .052", .056" .059" +/-0.002, . PAD SIZE: 1.0" x 1.0" +/-0.010", Material: 2124-T8 or 7075-T7 ALUMINUM. Chromic anodize and 1 coat of CMS 565-01 primer on chem mill side only. Chemical mill from stock thickness 0.063” (1.60 Includes certification Report Traceable to NIST and Certificate of Conformance(COC) Which Specifiy Conductivity Range of 35-45% IACS. | . | . | . | . | |
ET6018 | CUSTOM SIKORSKY S61-N FLAT BOTTOM HOLE AFT REAR FUSELAGE REFERENCE STANDARD 51-10-05 FIGURE 7 (SHEETS 1-5). MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certiicate of Conformance. | . | . | . | . | |
ETBS AL-1T/2024-T3 0.032 | MD REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02 | . | . | . | . | |
ETD2015-145-108529 | CUSTOM EDDY CURRENT STANDARD, 2024-T351 ALUMINUM .063"/.050". MS20426AD5 CSK RIVET 2 PLACES | . | . | . | . | |
F12-DEL-3C1N | REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance. | . | . | . | . | |
F12-DIS-3C1N | REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DISBOND and CORE FIBERGLASS INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance. | . | . | . | . | |
F15-AL-UT-0 125 | F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65 | . | . | . | . | |
F15-AL-UT-0 175 | F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65 | . | . | . | . | |
F15-AL-UT-0 225 | F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65 | . | . | . | . | |
F15-AL-UT-0 275 | F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65 | . | . | . | . | |
F15-AL-UT-0.175-2 | F15 REFERENCE STANDARD. MATERIAL: 2024-T3, OUTBOARD TORQUE BOX REAR SPAR, 68A115101, LOWER FLANGE FASTENER HOLES. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
F15-TI-UT-0.175 | F15 REFERENCE STANDARD,6AL-4V | . | . | . | . | |
FF171-5234 | BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM ROUND 2.50" DIAMETER O.D. / 1.125" DIAMETER I.D. EDM CORNER NOTCH: .030" x .030" +0.00/-0.002 WIDE | . | . | . | . | |
FOKKER-50/60 | FOKKER 50/60 CALIBRATION STANDARD PART 6 53-30-09 PAGE 6 FIGURE 3. MATERIAL: 2024-T3 ALUMINUM. NOTE: ***DOES NOT INCLUDE 3M BELLY PROTECTIVE TAPE 8641 | . | . | . | . | |
GIMBAL CROSS BAR | BOEING CUSTOM | . | . | . | . | |
GIMBAL CROSSBAR SINGLE | BOEING CUSTOM | . | . | . | . | |
GIMBAL FRAME | BOEING CUSTOM | . | . | . | . | |
GIMBAL FRAME PLATE | BOEING CUSTOM | . | . | . | . | |
GIMBAL FRAME SINGLE | BOEING CUSTOM | . | . | . | . | |
GSE 450 | EMBRAER190/195 REFERENCE STANDARD PART 6 57-50-00 PAGE 5 FIGURE 1. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
GSE 503 | EMBRAER 190/195 REFERENCE STANDARD PT 4 53-10-00 pages 1-12 Embraer 190-NDT 2824, 270-801-B. Includes Test Report and Certificate of Conformance. | 171T17969-401 | . | . | . | |
GSE 503/171T17969-401 | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
GSE 506 | EMBRAER 170/175/190/195 CALIBRATION STANDARD. PART NUMBER 171T17973-401. Includes Test Report and Certificate of Conformance. | 171T17973-401 | . | . | . | |
HOLDER ASSEMBLY | DELRIN HOLDER ASSEMBLY | . | . | . | . | |
Honeywell ET Standard | Honeywell Eddy Current Wheel Surface Standard. Material:2024-T6 Forged Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
IIW TYPE 1 TI | TITANIUM. IIW TYPE 1 TEST BLOCK. Titanium Ultrasonic Test Block 6AL-4V Titanium. 1 "x 4"x 12". Contains 2" diameter hole and 4" radius. Also, 1/8" x 1" radius alternate reflector and 1/16" deep on echo side. Meets ASTM-E-164, MIL-STD-2154 and AWS specifications. | . | . | . | . | |
IIW TYPE 2 AL | IIW TYPE 2 REFERENCE BLOCK 7075-T6 ALUMINUM WITH FORM FITTED CASE. IIW Block Type 2 to Specification USAF T.O. 33B-1-1. Includes Certificate of Conformance and mill spec. | 20113-3 | . | . | . | |
IIW TYPE 2 SS | IIW TYPE 2 REFERENCE BLOCK 304 STAINLESS STEEL WITH FORM FITTED CASE. IIW Block Type 2 to Specification USAF T.O. 33B-1-1. Includes Certificate of Conformance and mill spec. | 20113-1 | . | . | . | |
IIW-01S | Steel IIW Type 1 Reference Block.. Steel, nickel plated, Ultrasonic IIW Type 1 Test Block made of accurately machined, ultrasonically tested materials. | 802046 | CB-01-CS | . | . | |
IIW-01SS | IIW TYPE 1 TEST BLOCK. 304 Stainless Steel. 1 "x 4"x 12". Contains 2" diameter hole and 4" radius. Also, 1/8" x 1" radius alternate reflector and 1/16" deep on echo side. Meets ASTM-E-164, MIL-STD-2154 and AWS specifications. With Case. Includes Certificate of Conformance(COC). | . | . | . | . | |
IIW-V1-AL | V-1 (A-2) IIW Angle Beam Calibration Block (Metric). Made to British Standard: BS-2704, German Standard: DIN 54-120, Australian Standard AS 2803 and ISO 2400.Thickness of 1" / 25 mm, Height of 4" / 100 mm for straight beam calibration. 4" / 100 mm rad... | V1-AL | . | . | . | |
IIW-V1-CS | V-1 IIW Block Steel with Case. Metric Ultrasonic Calibration Block. 1018 carbon steel with certification. Includes form fitted case. | V1-S | . | . | . | |
IOW-CS | Metric Ultrasonic Calibration Block | . | . | . | . | |
IRP 0125/AL2124 | 1018 carbon steel with certification. Includes form fitted case. | . | . | . | . | |
IRP 0125/ST4340 | 12 HOLE REFERENCE STANDARD. MATERIAL: AISI 4340 STEEL. HOLE SIZES: 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8", 1.00", 1 1/8". .030"(+/-0.005) x .060"(+/-0.005) x .003" +0.005/-0.000" CORNER EDM NOTCH IN EACH HOLE. Includes Test R... | . | . | . | . | |
ISO 20601 A.1 | Reference Block A.1 as per ISO 20601. Material: 1018 carbon steel (non plated), R = 30 mm, 1,5 mm Thru Side Drilled Hole (SDH). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
IW523-1822-DEV | Custom Boeing Reference Standard. Material: 7050-T74511 Aluminum. Quantity of 1 (A) .030" x .030" +/- .002" Deep and + 0.00"/-.002" Wide and 1 (B) .050" x .050" +/- .002" Deep and + 0.00"/-.002" Wide corner EDM notch (6 places). Reference standard t... | . | . | . | . | |
IW531-1858-DEV | Custom Boeing Reference Standard. Material: 7050-T74511 Aluminum. Quantity of 1 (A) .030" x .030" +/- .002" Deep and + 0.00"/-.002" Wide and 1 (B) .050" x .050" +/- .002" Deep and + 0.00"/-.002" Wide corner EDM notch (2 places). Reference standard t... | . | . | . | . | |
KC10-7025-3 ASSEMBLY | CUSTOM MANUFACTURED BOEING REFERENCE STANDARD FOR ULTRASONIC INSPECTION 101/201 | . | . | |||
KC10-7027 | BOEING REFERENCE STANDARD KC10 FUEL COMPENSATOR CUTOUT-INSPECTION.( 301 GUIDE AND 302 GUIDE ARE PART OF INSPECTION AND SOLD SEPARATELY) | . | . | . | . | |
KT56778 | MESSIER-DOWTY REFERENCE STANDARD 631-32-181 2024-T3 | . | . | . | . | |
L72 BLOCK | British Aerospace test block. Material: 2024-T3 Aluminum .128: thick. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
LINEAR MOUNT PLATE | BOEING CUSTOM PLATE | . | . | . | . | |
LUG-LOWER | Custom Lower Lug Reference Standard APE-1, Primary, D204-12769-6 ASIP Inspecrion Program. Material: 4340 Steel Plate Per AMS 6359 Annealed. | . | . | . | . | |
M346 SPAR 4 STD-1 | CUSTOM REFERENCE STANDARD, H346 SPAR 4 STD-1 HOLE INTERFACE WITH FLAPS HINGE REWORK. MATERIAL: 7050-T7451 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MAB-CS | ROMPAS BLOCK, 7075-T6 or 7075-T73 ALUMINUM ½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version). SPECIFICATION: ASTM E-164. (Includes wooden case). Note: B777-200/300 Part 4 53-40-05 Page 8 Figure 2. Includes Material Certification and Certificate of Conformance. | 6635-00-022-0367 | TB7150-1 | . | . | |
MD STEPWEDGE/AL/.020-.100 | MD STEP WEDGE, AL, .020, .040, .060 ,.080 ,.100 | . | . | . | . | |
MD STEPWEDGE/AL/.050-.250 | MD STEP WEDGE, AL, ..05, .100, .150, .200, .250 | . | . | . | . | |
MD STEPWEDGE/AL/.300-.500 | MD STEP WEDGE, AL, .300, .350, .400, .450, .500 | . | . | . | . | |
MD11/57-10-25 | MD11 REFERENCE STANDARD 57-10-25 FIG 603 (Sheet 13) Page 618. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-04-210 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K225) FIGURE 1.29, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-04-325 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 FIGURE 1.30, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-04-400 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K225) FIGURE 1.31, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-05b | MD11 SUBSURFACE ALUMINUM ETLF REFERENCE STANDARD FIG 1.10 (Sheets 1-5) Section 2-1 Pages 1-5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-05c | MD11 SUBSURFACE ALUMINUM ETLF REFERENCE STANDARD FIG 1.11 (Sheets 1-5) Section 2-1 Pages 1-5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-09 | MD11 REFERENCE STANDARD MDC-K5225 SECTION 2-1 FIG 1.22. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MD11-10 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 SECTION 2-1 PG.1 FIG.1.23.. 2024-T3 ALUMINUM | . | . | . | . | |
MD11-11 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 FIGURE 1.27 SHEETS 1-6, PG.1-6 SECTION 2-1 | . | . | . | . | |
MD90-01 | MD-90 REFERENCE STANDARD, SECTION 2-1 FIG 1.1 FASTENER (HL19PB-6-4 +NAS1252-10L + NAS679A3) | . | . | |||
MERC-03-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 301 1/4 HARD, 2024-T3 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-07-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 2024-T4 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-08-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 4340 or 4130 STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-09-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-13-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.ERIAL: 2024-T3 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-15-29-LFEC-063 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-15-29-LFEC-064 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-15-29-LFEC-065 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-17-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-17-LFEC-02 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-17-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 2024-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-20-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-22-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-25-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 4340 or 4340M STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-26-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-27-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.TOTAL OF 4 STANDARDS PER SKIN THICKNESS TABLE 1. MATERIAL: 2024-T3 or 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-27-LFEC-02 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-27-UT-01 | CUSTOM UT CURRENT REFERENCE STANDARD.MATERIAL: 2024-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
MERC-30-LFEC-01 | CUSTOM EDDY CURRENT REFERENCE STANDARD.MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT 2797 | EMBRAER 170 REFERENCE STANDARD PT 6 53-10-00 pages 4-8 figure 1 sheets 1 and 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1016 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1017 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1018 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1019 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1020 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1021 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1022 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1022 | BOEING REFERENCE STANDARD ALL MODELS PT 6 51-00-00 FIG 16.. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
NDT1022-27/6 | BOEING REFERENCE STANDARD 767 51-00-14 PT 6 FIG 3. SINGLE STANDARD WITH ALL SIX HOLES..MATERIAL(6AL-4V) TITANIUM | . | . | . | . | |
NDT1023 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1023 | BOEING REFERENCE STANDARD ALL MODELS PT 6 51-00-00 FIG 16.. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
NDT1024 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1024 | BOEING REFERENCE STANDARD ALL MODELS PT 6 51-00-00 FIG 16.. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
NDT1025 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1025 | BOEING REFERENCE STANDARD ALL MODELS PT 6 51-00-00 FIG 16.. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
NDT1026 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1026 | BOEING REFERENCE STANDARD ALL MODELS PT 6 51-00-00 FIG 16.. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance... | . | . | . | . | |
NDT1027 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1027 | BOEING REFERENCE STANDARD ALL MODELS PT 6 51-00-00 FIG 16.. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. .. | . | . | . | . | |
NDT1031 | BOEING 707 REFERENCE STANDARD 707 PART 6, 57-10-07 DETAIL 2 FIGURE 93 SHEET 7 PG.1525. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1036-P1 | BOEING POSITIONER PT 4 54-40-07 | . | . | . | . | |
NDT1036-P2 | BOEING POSITIONER PT 4 54-40-07 | . | . | . | . | |
NDT1036-P4 | BOEING POSITIONER PT 4 54-40-07 | . | . | . | . | |
NDT1037-0.032 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.036 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.040 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.050 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.063 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.072 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.080 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.090 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.100 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.110 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1037-0.125 | BOEING REFERENCE STANDARD 767 PT 6 51-00-20 FIG 2 | . | . | . | . | |
NDT1038 | BOEING REFERENCE STANDARD (ALUMINUM SKIN/CORE DEFECTS) 737/757 -PT 4 -51-00-05 PAGE 5 | . | . | . | . | |
NDT1039-0.016/0.016 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.016". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.016/0.020 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.020". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.016/0.025 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.025". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.016/0.100 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.100". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.020/0.020 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.016". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.020/0.025 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.020"/0.025". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.020/0.032 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.020"/0.032". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.025/0.025 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.030/0.030 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.030"/0.030". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.032/0.032 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.032"/0.032". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.032/0.036 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.032/0.050 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.032"/0.050". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.036/0.036 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.040/0.020 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.040/0.032 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.040/0.036 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.040/0.040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.040/0.050 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.040"/0.050". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.040/0.056 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.045/0.040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.050/0.040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.050/0.056 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.050/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.050/0.080 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.063/0.040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.063/0.056 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.063/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.063/0.080 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 PAGE 5 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.071/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.080/0.025 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.080/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-0.080/0.100 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1039-T1/T2 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1040 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1041 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.250” DIAMETER. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1042 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.313” DIAMETER. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1043 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1044 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.438” DIAMETER. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1045 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.500” DIAMETER. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1047 | BOEING 737 REFERENCE STANDARD PART 6 51-00-00 PAGE 5 FIGURE 1. MATERIAL: LOW ALLOY 4000 SERIES STEEL 4130. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1048 | BOEING REFERENCE STANDARD 51-00-01 PT 6 FIG 5 FASTENER (BACB30JC8, BACR15BA8DD, BACC30M8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1061 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 FASTENER (BACB30JC8, BACB30NY8K). Includes Test Report and Certificte of Conformance. | . | . | . | . | |
NDT1062 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 24 FASTENER (BACB30NF4 + AN960-416, BACB30NM4K + AN960D-416). Includes Test Report and Certificte of Conformance. | . | . | . | . | |
NDT1069A | BOEING REFERENCE STANDARD 737 pt 6 53-30-19 FIGURE 3 SHEET 1 PAGE 9. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1069B | BOEING REFERENCE STANDARD 737 PT 6 53-30-19 FIGURE 3 SHEET 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1071 | BOEING REFERENCE STANDARD 767 PT 6 51-00-22 | . | . | . | . | |
NDT1072 | BOEING REFERENCE STANDARD PT 6, 51-00-00 fig. 13 PG.11 . MATERIAL-301 1/2 HARD. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1073 | BOEING 747 REFERENCE STANDARD PT 6 51-00-00, PG.12 FIG 13 DETAIL 5 FASTENER (BACB30JC8, BACB30NY8K) | . | . | . | . | |
NDT1074 | BOEING 747 REFERENCE STANDARD PT 6 51-00-00, PG.11 FIG 24 FASTENER (BACB30NF4 + AN960-416, BACB30NM4K + AN960D-416) | . | . | . | . | |
NDT1075 | BOEING 747 REFERENCE STANDARD PT 6 51-00-00, PG.14 FIG 13 DETAIL 7 FASTENER (BACR15BB6) | . | . | . | . | |
NDT1080 | BOEING REFERENCE STANDARD 767 PT 6 53-00-07 FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, BACR15BB7AD-4, BACR15BB8AD-4, ALL ALODINE) | . | . | . | . | |
NDT1081 | BOEING REFERENCE STANDARD 767 PT 6 53-00-07 FASTENER (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE) | . | . | . | . | |
NDT1083 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-.157 | BOEING REFERENCE STANDARD 737 PART 6 51-00-00 FIG.3 PG. 8, 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. HOLE SIZE: .157"Ø Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1083-.5625 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-.630 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.5620 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.563 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.625 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.630 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.688 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.695 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.750 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.787 | BOEING REFERENCE STANDARD 767 PT 6 51-00-16 PAGE 7 FIG 3 | . | . | . | . | |
NDT1083-0.812 | BOEING REFERENCE STANDARD 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1083-0.813 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.875 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-0.938 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-1.000 | BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3 | . | . | . | . | |
NDT1083-1.286 | BOEING REFERENCE STANDARD 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1083-1.347 | BOEING REFERENCE STANDARD 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance. | |||||
NDT1084 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 | . | . | . | . | |
NDT1084-.096 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. .096" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. HOLE DIAMETER = .096"Ø | . | . | . | . | |
NDT1084-.562 | BOEING REFERENCE STANDARD 737&747 55-10-26, 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-.5625 | BOEING REFERENCE STANDARD 737&747 55-10-26, 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.09375 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. 3/32" DIAMETER HOLE. Includes Test Report and Certificate of Conformance.3/32" DIAMETER HOLE. | . | . | . | . | |
NDT1084-0.122 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.125 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.127 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 PAGE 9 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.129 | BOEING REFERENCE STANDARD 787 PT 6 51-00-02 FIGURE 3, PAGE 7 and 8, 0.129" DIAMETER HOLE | . | . | . | . | |
NDT1084-0.156 | BOEING REFERENCE STANDARD 787 PT 6 51-00-02 FIGURE 3, PAGE 7 and 8, 0.156" DIAMETER HOLE | . | . | . | . | |
NDT1084-0.157 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.157" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.161 | BOEING REFERENCE STANDARD 767, PT 6 51-00-16 PAGE 7 AND 777, PART 6 51-00-02 PAGE 8 FIG. 3 | . | . | . | . | |
NDT1084-0.218 | BOEING REFERENCE STANDARD 787 PT 6 51-00-02 FIGURE 3, PAGE 7 and 8, 0.218" DIAMETER HOLE | . | . | . | . | |
NDT1084-0.234 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.234" (15/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.265 | BOEING REFERENCE STANDARD 787 PT 6 51-00-02 FIGURE 3, PAGE 7 and 8, 0.265" DIAMETER HOLE | . | . | . | . | |
NDT1084-0.281 | BOEING REFERENCE STANDARD 787 PT 6 51-00-02 FIGURE 3, PAGE 7 and 8, 0.281" DIAMETER HOLE | . | . | . | . | |
NDT1084-0.297 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.297" (19/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.328 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.328" (21/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.359 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.359" (23/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.391 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.391" (25/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.422 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.422" (27/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.453 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.453" (29/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.469 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.469" (15/32")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.484 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.484" (31/64")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.531 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.531" (17/32")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.562 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.562" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.563 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.563" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.578 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.562" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | |||||
NDT1084-0.594 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.594" (19/32")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.600 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.600" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | .. | . | |
NDT1084-0.625 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.625" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.630 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.630" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.640 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.640" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.656 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.656" (21/32")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.675 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. Hole Size: .675" Ø | . | . | . | . | |
NDT1084-0.688 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.688" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.689 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.689" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.695 | BOEING REFERENCE STANDARD 767 PT 6 51-00-16 PAGE 7 | . | . | . | . | |
NDT1084-0.700 | BOEING REFERENCE STANDARD 737 51-00-00 FIGURE 3 and 767 PT 6 51-00-16 PAGE 7 and 777 PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. Hole Size: .700" Ø | . | . | . | . | |
NDT1084-0.719 | BOEING REFERENCE STANDARD, ALL MODELS, PT 6 51-00-16 FIGURE 3, PAGE 7, 0.719" (23/32")DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.750 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.750" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.787 | BOEING REFERENCE STANDARD ALL PT 6 51-00-16 FIGURE 3, PAGE 7, 0.787" DIAMETER HOLE | . | . | . | . | |
NDT1084-0.813 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.813" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.875 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.875" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.906 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.5776" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.938 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 0.938" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-0.XXX | BOEING 777 PART 6 51-00-02 FIG.3..REFERENCE STANDARD WITH CUSTOM HOLE SIZE TO BE DETERMINED BY CUSTOMER | . | . | . | . | |
NDT1084-1.000 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 1.000" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.062 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 1.062" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.100 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3, 1.10" DIAMETER HOLE | . | . | . | . | |
NDT1084-1.124 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3. Includes Test Report and Certificate of Conformance 1.124"Ø DIAMETER HOLE | . | . | . | . | |
NDT1084-1.125 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9, 767 PT 6 51-00-16 PAGE 7, 777 & 787 PT 6 51-00-02 PAGE 7-8, 1.125" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.187 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.187" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.200 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3. Includes Test Report and Certificate of Conformance 1.200"Ø DIAMETER HOLE | . | . | . | . | |
NDT1084-1.250 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.250" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.300 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3. Includes Test Report and Certificate of Conformance 1.300"Ø DIAMETER HOLE | . | . | . | . | |
NDT1084-1.312 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3. Includes Test Report and Certificate of Conformance 1.312"Ø DIAMETER HOLE | . | . | . | . | |
NDT1084-1.3605 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3 1.3605" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.375 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.375" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.400 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3 1.400" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.437 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.437" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.500 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.500" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.625 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.625" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.750 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.750" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.875 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.875" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.940 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 1.940" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-1.9855 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Procedure 16 Figure 3, 757 Part 6 51-00-16 Page 9 Figure 3, 777-200/300 Part 6 51-00-02 Page 9 Procedure 3 Figure 3 1.9855" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-11.5MM | Custom Hole Reference Standard, Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Material: 2024-T3 Aluminum. Hole Size: 11.5mm, Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-14.4MM | Custom Hole Reference Standard, Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Material: 2024-T3 Aluminum. Hole Size: 14.4mm, Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-14.6MM | Custom Hole Reference Standard, Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Material: 2024-T3 Aluminum. Hole Size: 14.6mm, Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-17.4MM | Custom Hole Reference Standard, Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Material: 2024-T3 Aluminum. Hole Size: 17.4mm, Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-17.5MM | Custom Hole Reference Standard, Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Material: 2024-T3 Aluminum. Hole Size: 17.5mm, Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-2.000 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8 2.00" DIAMETER HOLE. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1084-2.250 | BOEING REFERENCE STANDARD 777 PT 6 51-00-02 PAGE 7-8 2.250" DIAMETER HOLE | . | . | . | . | |
NDT1084-27.6MM | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance 27.6mm"Ø DIAMETER HOLE | . | . | . | . | |
NDT1085-032 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-036 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-050 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-063 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-071 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-080 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-090 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-100 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-112 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1085-125 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-032 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-040 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-050 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-060 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-070 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-080 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-090 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-100 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-110 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1086-120 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-1 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT 6 53-30-09 .050/.040 FASTENER(NAS1097D6-5D, NAS1097D5-4D, ALL ANODIZED) ( BACR15GF6D5, BACR15GF5D4, ALL ALODINE). INCLUDES NDT1087-P1 POSITIONERS. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-10 | BOEING REFERENCE STANDARD, 767 PT6 53-30-11, PG.7-9, .132"/.056". Includes Certification Report. | . | . | . | . | |
NDT1087-11 | BOEING REFERENCE STANDARD, 757 PT6 53-00-11 .140 / .080 | . | . | . | . | |
NDT1087-12 | BOEING REFERENCE STANDARD, 757 PT6 53-00-11 PAGE 8, .120 / .063 | . | . | . | . | |
NDT1087-13 | BOEING REFERENCE STANDARD, 757 PT6 53-00-11 PAGE 8, .140 / .063 | . | . | . | . | |
NDT1087-14 | BOEING REFERENCE STANDARD, 757 PT6 53-00-11 PAGE 8, .160 / .100 | . | . | . | . | |
NDT1087-2 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT 6 53-30-09. .071/.040 FASTENER(NAS1097D6-5D, NAS1097D5-4D, ALL ANODIZED) ( BACR15GF6D5, BACR15GF5D4, ALL ALODINE). INCLUDES NDT1087-P1 POSITIONERS. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-3 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT 6 53-30-09, .080/.040 FASTENER(NAS1097D6-5D, NAS1097D5-4D, ALL ANODIZED) ( BACR15GF6D5, BACR15GF5D4, ALL ALODINE). INCLUDES NDT1087-P1 POSITIONERS. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-4 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .090/.040 FASTENER (NAS1097D6-5D, NAS1097D5-5D, ALL ALODIZED) (BACR15GF6D5, BACR14GF5D5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-5 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .100/.050 FASTENER (NAS1097D6-6D, NAS1097D5-5D, ALL ALODIZED) (BACR15GF6D6, BACR15GF5D5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-6 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .071/.063 FASTENER (NAS1097D6-6D, NAS1097D5-6D, ALL ALODIZED) (BACR15GF6D6, BACR14GF5D6, ALL ALODINED). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-7 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .090/.080 FASTNER (NAS1097D6-6D, NAS1097D5-6D, ALL ALODIZED) (BACR15GF6D6, BACR15GF5D6, ALL ALODINED). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-8 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .100/.090 FASTENER (NAS1097D6-6DM NAS1097D5-6D, ALL ALDOIZED) (BACR15GF6D7, BACRGF5D6, ALL ALODINED). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1087-9 | BOEING REFERENCE STANDARD,. Includes Certification Report. | . | . | . | . | |
NDT1087-P1 | PROBE GUIDE USED WITH NDT1087 SERIES REFERENCE STANDARDS. BOEING 737 PART 6 53-30-00 and 777 PART 6 53-00-09 PAGE 9 FIGURE 3 | . | . | . | . | |
NDT1088-050/063 | BOEING REFERENCE STANDARD 737 53-30-24 PT 6 FIG 2 | . | . | . | . | |
NDT1088-062/071 | BOEING REFERENCE STANDARD 737 53-30-24 PT 6 FIG 2 | . | . | . | . | |
NDT1088-072/050 | BOEING REFERENCE STANDARD 757 53-30-09 PT 6 FIG 2 FASTENER (BACR15CE6D4) | . | . | . | . | |
NDT1088-095/071 | BOEING REFERENCE STANDARD 737 53-30-24 PT 6 FIG 2 | . | . | . | . | |
NDT1088-112/100 | BOEING REFERENCE STANDARD 737 53-30-24 PT 6 FIG 2 | . | . | . | . | |
NDT1088-133/071 | BOEING REFERENCE STANDARD 737 53-30-24 PT 6 FIG 2 | . | . | . | . | |
NDT1088-144/050 | BOEING REFERENCE STANDARD 737 53-30-24 PT 6 FIG 2 FASTENER (BACR15CE6D4) | . | . | . | . | |
NDT1088-156/100 | BOEING REFERENCE STANDARD 757 53-00-13 PT 6 FIG 3 PAGE 7 | . | . | . | . | |
NDT1088-180/180 | BOEING REFERENCE STANDARD 757 53-00-13 PT 6 FIG 5 PAGE 9 | . | . | . | . | |
NDT1089-.500 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-.626 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-.750 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-0.157 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø0.157" | . | . | . | . | |
NDT1089-0.563 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance.Hole Ø 0.563" | . | . | . | . | |
NDT1089-0.600 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. HOLE SIZE: 0.600". Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-0.625 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.625" | . | . | . | . | |
NDT1089-0.656 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-0.660 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-0.688 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.688" | . | . | . | . | |
NDT1089-0.750 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.750" | . | . | . | . | |
NDT1089-0.813 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.813" | . | . | . | . | |
NDT1089-0.875 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.875" | . | . | . | . | |
NDT1089-0.938 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.938" | . | . | . | . | |
NDT1089-1.000 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 1.000" | . | . | . | . | |
NDT1089-1.375 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-1.375 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-1.438 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-1.438 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-1.500 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-1.500 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1089-1.9855 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | |||||
NDT1092-.050/.040 | BOEING REFERENCE STANDARD 737 PT9 51-00-03 | . | . | . | . | |
NDT1092-.071/.056 | BOEING REFERENCE STANDARD 737 PT9 51-00-03 | . | . | . | . | |
NDT1094-040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-040-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4, #49) | . | . | . | . | |
NDT1094-050 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-050/010-A | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 FASTENER (BACR15GF5D-4, #49) | . | . | . | . | |
NDT1094-050-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4, # 49) | . | . | . | . | |
NDT1094-070 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-070-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4, #49) | . | . | . | . | |
NDT1094-090 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-090-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4, #49) | . | . | . | . | |
NDT1094-110 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-5,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-110-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-5, #49) | . | . | . | . | |
NDT1094-130 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-5,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-130-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-5, #49) | . | . | . | . | |
NDT1094-155 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-6,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-155-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-6, #93) | . | . | . | . | |
NDT1094-185 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-7,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-185-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 PAGE 4. FASTENER: (BACR15GF5D-6). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-215 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-8,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-215-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-8, #50) | . | . | . | . | |
NDT1094-245 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-8,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-245-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-8, #50) | . | . | . | . | |
NDT1094-275 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-9,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-275-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2FASTENER (BACR15GF5D-8, #50) | . | . | . | . | |
NDT1094-300 | BOEING REFERENCE STANDARD 737 PT 4 53-30-07 & 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-9,). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1094-300-A | BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-8, #50) | . | . | . | . | |
NDT1096-040 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTNER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-040-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-050 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-050-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-070 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-070-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-090 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-090-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-4). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-110 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-5). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-110-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-5). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-130 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-5). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-130-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-5). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-155 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-6) . Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-155-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-6). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-185 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-6). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-185-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-6). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-215 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-7). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-215-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-7). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-245 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-245-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-275 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-275-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-300 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1096-300-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. FASTENER (BACR15GF5D-8). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1097-A | BOEING REFERENCE STANDARD PT 6 53-30-25 FIG 2. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
NDT1097-B | BOEING REFERENCE STANDARD PT 6 53-30-25 FIG 2. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
NDT1097-C | BOEING REFERENCE STANDARD PT 6 53-30-25 FIG 2. Includes Certification Report and Certificate of Conformance. | . | . | . | . | |
NDT1099 | BOEING REFERENCE STANDARD 757 PT 6 53-30-14 Page 5 Figure 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT1099G-P1 | BEOING REFERENCE STANDARD 757 PT 4 53-30-04 FIG 3. *** SEE FINALIZED DRAWING*** | . | . | . | . | |
NDT1102-100 | BOEING REFERENCE STANDARD 787 PT 6 51-00-11 | . | . | . | . | |
NDT1102-200 | BOEING REFERENCE STANDARD 787 PT 6 51-00-11 | . | . | . | . | |
NDT1102-300 | BOEING REFERENCE STANDARD 787 PT 6 51-00-11 | . | . | . | . | |
NDT1102-400 | BOEING REFERENCE STANDARD 787 PT 6 51-00-11 | . | . | . | . | |
NDT1102-500 | BOEING REFERENCE STANDARD 787 PT 6 51-00-11 | . | . | . | . | |
NDT1102-600 | BOEING REFERENCE STANDARD 787 PT 6 51-00-11 | . | . | . | . | |
NDT1106 | BOEING REFERENCE STANDARD 737 PT. 4; 51-00-05 PG.5-6; FIG.1. Includes C-Scan Report and Certificate of Conformance. | . | . | . | . | |
NDT194B | BOEING REFERENCE STANDARD PT 6 53-30-02. SHEET 1&2. PAGE 6&7 FIGURE 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT194C | BOEING REFERENCE STANDARD PART 6 53-30-00 PAGE 10 FIGURE 6 PROCEDURE 3. MATERIAL: 2024-T3 OR T4 CLAD ALUMINUM. | . | . | . | . | |
NDT2015 | BOEING REFERENCE STANDARD 727 PT 4 54-30-27. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT2016 | BOEING REFERENCE STANDARD 727 PT 6 54-40-27 FASTENER (HL31-10-5, NUT OR COLLAR) | . | . | |||
NDT2017 | BOEING REFERENCE STANDARD, 727 PART 4 57-10-27 FIGURE 1 PAGE 6. MATERIAL: 2024-T3 or 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT2019 | BOEING REFERENCE STANDARD 727 PT 6 57-40-27 DETAIL II. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT2024 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
NDT2025 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
NDT2026 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
NDT2027 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
NDT2028 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
NDT2029 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 | . | . | . | . | |
NDT2031 | BOEING REFERENCE STANDARD 727 PART 6 55-30-27 FIGURE 3 PAGE 22. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT2032-A | BOEING REFERENCE STANDARD 727 PT 6 57-10-28 FASATENER (BACR15BB8) | . | . | . | . | |
NDT2033 | BOEING REFERENCE STANDARD, 727 PART 6 57-53-03 FIGURE 2 PAGE 6. MATERIAL:4340M OR 4330M STEEL. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT297 | BOEING REFERENCE STANDARD 727 PART 4 32-30-27 PROCEDURE 5 PAGE 10 FIGURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT298 | BOEING REFERENCE STANDARD 727 PART 4 32-30-27 PROCEDURE 5 PAGE 11 FIGURE 1. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3001 | BOEING REFERENCE STANDARD, 737 53-10-02 FIG 2, PAGE 8 | . | . | . | . | |
NDT3004 | BOEING REFERENCE STANDARD PART 6 53-30-10 FIGURE 2 (SHEET1&2) PAGE 9&10. | . | . | . | . | |
NDT3005 | BOEING REFERENCE STANDARD 737 PT 6 53-30-13 FASTENER (BACB30JC5-1) | . | . | . | . | |
NDT3008 | BOEING REFERENCE STANDARD 737 PT 6 54-40-01 | . | . | . | . | |
NDT3009 | BOEING REFERENCE STANDARD 737 PT 6 54-40-01 | . | . | . | . | |
NDT3010 | BOEING REFERENCE STANDARD 737 PT 6 54-40-01 | . | . | . | . | |
NDT3011 | BOEING REFERENCE STANDARD PART 6 53-30-10 FIGURE 2 (SHEET1&2) PAGE 9&10. | . | . | . | . | |
NDT3012 | BOEING REFERENCE STANDARD 737 PART 4 53-10-03 FIGURE 3 PAGE 8. | . | . | . | . | |
NDT3014-A | BOEING REFERENCE STANDARD 737 PART 4 27-00-01 FIGURE 5 PAGE 13. | . | . | . | . | |
NDT3014-B | BOEING REFERENCE STANDARD 737 PART 4 27-00-01 FIGURE 5 PAGE 13. | . | . | . | . | |
NDT3015 | BOEING REFERENCE STANDARD 737 PT 6 53-30-15 FASTENER (BACB20NW6K5Y + BACC3R6, BACB30VU8K5 + BACC30BL8, BACR15CE6D6) | . | . | . | . | |
NDT3019 | BOEING REFERENCE STANDARD 737 PT 6 53-30-16 FIG 1 & 727 PT 6 53-30-27 FIG.17 SHEET 5 PAGE 115. FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, ALL ALODINE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3021 | BOEING REFERENCE STANDARD, Part 4 57-50-01 Page 8 Figure 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3023 | BOEING REFERENCE STANDARD 737 PT 4 32-10-02 FIG 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3023P1 | TRANSDUCER POSITIONER 32-10-02 PT 4 FIG 2. Includes Certificate of Conformance. | . | . | . | . | |
NDT3023P2 | TRANSDUCER POSITIONER 32-10-02 PT 4 FIG 2 SHOE GUIDE. Includes Certificate of Conformance. | . | . | . | . | |
NDT3023P3 | TRANSDUCER POSITIONER 32-10-02 PT 4 FIG 2 SHOE GUIDE. Includes Certificate of Conformance. | . | . | . | . | |
NDT3024A | BOEING REFERENCE STANDARD 737 PT 4 53-10-04. Includes test report and Certificate of Conformance. | . | . | . | . | |
NDT3030 | BOEING REFERENCE STANDARD 737 PT 4 57-10-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3038 | BOEING REFERENCE STANDARD 737 57-50-02 PT 4 FIG 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3038-P1 | BOEING TRANSDUCER POSITIONER 737 57-50-02 PT 4 FIG 3. Includes Certificate of Conformance | . | . | . | . | |
NDT3039 | BOEING REFERENCE STANDARD 737 53-30-04 PT 4 FIG 2 SHEETS 1&2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3041 | BOEING REFERENCE STANDARD PT 6 57-50-15 PAGE 7 FIGURE 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3046 | BOEING REFERENCE STANDARD 767 PT 4 53-20-01. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3048D | BOEING REFERENCE STANDARD 737 PART 6 53-10-56 FIGURE 4. | . | . | . | . | |
NDT3049 | BOEING REFERENCE STANDARD 737 PT 6 53-10-67 FASTENER (BAC30FN6A8 + BACC30M6, BAC30FN6A9 + BACC30M6, BACB30FN8A8 + BACC30M8, BACB30FN8A9 + BACC30M8). Includes test report and Certificate of Conformance. | . | . | . | . | |
NDT3050 | BOEING REFERENCE STANDARD PT 6 53-30-20 FIG 2. Includes Test Report and Certificate of Conformance. (SCREW AND NUT) | . | . | . | . | |
NDT3052 | BOEING REFERENCE STANDARD 737 pt 6 57-10-26 FASTENER (BACB30YP12K12 + BACC30M12, BAC30YP12K14 + BACC30M12) | . | . | . | . | |
NDT3053 | BOEING REFERENCE STANDARD 737 PT 6 53-30-21 FASTENER (BACR15CE). Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3054 | BOEING REFERENCE STANDARD 737 PART 4 57-10-04 FIGURE 2 PAGE 12 | . | . | . | . | |
NDT3062 | BOEING REFERENCE STANDARD 737 PART 4 57-10-02 FIGURE 2 PAGE 8 | . | . | . | . | |
NDT3065 | BOEING REFERENCE STANDARD 767 PT 6 53-00-12 FIG 2.707, 727, 737, 747 Aircrafts; Part 6, 53-30-22. On 737 Aircraft; Part 4, 53-30-06. On 757, 767 Aircrafts; Part 6, 53-00-09. On 777 Aircraft; Part 6,53-00-07. Includes Test Report and certificate of Conformance. FASTENER(BACR15CE5D4). | . | . | . | . | |
NDT3065-STL | BOEING REFERENCE STANDARD 777 PT 6 53-00-07 FASTENER (BACR15CE5D4) | . | . | . | . | |
NDT3068 | BOEING REFERENCE STANDARD 52-10-02 PT 4 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3070 | BOEING REFERENCE STANDARD 737 PART 6 57-10-30 FIGURE 2 PAGE 4 | . | . | . | . | |
NDT3071 | BOEING REFERENCE STANDARD 737 PT 6 53-10-65 FASTENER (BACR15GF5D8, BAC15GF5D6) | . | . | . | . | |
NDT3073 | BOEING REFERENCE STANDARD 737 PT 6 57-10-31 FASTENER (BACB30YP10K11 + BACC30M10, BACB30YP10K13 + BACC30M10, BACB30YP10K15 + BACC30M10) | . | . | . | . | |
NDT3077 | BOEING REFERENCE STANDARD 737 PT 6 53-10-69 FASTENER (BACB30FN6A4 + BACC30M6, BACB30FN6A5 + BACC30M6) | . | . | . | . | |
NDT3078 | BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 4 PAGE 9 | . | . | . | . | |
NDT3080 | BOEING REFERENCE STANDARD 737 PART 4 55-30-02 FIGURE 3 PAGE 10 | . | . | . | . | |
NDT3080-B | BOEING REFERENCE STANDARD 737 PART 4 55-30-02 FIGURE 4 PAGE 11 | . | . | . | . | |
NDT3081 | BOEING REFERENCE STANDARD 737 PT 4 55-10-01 FIG 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3082A | BOEING REFERENCE STANDARD 737 PT 6 53-10-70. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3082B | BOEING REFERENCE STANDARD 737 PT 6 53-10-70. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3082C | BOEING REFERENCE STANDARD 737 PT 6 53-10-70. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3083 | BOEING REFERENCE STANDARD 737 PART 4 55-10-03 PAGE 12 FIGURE 3. 2024-T3 ALUMINUM. | . | . | . | . | |
NDT3085A | BOEING REFERENCE STANDARD 737 PT 6 57-10-32 FIG 3 FASTENER (BACB30NX14K14, BACB30NX14K13 + BACC30BH14) | . | . | . | . | |
NDT3085B | BOEING REFERENCE STANDARD 737 PT 6 57-10-32 FIG 3 FASTENER (BACB30NX14K14, BACB30NX14K13 + BACC30BH14) | . | . | . | . | |
NDT3085C | BOEING REFERENCE STANDARD 737 PT 6 57-10-32 FIG 3 FASTENER (BACB30NX14K14, BACB30NX14K13 + BACC30BH14) | . | . | . | . | |
NDT3086A | BOEING REFERENCE STANDARD 737 PT 6 57-10-32 FASTENER (BACB30NX14K14, BACB30NX14K13, BACB30NX14K11 + BACC30BH14) | . | . | . | . | |
NDT3086B | BOEING REFERENCE STANDARD 737 PT 6 57-10-32 FASTENER (BACB30NX14K14, BACB30NX14K13, BACB30NX14K11 + BACC30BH14) | . | . | . | . | |
NDT3086C | BOEING REFERENCE STANDARD 737 PT 6 57-10-32 FASTENER (BACB30NX14K14, BACB30NX14K13, BACB30NX14K11 + BACC30BH14) | . | . | . | . | |
NDT3090A | BOEING REFERENCE STANDARD 737 PT 6 53-10-52 FIG 2 FASTENER (BACR15GF5D5, ALODINE) (AF1049U1D55C5, ANODIZED) | . | . | . | . | |
NDT3090B | BOEING REFERENCE STANDARD 737 PT 6 53-10-52 FIG 3 FASTENER (BACR15GF5D5, ALODINE) (AF1049U1D55C5, ANODIZED) | . | . | . | . | |
NDT3090C | BOEING REFERENCE STANDARD 737 PT 6 53-10-52 FIG 3 FASTENER (BACR15GF5D5, ALODINE) (AF1049U1D55C5, ANODIZED) | . | . | . | . | |
NDT3091 | BOEING REFERENCE STANDARD B737 53-30-20 PART 6 & B727 53-30-21 PT 6 FIG 2 PG. 6. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3092 | BOEING REFERENCE STANDARD 53-10-05 PT 4 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3094 | BOEING REFERENCE STANDARD PART 4 55-10-24 PAGE 14 FIGURE 4. MATERIAL: 2024-T3 or 7075-T6 ALUMINUM | . | . | . | . | |
NDT3098 | BOEING REFERENCE STANDARD 737 PT 4 55-10-07 FIG 2 | . | . | . | . | |
NDT3099 | BOEING REFERENCE STANDARD 737 PART 4 55-10-06 | . | . | . | . | |
NDT3100 | BOEING REFERENCE STANDARD 737 PT 4 55-10-08. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3101 | BOEING REFERENCE STANDARD 737 PT 4 55-10-12 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3102 | BOEING REFERENCE STANDARD 737 PT 4 55-10-10 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3104 | BOEING REFERENCE STANDARD 737 PT 4 55-10-04 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3105 | BOEING REFERENCE STANDARD 737 PT 4 55-10-15 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3106 | BOEING REFERENCE STANDARD 737 PT 6 55-10-30 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3107 | BOEING REFERENCE STANDARD 737 PT 4 55-10-09 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3109 | BOEING REFERENCE STANDARD 737 PT 4 53-80-01 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3111 | BOEING REFERENCE STANDARD 737 PT 4 55-10-05 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3112 | BOEING REFERENCE STANDARD PART 4 57-50-05 PAGE 7 FIGURE 2. MATERIAL: 15-5PH STEEL | . | . | . | . | |
NDT3114 | BOEING REFERENCE STANDARD 737 PART 6 53-30-31 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3115 | BOEING REFERENCE STANDARD 737 PART 6 53-30-31 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | . | , | . | .. | |
NDT3116 | BOEING REFERENCE STANDARD 737 PT 4 53-10-06 FIG 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3117 | BOEING REFERENCE STANDARD 737 PT 6 54-40-03 FASTENER (BUTTON HEAD AND NUT) | . | . | . | . | |
NDT3118 | BOEING REFERENCE STANDARD, 737 PT6 52-30-01: FIG 3 PG 6 FASTENER (BACR15GF5D5, BACR15GF6D5, BACR30FN6A2 + BACC30M6).. | . | . | . | . | |
NDT3120 | BOEING REFERENCE STANDARD, 737 PT6 55-10-28: FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3121 | BOEING REFERENCE STANDARD, 737 PT6 55-10-28: FIGURE 3 PAGE 8. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3122 | BOEING REFERENCE STANDARD 737 PART 4 55-10-20 PAGE 14 FIGURE 2. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3123 | BOEING REFERENCE STANDARD 737 PART 4 55-10-20 PAGE 15 FIGURE 3. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3124 | BOEING REFERENCE STANDARD 737 PART 4 55-10-20 PAGE 16 FIGURE 4. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3125 | BOEING REFERENCE STANDARD PART 4 55-10-25 FIGURE 2 PAGE 18. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3126 | BOEING REFERENCE STANDARD PART 4 55-10-25 FIGURE 3 PAGE 19. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3127 | BOEING REFERENCE STANDARD PART 4 55-10-25 FIGURE 4 PAGE 20. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3129 | BOEING 737 REFERENCE STANDARD PART 6, 53-11-34 PAGE 8 FIGURE 2. FASTENER = BACB30VU8K BOLT and BACC30BL8 COLLARS | |||||
NDT3130 | BOEING REFERENCE STANDARD 737, PART 6 53-30-37 PAGE 8 FIGURE 2. FASTENER (BACB30VU8K + BACC30BL8). Includes Test Report and Certificate of Conformance. | |||||
NDT3131 | BOEING REFERENCE STANDARD 737 PT 6 -53-11-10 FIG 2 | . | . | . | . | |
NDT3132 | BOEING REFERENCE STANDARD 737 PT 6 -53-11-18 FIG 2 | . | . | . | . | |
NDT3132B | BOEING REFERENCE STANDARD 737 PT 6 -53-11-18 FIG 3 | . | . | . | . | |
NDT3133 | BOEING REFERENCE STANDARD 737 PT 6 -53-11-16 FIG 2 | . | . | . | . | |
NDT3136 | BOEING REFERENCE STANDARD 737 PT 4 55-10-14 FIG 2 | . | . | . | . | |
NDT3137 | BOEING REFERENCE STANDARD 737 PT 6 57-50-30 FASTENER (BACB30XD3K3 + BACN10YF32, BACB30VU6K5 + BACC30BL6, BACB30VT8K5 + BACC30BL6) | . | . | . | . | |
NDT3139 | BOEING REFERENCE STANDARD 737 9T 4 53-10-07. Includes Test Report and Certificate of Conformance. | . | . | . | . | |
NDT3141 | BOEING REFERENCE STANDARD 737 PT 4 55-10-13 FIG 2. MATERIAL: 6AL-4V TITANIUM | . | . | . | . | |
NDT3141G1 | TRANSDUCER GUIDE 737 PT 4 55-10-13 FIG 3 | . | . | . | . | |
NDT3142 | BOEING REFERENCE STANDARD 737 PT 6 53-11-08 FIG 2 FASTENER (BACR15FT6D) | . | . | . | . | |
NDT3144 | BOEING REFERENCE STANDARD 737 PART 4 55-10-16 PAGE 6 FIGURE 2. MATERIAL: 7075-T6 ALUMINUM | . | . | . | . | |
NDT3145 | BOEING REFERENCE STANDARD 737 PART 4 55-10-16 PAGE 7 FIGURE 3. MATERIAL: 7075-T6 ALUMINUM | . |