| 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 |
|
| 10-0108-00 |
|
|
| 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 |
|
| 1003 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 14 and 51-00-06 |
|
| 1004 |
BOEING REFERENCE STANDARD PT 6 51-00-0 FIG 14 PARAGRAPPH 2.C. |
|
| 1005 |
BOEING REFERENCE STANDARD PT 6 51-00-00 and 51-00-06, MATERIAL: 6AL-4V TITANIUM |
|
| 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 |
|
| 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-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.53-1-MLGF-BUSHG |
MD-10 REFERENCE STANDARD FIXTURE FIGURE 1.2. MATERIAL: BLACK ACETAL(DELRIN). Includes Test Report and Certificate of Conformance. MDC-99K1082 |
|
| 10RS.53-2-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.53-2&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.53-3-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 |
|
| 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 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.036 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.040 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.050 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.063 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.072 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.080 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.090 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.100 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.110 |
BOEING REFERENCE STANDARD 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. |
|
| 127-0.125 |
BOEING REFERENCE STANDARD 747 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 |
|
| 135-UTS-CRES-A |
ULTRASONIC THICKNESS STANDARD - 304 STAINLESS |
|
| 135-UTS-CUNI-D |
ULTRASONIC THICKNESS STANDARD - CUNI 70-30 |
|
| 135-UTS-FE-B |
ULTRASONIC THICKNESS STANDARD - STEEL |
|
| 135-UTS-INC-E |
ULTRASONIC THICKNESS STANDARD - INCONEL 625 |
|
| 135-UTS-MON-C |
ULTRASONIC THICKNESS STANDARD - MONEL |
|
| 145-15998-001 |
EMBRAER REFERENCE STANDARD 54-50-00 FIG 603, 4340 STEEL |
|
| 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. |
|
| 171T17969-401 |
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance. |
|
| 171T17973-401 |
EMBRAER 170/175/190/195 CALIBRATION STANDARD. PART NUMBER 171T17973-401. Includes Test Report and Certificate of Conformance. |
|
| 185 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 |
|
| 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. |
|
| 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 6. Includes Test Report and Certificate of Conformance. |
|
| 190 |
NEED DRAWING TO QUOTE |
|
| 191 |
NEED DRAWING TO QUOTE |
|
| 192 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 |
|
| 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. |
|
| 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 REFERENCE STANDARD 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) |
|
| 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. |
|
| 2-887-01-9319S |
SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T3 Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. Includes Test Report and Certificate of Conformance. |
|
| 2-887-01-9321S |
SPLITTED CONICAL CALIBRATION STANDARD IN 2024-T3 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 2024-T3 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 2024-T3 Titanium..TYPE SCCS3-7, A318 51-63-07-991-002A. 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 |
|
| 235502 |
CASA REFERENCE STANDARD 57-10-05 FIG 504B |
|
| 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. |
|
| 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. |
|
| 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..... |
|
| 29A029 |
AIRBUS SURFACE CALIBRATION STANDARD 51-63-01 PT 6 FIG 601 ALUMINUM 7075-T6 (32% IACS), 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE) +/-.03mm. 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. |
|
| 29A049 |
AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601, 304SS 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. |
|
| 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" |
|
| 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 |
|
| 313A&B |
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. |
|
| 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 |
|
| 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 |
|
| 363 |
BOEING REFERENCE STANDARD PART 6 53-30-03 FIGURE 1 PAGE 6. 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 PT 6 53-30-27 |
|
| 370 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-02 |
|
| 375 |
BOEING REFERENCE STANDARD 737 PT 4 55-10-02 |
|
| 382-57-74 82-688 |
HERCULES CALIBRATION BLOCK 382-57-74 82-688 |
|
| 4004 |
BOEING REFERENCE STANDARD 747 PART 4 53-40-01 PAGE 10 FIGURE 6. Includes Test Report and Certificate of Confromance. |
|
| 4025 |
|
|
| 4028 |
BOEING REFERENCE STANDARD 747 PART 4 57-40-03 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance. |
|
| 4057 |
BOEING REFERENCE STANDARD 747 PT 6 53-30-03 |
|
| 4340-3-0050 |
DC9 REFERENCE STANDARD S/B 57-118 SERVICE SKETCH 2671 SHEET 4 OF 7. MATERIAL: 4340 STEEL. |
|
| 497 |
BOEING REFERENCE STANDARD 767 PT 6 53-00-05 |
|
| 51-10-04-991-007-A |
Airbus A318/A319/A320/A321 51-10-04-270-802-01 Page 4, Measurement of Remaining Thickness in Large Blended Out Areas-Procedure A. Material: 2024-T3 Aluminum. Thickness Size: Step 1(TN) = .630" and Step 2(TR) = .024" thick. Includes Test Report and Ce... |
|
| 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. |
|
| 53-10-130/158/1 |
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 REFERENCE STANDARD SET OF 8 53-10-12 |
|
| 53-10-145/1 |
BAE 146-RJ SERIES REFERENCE STANDARD 53-20-03 PT 6 FIGURES 4&5 PAGES 8&9. 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. |
|
| 53-20-104/1 |
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. |
|
| 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. |
|
| 53-20-155/1/1 |
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. |
|
| 53-20-165 |
BAE 146 BRITISH AIRCRAFT PT 4 53-20-14, 2024-T6 |
|
| 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 |
|
| 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. |
|
| 53-30-174/177/179/1 |
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. |
|
| 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. |
|
| 55-33-101/1 |
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. |
|
| 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. |
|
| 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. |
|
| 57-20-179/1 |
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-10 PT 4 FIGURES 4 PAGE 8. Includes Test Report and Certificate of Conformance. |
|
| 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 |
|
| 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 |
|
| 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 |
|
| 717RST5 |
Boeing 717 Reference Standard 717RST5..Figure 1.18 (Sheet 1-3) MDC-96K9063 |
|
| 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... |
|
| 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... |
|
| 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) |
|
| 80RS13 |
MD-80 REFERENCE STANDARD 57.80.012 FASTENER (HLT335-6-7 + NAS1252-10L + MS21042L3, MS20426AD5, NAS1478 + NAS1080-08) |
|
| 80RS15 |
MD-80 REFERENCE STANDARD FASTENER (S4932869-06-04 + NAS1080-6, NAS1466-04 + NAS1080-6) |
|
| 80RS16 |
MD-80 REFERENCE STANDARD FASTENER (MS20470-AD5, NAS1097-AD6, NAS1097-AD5) |
|
| 80RS18 |
MD-80 REFERENCE STANDARD 53.80.003 FASTENER (S4932868-06 + NAS1080-6, 3D0009-6 + 3D0007-3, NAS1097-AD6) |
|
| 80RS19 |
MD-80 REFERENCE STANDARD FASTENER (NAS1097-AD6) |
|
| 80RS2 |
MD-80 REFERENCE STANDARD FASTENER (S4932867-10-13 + NAS1080-P1) |
|
| 80RS21 |
MD-80 REFERENCE STANDARD 54.80.002 |
|
| 80RS22 |
MD-80 REFERENCE STANDARD FASTENER (S4932868-06 + NAS1080-6) |
|
| 80RS23 |
MD-80 REFERENCE STANDARD FASTENER (MS20470-AD5, NAS1097AD6, S4932868-06-03 + NAS1080-6, 3D0009-6 + 3D0007-3) |
|
| 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) |
|
| 80RS7 |
MD-80 REFERENCE STANDARD FASTENER (S4932867-08-7 + NAS1080-08) |
|
| 80RS8 |
MD-80 REFERENCE STANDARD FASTENER (S4932868-08 + NAS1080-08) |
|
| 80RS9 |
MD-80 REFERENCE STANDARD FASTENER (S4932867-06-5 + NAS1080-06) |
|
| 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 |
|
| 98A54003072000 |
AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 FIG 403 |
|
| 98A54003073000 |
AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 FIG 404 |
|
| 98A54003074000 |
AIRBUS A300-600 CALIBRATION STANDARD PART 4 54-50-15 PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. |
|
| 98A54403026000 |
AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 |
|
| 98A57103013000 |
AIRBUS TAP TOOL . CORROSION RESISTANT STEEL-TEMPERED (LN-1.1044; MIL-S-18732 |
|
| 98D52103501000 |
|
|
| 98D57204183000 |
|
|
| 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. |
|
| 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 |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 98S53305005 |
|
|
| 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 |
|
| 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. |
|
| 98S53805008-000 |
|
|
| 98S54305001-200 |
AIRBUS REFERENCE STANDARD 54-31-70 PT 4 FIG 401 |
|
| 98S54305001-202 |
AIRBUS REFERENCE STANDARD 54-31-70 PT 4 FIG 401 |
|
| 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 |
|
| 98S57105011-200 |
ATR CALIBRATION STANDARD 57-15-11 PART 4 PAGE 403 FIGURE 401. MATERIAL: 6AL-4V TITANIUM |
|
| 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 |
|
| 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 |
|
| 98S57205029-000 |
|
|
| 99A51003000000 |
AIRBUS REFERENCE STANDARD 53-00-02 99A51003000000 FASTENER (NSA5050-3, EN6114-3-3, EN6114V-3-3) |
|
| 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 |
|
| 99A53003001101 |
AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM.. |
|
| 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 Test Report anc Certificate of Conformance... |
|
| 99A53003001104 |
AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A 6AL-4V TITANIUM. Includes Test Report anc Certificate of Conformance... |
|
| 99A53003001105 |
AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, 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, A340_500_600 51-63-05-991-001-A 2024-T3 ALUMINUM. Includes Test Report anc Certificate of Conformance. |
|
| 99A53003001107 |
AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A 6AL-4V TITANIUM. Includes Test Report anc Certificate of Conformance. |
|
| 99A53003001108 |
AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A MATERIAL: 4130 STEE. 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 53-31-81 99A53107215000 FASTENER (HL11VF6-6, HL70-6). Includes Test Report and Certificate of Conformance. |
|
| 99A53107265001 |
AIRBUS REFERENCE STANDARD A300-600 PT 6 53-19-21 FASTENER (NAS1474A4, LN9198, LN9199) |
|
| 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) |
|
| 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. 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. |
|
| 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. |
|
| 99A54403004000 |
AIRBUS REFERENCE STANDARD A300-600 A300-54-6015 |
|
| 99A55109003000 |
AIRBUS REFERENCE STANDARD A300-600 PT 4 55-10-72 FASTENER (HST756CB-6, HST881-8) |
|
| 99A55209001000 |
AIRBUS REFERENCE STANDARD A318-A321 PT 5 51-10-03 |
|
| 99A55307306000 |
MUST BE MANUFACTURED FROM AN ACTUAL AIRCRAFT!!! |
|
| 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 |
|
| 99A571004101000 |
NEED DRAWING |
|
| 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 |
|
| 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 4045/406 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) |
|
| 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 |
|
| 99A57103038000 |
|
|
| 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) |
|
| 99A57104329000 |
AIRBUS A300-600 CALIBRATION STANDARD 57-21-04 PAGE 405 FIGURE 403. Includes Test Report and Certificate of Conformance. |
|
| 99A57104330000 |
AIRBUS A300-600 CALIBRATION STANDARD 57-21-04 PAGE 406 FIGURE 404. Includes Test Report and Certificate of Conformance. |
|
| 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 |
|
| 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 |
|
| 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 |
|
| 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. Includes Test Report and Certificate of Conformance. |
|
| 99A57504296000 |
AIRBUS REFERENCE STANDARD A300 57-42-11, A300-600 57-51-34 and A310 57-51-11 PART PAGE 404 FIGURE 403 |
|
| 99D51103001000 |
NEED DRAWING |
|
| 99D51103004000 |
NEED DRAWING |
|
| 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 |
|
| 99D53103001000 |
AIRBUS REFERENCE STANDARD A318/319/320/321 NTM 53-11-82-PB6 Page 14 Figure 403.. |
|
| 99D53203000000 |
|
|
| 99D53203000002 |
AIRBUS REFERENCE STANDARD A318-A321 PT 6 53-21-86 FASTENER (ASN-A2026V3-4, ASN-A2026V3-5, ASN-A258-3) |
|
| 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) |
|
| 99D54403000003 |
Need Drawing |
|
| 99D54403000004 |
AIRBUS REFERENCE STANDARD A320 PT4 54-51-02-PB4:PG12..FIG54-51-02-991-004-A SHEET01 |
|
| 99D54403000005 |
NEED DRAWING |
|
| 99D54403000006 |
NEED DRAWING |
|
| 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. |
|
| 99D54430001002 |
Need NTM procedure |
|
| 99D54503004000 |
AIRBUS CALIBRATION BLOCK A318/A319/A320/A321: PART 4 54-53-17-991-003-A SHEET 01, PAGE7. MATERIAL: 15-5PH STEEL |
|
| 99D54503005040 |
NEED DRAWING |
|
| 99D54503005041 |
NEED DRAWING |
|
| 99D54503005042 |
NEED DRAWING |
|
| 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 |
|
| 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 |
|
| 99D57103022001 |
Need Drawing |
|
| 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 |
|
| 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 PAGE 1. 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. |
|
| 99D5710307000 |
Need NTM procedure drawing |
|
| 99D5710308000 |
Need NTM procedure drawing |
|
| 99D5710309000 |
Need NTM procedure drawing |
|
| 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.. |
|
| 99D57204129000 |
Need Drawing |
|
| 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. |
|
| 99D57204166000 |
NEED DRAWING |
|
| 99D57204167000 |
NEED DRAWING |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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 . Includes Test Report and Certificate of Conformance. |
|
| 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) |
|
| 99D57704100000 |
AIRBUS REFERENCE STANDARD A320..FIGURE 402, 57-70-06, PG. 404 |
|
| 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 |
Need Drawing |
|
| 99F53103007000 |
AIRBUS REFERENCE STANDARD A330, 53-11-82-991-003-A FASTENER (ASNA2391-3-6 + ASNA2025-3). lncludes Test Report and Certificate of Conformance. |
|
| 99F53107330000 |
Airbus A318/A319/A320/A321 Conductivity Standard Block Set SB A320 57-1190 Figure 3. Material: 2024-T3 and 2024-T0 Aluminum. .047", 063" and .080" thickness in each Aluminum Temper Painted with Primer. Includes 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 |
Need Drawing |
|
| 99F53303009000 |
AIRBUS REFERENCE STANDARD A330 PT 6 53-30-10 FASTENER (ASNA 2391-4-07 + ASNA2025-4). lncludes Test Report and Certificate of Conformance. |
|
| 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) |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 99F53303087000 |
AIRBUS REFERENCES STANDARD A330, 53-31-87-PB4 FASTENER (EN6115V3-3, NAS5050-3). lncludes Test Report and Certificate of Conformance. |
|
| 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 |
Need drawing |
|
| 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. |
|
| 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 1&2.(Rev. Jan 01,2017) |
|
| 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. |
|
| 99F53305399000 |
|
|
| 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. |
|
| 99F53407333000 |
Airbus A330 Reference Block 53-40-20-991-025-A. ludes Test Report 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. |
|
| 99F54503000000 |
MUST BE PURCHASED DIRECTLY FROM AIRBUS |
|
| 99F54503005000 |
MUST BE PURCHASED DIRECTLY FROM AIRBUS |
|
| 99F54503006000 |
NO BID. MUST BE PURCHASED DIRECTLY FROM AIRBUS |
|
| 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. |
|
| 99F54503013000 |
NO BID. MUST BE PURCHASED DIRECTLY FROM AIRBUS |
|
| 99F54503014000 |
NO BID. MUST BE PURCHASED DIRECTLY FROM AIRBUS |
|
| 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 STANDAR A330 PT 4 57-11-48. ludes 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 |
Need NTM |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 99F57204136000 |
AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403 SHEET 1 PAGE 407. Includes Test Report and Certificate of Conformance. |
|
| 99F57204137000 |
AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403. Includes Test Report and Certificate of Conformance. |
|
| 99F57204138001 |
AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403. Includes Test Report and Certificate of Conformance. |
|
| 99F57204140000 |
AIRBUS REFERENCE STANDARD A330 57-20-02 FIG 603 FASATENER (ASNA2027VHK5-13, ABS0813-5C) |
|
| 99F57204144000 |
AIRBUS REFERENCE STANDARD A330 57-20-93 FIG 403 FASTENER (ASNA2026-7-19, NSA472-7K7) |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 99L52103000000 |
AIRBUS REFERENCE STANDARD A380 52-81-01-991-012-A |
|
| 99L52107325000 |
AIRBUS REFERENCE STANDARD A380 52-11-01-01 |
|
| 99L53103004000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-09-991-003-A |
|
| 99L53103005000 |
A380 REFERENCE STANDARD 7010 ALUMINUM; FIGURE:53-11-23-991-003-A |
|
| 99L53103006000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-07-991-003-A |
|
| 99L53103008000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-11-991-003-A |
|
| 99L53103010000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-31-24-991-003-A |
|
| 99L53103012000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.53-11-22-991-009-A |
|
| 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) |
|
| 99L53303001000 |
AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-36-991--003-A |
|
| 99L53303005000 |
AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-21-991-003-A |
|
| 99L53303008000 |
AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-19-991-003-A |
|
| 99L53303009000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-31-20-991-003-A |
|
| 99L53303016000 |
A380 REFERENCE STANDARD 7075-T6 OR 7075-T7 ALUMINUM; FIGURE:53-31-30-991-003-A |
|
| 99L53303017000 |
A380 REFERENCE STANDARD 7050-T73 OR 7075-T73 ALUMINUM; FIG.53-31-30-991-009-A |
|
| 99L53303019000 |
AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-11-991-003-A |
|
| 99L53303021000 |
AIRBUS A380-800 CALIBRATION BLOCK 53-31-33-991-006-A (SHEET 01& 02) PAGES 20-21 |
|
| 99L53509001000 |
AIRBUS A380 REFERENCE STANDARD 7050-T7 OR 2024 ALUMINUM; FIGURE:53-51-02-991-008-A |
|
| 99L53509003000 |
AIRBUS REFERENCE STANDARD A380-800 53-51-08-991-004-A |
|
| 99L53509006000 |
AIRBUS REFERENCE STANDARD A380-800 53-51-37-270-801-A-01 |
|
| 99L54503000000 |
AIRBUS A380 REFERENCE STANDARD FIGURE:54-51-04-991-012-A. MATERIA L: 718 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 |
|
| 99L55209001000 |
AIRBUS REFERENCE STANDARD 55-21-03-991-003-1. 7050-T7451 ALUMINUM |
|
| 99L57203002000 |
AIRBIS REFERENCE STANDARD A380-800, 57-21-05 |
|
| 99L57203003000 |
AIRBUS A380 REFERENCE STANDARD FIGURE 57-21-02-991-003-A |
|
| 99L57203005000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.57-11-03-991-008-A |
|
| 99L57203006000 |
A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.57-11-03-991-014-A |
|
| 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. |
|
| 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 |
|
| 99N51107332000-B |
AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT |
|
| 99N51107332000-C |
AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT |
|
| 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. |
|
| 9RS1 |
DC-9 REFERENCE STANDARD FASTENER (NAS1097AD6) |
|
| 9RS11 |
MD-80 REFERENCE STANDARD...FIG.15 SHEET 1-3 .. MD-80 SID SECTION 2-1 |
|
| 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 |
DC-9 REFERENCE STANDARD 57-80-008 FASTENER (MS20470AD8, NAS1478-6 + NAS1080-8) |
|
| 9RST8 |
REFERENCE STANDARD 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 |
|
| A305 |
NEED DRAWING |
|
| A306 |
BOEING REFERENCE STANDARD 737 PART 6 57-10-07 FIGURE 1 PAGE 4. |
|
| 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. |
|
| A389B |
BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. |
|
| A389C |
BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. |
|
| 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... |
|
| 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.... |
|
| AF5-2024-T3-.020-.100 |
UT 5 STEP WEDGE .020", .040", .060", .080", .100. MATERIAL: 2024-T3 ALUMINUM |
|
| 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... |
|
| AFK-FHF-B:AF-5098RS/.875 |
BOEING DC9 REFERENCE STANDARD -57-225 |
|
| AFK-PWA28403B:PWA28403B |
PRATT & WHITTNEY ENGINE BLADE REFERENCE STANDARD |
|
| 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-1010-ALNIBR |
BOEING TOOL ST8809C LETTER CODE F Al-NI-BR |
|
| AFNDT-1010A |
BOEING TOOL ST8809C LETTER CODE B 2024-T3 ALUMINUM |
|
| 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-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-1025A |
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", 3/4" ( .030X.030 Corner Notches and .010, .020, .040 Surface notches)... |
|
| AFNDT-1025TI |
MHS style Multi-Hole reference standard (Titanium 6AL-4V 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", 3/4" ( .030X.030 Corner Notches and .010, .020, .040 Surface notches)... |
|
| 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-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-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-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-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-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. |
|
| 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-1096/6AL4V |
10 STEP REFERENCE BLOCK,.030,.040,.050,.063,.071,.080,.090,100,.120 6AL4V |
|
| AFNDT-1096SS |
10 STEP REFERENCE BLOCK .20",.40,.60,.80,1.00,1.20,1.40,1.60,1.80,2.0 304 STAINLESS |
|
| 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-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 |
|
| 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 |
|
| 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... |
|
| 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-20043RS |
EDDY CURRENT SURFACE STANDARD WITH 3 EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T3 ALUMINUM |
|
| 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-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",... |
|
| 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... |
|
| 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... |
|
| AFNDT-2006TI |
12 HOLE REFERENCE STANDARD 304 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" ... |
|
| 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-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 |
|
| 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-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" |
|
| 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. |
|
| 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-2030/17-7 |
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-2030/17-7PH |
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-2030/2024 |
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. |
|
| 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. |
|
| 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. |
|
| AFNDT-2030/4130 |
EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002, MAX.006), 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. |
|
| 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. |
|
| 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/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 |
|
| 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-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 .040", .080", .120", .160", .200", .240", .280", .320", .360", .400" +/-.001" 7075-T6 ALUMINUM .75" x .75" STEP FACE |
|
| 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-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 |
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| 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/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) |
|
| 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) |
|
| 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) |
|
| 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) |
|
| 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) |
|
| 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... |
|
| 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... |
|
| 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... |
|
| 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... |
|
| 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... |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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. |
|
| 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... |
|
| 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) |
|
| 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. |
|
| AFNDT-2048/TI |
CUSTOM NAVY BLOCK, 6AL-4V TITANIUM ,WITH 20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES NOTCHES |
|
| 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-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 |
|
| 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 |
|
| 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-2064/AL |
SAFRAN MESSIER-BUGATTI-DOWTY REFERENCE STANDARD 32-09-01 2024-T351 ALUMINUM |
|
| 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 |
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| 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) |
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| 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" |
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| 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" |
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| AFNDT-2067/1018 |
5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 1018 CRES STEEL PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| AFNDT-2067/304S |
5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 304 STAINLESS STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| AFNDT-2067/4340 |
5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 4340 CARBON STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| AFNDT-2067/7075T6 |
5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 7075-T6 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| AFNDT-2067/7075T7 |
5 STEP WEDGE .100", .200",. 300", .400", .500" MATERIAL: 7075-T7 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| 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... |
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| 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. |
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| 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. |
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| 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... |
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| 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" ±.... |
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| 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... |
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| 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. |
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| 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... |
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| 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 ... |
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| 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. |
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| AFNDT-2075/AL-1 |
5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". MATERIAL: 7075-T6 ALUMINUM .PAD SIZE: 75" x .75" . Includes Test Report traceable to NIST and Certificate of Conformance. |
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| AFNDT-2075/AL-2 |
5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". ..MATERIAL: 2024-T3 ALUMINUM .PAD SIZE: 75" x .75" . Includes Test Report traceable to NIST and Certificate of Conformance. |
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| AFNDT-2075/TI |
5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". ..MATERIAL: 6AL-4V TITANIUM . PAD SIZE: 75" x .75" . 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". Includes Test Report traceable to NIST and Certificate of Conformance. |
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| AFNDT-2075SS |
5 STEP WEDGE .020", .040", .060", .080", .100". TOLERANCE +/-.001". ..MATERIAL: 304 STAINLESS. PAD SIZE: 75" x .75" . 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. |
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| 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. |
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| AFNDT-2077/7075T6 |
5 STEP WEDGE .040", .080", .120", .160", .200" +/-.001", 7075-T6 ALUMINUM .75" x .75" STEP FACE |
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| AFNDT-2078/7075T6 |
5 STEP WEDGE .240", .280", .320", .360", .400" +/-.001", 7075-T6 ALUMINUM 1.0" x 1.0" STEP FACE |
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| 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. |
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| 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 |
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| 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 |
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| 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.. |
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| AFNDT-2086/CS |
CUSTOM 4 STEP CALIBRATION BLOCK, .250, .500, .750, 1.0, ±.001, 3/4X3/4 FACE, CARBON STEEL |
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| AFNDT-2086/SS |
CUSTOM 4 STEP CALIBRATION BLOCK, .250, .500, .750, 1.0, ±.001, 3/4X3/4 FACE, STAINLESS STEEL |
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| AFNDT-2087/CS |
5 STEP CALIBRATION BLOCK, .100, .200, .300, .400, .500, ± .001, 3/4X3/4 FACE, CARBON STEEL |
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| AFNDT-2087/SS |
5 STEP CALIBRATION BLOCK, .100, .200, .300, .400, .500, ± .001, 3/4X3/4 FACE, STAINLESS STEEL |
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| AFNDT-2088/CS |
METRIC 10 STEP CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 19mm X 19mm. Material: 4340 Carbon Steel. |
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| AFNDT-2088/SS |
METRIC 10 STEP CALIBRATION BLOCK, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm ± .05mm. Pad Size: 19mm X 19mm. Material: 304 Stainless Steel. |
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| 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. |
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| AFNDT-2090/AL |
5 STEP WEDGE .220", .240", .260", .280", .300" +/-.001", 7075-T6 ALUMINUM .75" x .75" STEP FACE.. |
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| 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. |
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| 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 |
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| AFNDT-2094/6.2 |
EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 6.2 |
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| AFNDT-2094/7.8 |
EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 7.8 |
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| AFNDT-2094/8.2 |
EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 8.2 |
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| 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. |
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| 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. |
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| 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. |
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| 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 |
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| 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 |
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| 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 |
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| AFNDT-2103AL |
METRIC 5 STEP CALIBRATION BLOCK, 7075-T6 ALUMINUM. STEP SIZES: 2.5mm, 5.0mm, 7.5mm, 10.0mm, 12.5mm. Includes Test Report and Certificate of Conformance. |
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| 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. |
|
| 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. |
|
| 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-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. |
|
| 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. |
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| 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-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 |
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| AFNDT-2113/2024 |
10 PIECE SHIM THICKNESS SET. SHIM SIZE: 0.787" x 0.787". THICKNESSES: .020", .032", .040", .050", .063", .070", .080", .090", .100", .125". Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. |
|
| 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. |
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| 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-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-2119 |
CUSTOM 5 STEP BLOCK, 6mm,7mm, 8mm, 9mm, 10mm +/- .05mm . Pad Size: .750" x .750" Material- 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. |
|
| 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-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-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-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 |
6 STEP BLOCK, 4130 STEEL, .050, .060, .070, .080, .090, .100. .750"X.750", ±.001 |
|
| 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-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-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 ... |
|
| 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 |
|
| 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 |
|
| 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 |
|
| 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 |
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| 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" |
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| 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 |
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| 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 |
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| 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. |
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| 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. |
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| 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. |
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| AFNDT-2140/7075T6 |
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. |
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| 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 NOTCH and .020" x .020" CORNER NOTCH IN EACH HOLE. Tolerance: .005" +/-.001" |
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| 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 |
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| 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... |
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| 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 |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| AFNDT-2147 |
Step Wedge: 7075-T6 Aluminium, 5 Steps total (2.5mm, 5.0mm, 7.5mm, 10.0mm and 12.5mm). Step pad size: 1” x 1”. Includes Test Report and Certificate of Conformance. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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... |
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| 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. |
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| 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. |
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| 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. |
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| 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" |
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| 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 |
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| 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 |
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| 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... |
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| 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. |
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| 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... |
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| 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 |
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| AFNDT-3005 |
Cessna Eddy Current reference standard stack per customer supplied drawing. Material: 7075-T7. Includes Test Report traceable to NIST. |
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| 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. |
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| 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. |
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| 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 |
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| AFNDT-3010/304 |
11 STEP WEDGE STEP THICKNESS OF .050", .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001" 304 STAINLESS STEEL |
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| AFNDT-3010/4340 |
11 STEP WEDGE STEP THICKNESS OF .050", .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001" 4340 STEEL |
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| AFNDT-3010/7075-T6 |
10 STEP ALUMINUM WEDGE. STEP THICKNESS OF , .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001". Material: 7075-T651 Aluminum. Includes Certification Report traceable to NIST. |
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| AFNDT-3010/7075-T7 |
11 STEP WEDGE STEP THICKNESS OF .050", .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001" 7075-T7 ALUMINUM |
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| AFNDT-3010/MAG |
11 STEP WEDGE STEP THICKNESS OF .050", .100", .200", .300", .400", .500", .600", .700", .800", .900" 1.00" +/-.001" AZ31B MAGNESIUM |
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| 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... |
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| 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... |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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 |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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 ... |
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| 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... |
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| 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... |
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| 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 ... |
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| 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... |
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| 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... |
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| 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 |
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| 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 |
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| 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 |
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| 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. |
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| AFNDT-3033AL |
5 STEP WEDGE, .100", .200",. 300", .400", .500" MATERIAL: ANODIZED 2024-T4 ALUMINUM. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| 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... |
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| 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... |
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| 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-3045-2024T3 |
10 STEP REFERENCE BLOCK .010", .020", .030", .040", .050", .060", .070", .080", .090", .100", +/-.001" . Material: 7075-T6 ALUMINUM, Pad Size: 1.0" x 1.0" . 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: 1.0" x 1.0" . Includes Test Report and Certificate of Conformance. |
|
| 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 ... |
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| 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"... |
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| 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. |
|
| AFNDT-3054/CS |
5 STEP WEDGE .100", .125",. 150", .175", .200" MATERIAL: 4340 CARBON STEEL. PAD SIZE: .75" X .75" TOLEREANCE = +/- .001 |
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| 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... |
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| 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... |
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| 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... |
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| 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 .... |
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| 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... |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. Black Anodized. Includes Test Report and Certificate of Conformance. |
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| 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 |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| AFNDT-3110C |
Custom Multi-Hole Standard made to the Specifications of 99A53003001101. Material: 2024-T351. 28 Total Hole Sizes: 27/32, 55/64, 7/8, 57/64, 29/32, 59/64. Includes Test Report and Certificate of Conformance. |
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| 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. |
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| 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. |
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| 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. |
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| 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... |
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| 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... |
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| 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... |
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| AFNDT-3117 |
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.( .050X.050 CORNER NOTCH and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.) Material: 15-5PH Stainless S... |
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| 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. |
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| 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 +/... |
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| 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 +/- .... |
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| 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... |
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| 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", ... |
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| AFNDT-3122TI |
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... |
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| 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. |
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| 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. |
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| 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 EDM Notches. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. |
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| AFNDT-3125CS |
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 and 3 SURFACE NOTCHES .010", .020", .040" DEEP x .750" LONG.). Material: 4340 Carbon Steel. Include... |
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| 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... |
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| AFNDT-3127 |
SPACEX CUSTOM HOLE STANDARD, 7050-T7 ALUMINUM. HOLE SIZES: .125",.156", .187", .218", .250", .281", .313", .343", .375", .438", .500", 563", .625", 750", .875", 1.000", 1.375", 1.500". A3 Size EDM Notches: Axial Mid-Hole and Coner Notches in each hole |
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| AFNDT-3127A |
Custom Spacex Eddy Current Surface Notch Standard to Compliment AFNDT-3127. Contains 8 EDM Surface Notches A0 thru A7. Material: 7050-T7 Aluminum. Includes Test Report and Certificate of Conformance. |
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| 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... |
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| 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... |
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| 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... |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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 |
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| AFNDT-3137AL |
13 Hole Calibration Standard, Hole Sizes; 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. ( .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 Surf... |
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| 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. |
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| 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... |
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| 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... |
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| 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 ... |
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| 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... |
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| 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... |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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 and ... |
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| 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... |
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| 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. |
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| 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. |
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| 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. |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| 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... |
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| AFNDT-PLUG |
PLUG - 54-10-33 |
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| 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. |
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| 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) |
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| AFNDT-SA227 |
FAIRCHILD REFERENCE STARDARD FOR THE SA227 DOOR use fastener MS2042AD4-10 |
|
| 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... |
|
| 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 ... |
|
| AFNDT-SRS-4A |
SURFACE STANDARD ALUMINUM(2024-T351) 1 EDM SLOT (0.040 DEEP) |
|
| AFNDT-SRS-4S |
SURFACE STANDARD STEEL 4340 1 EDM SLOT (0.40 DEEP) |
|
| AFNDT-SRS-4T |
SURFACE STANDARD TITANIUM 1 EDM SLOT (0.40 DEEP) |
|
| 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/... |
|
| 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/... |
|
| 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... |
|
| 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",... |
|
| 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/... |
|
| 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... |
|
| ANDT1015 |
BOEING REFERENCE STANDARD 53-30-00 PT 6 FIG 5 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 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 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 FASTENER (BACB30FN6-2, BACR15CE6D-2, BACR15BB8D-2). Includes Test Report and Certificate of Conformance. |
|
| ANDT1052 |
BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 FASTENER (BACB30FN8-2, BACR15CE8D-2, BACR15BB8D-2). Includes Test Report and Certificate of Conformance. |
|
| 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. |
|
| ANDT1054 |
BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 FASTENER (BACB30FN8-3, BACR158D-3, BACR15BB8D-3). Includes Test Report and Certificate of Conformance. |
|
| ANDT1055 |
BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. |
|
| ANDT1056 |
BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 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 FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. |
|
| ANDT1077 |
BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 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. Includes Test Report and Certificate of Conformance. FASTENER (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE) |
|
| 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. Includes Test Report and Certificate of Conformance.. FASTENERS: (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Inclu... |
|
| 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 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-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 SHEET 1. 2024-T351 ALUMINUM. |
|
| 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) |
|
| APN-45-4C |
SURFACE PROBE, CURVED, 50-500KHZ |
|
| ARP-.300/.750 |
DIFFERENTIAL/BRIDGE LOW FREQUENCY RING PROBE, 500HZ-10KHZ, .300"Ø ID, .750"Ø OD WITH TRIAX CONNECTOR. Includes Test Report and Certificate of Conformance. |
|
| 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 |
|
| 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-0824/2024-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-0824/7475-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-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.... |
|
| 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 |
|
| BAe 146 20-00-00 |
BAE 146-RJ SERIES REFERENCE STANDARD 20-00-00 PT 6 FIGURES 5 PAGES 9. MATERIAL: 7075-T6 Aluminum Includes Test Report and Certificate of Conformance. |
|
| 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 |
|
| 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. |
|
| 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 |
|
| 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/ 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-.04 |
BOEING REFERENCE STANDARD |
|
| 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-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 |
|
| DC-10 FIG603/30TI |
DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 642 FIG.603 SHEET 30 |
|
| 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 FIG603/43 |
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 |
|
| 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. |
|
| DC3-1 |
DC-3 REFERENCE STANDARD ..SECTION 3 PAGE 2 FIGURE 1.1 |
|
| 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. |
|
| 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. Includes Test Report and Certificate of Conformance. |
|
| E53-002B |
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. |
|
| E53-002C |
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. |
|
| E53-002D |
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. |
|
| E53-002E |
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. |
|
| E53-002F |
EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance. |
|
| 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. |
|
| 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. |
|
| EM145NDI540043A |
EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 606 |
|
| EM145NDI540047A |
EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 615 |
|
| 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-0 175-2 |
F15 REFERENCE STANDARD, 2024-T3, 1F-15A-36-2-65, STRAIGHT SHANK HOLES |
|
| 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-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 |
|
| 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. |
|
| 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. |
|
| IIW-01S |
Steel IIW Type 1 Reference Block.. Steel, nickel plated, Ultrasonic IIW Type 1 Test Block made of accurately machined, ultrasonically tested materials. |
|
| IIW-V1-S |
V-1 IIW Block Steel with Case..Metric Ultrasonic Calibration Block.. 1018 carbon steel with certification. Includes form fitted case. |
|
| 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. |
|
| 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. |
|
| IRP 0125/AL2124 |
12 HOLE REFERENCE STANDARD. MATERIAL: 2124-T851 ALUMINUM. 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 Tes... |
|
| 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... |
|
| 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. |
|
| 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 |
|
| MD11/57-10-25 |
MD11 REFERENCE STANDARD 57-10-25 FIG 603 (Sheet 13) Page 618. Includes Test Report and Certificate of Conformance. |
|
| MD90-01 |
MD-90 REFERENCE STANDARD, SECTION 2-1 FIG 1.1 FASTENER (HL19PB-6-4 +NAS1252-10L + NAS679A3) |
|
| 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 ALL MODELS 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 ALL MODELS 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 ALL MODELS 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... |
|
| NDT1027-.500 |
BOEING REFERENCE STANDARD.. 757 PT 6 51-00-00 FIG 16 ..MATERIAL(6AL-4V) TITANIUM |
|
| 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-.016/.016 |
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-.016/.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-.016/.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-.020/.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-.020/.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-.025/.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-.032/.032 |
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-.032/.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-.036/.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-.040/.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-.040/.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-.040/.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-.040/.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-.040/.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-.045/.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-.050/.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-.050/.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-.050/.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-.050/.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-.063/.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-.063/.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-.063/.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-.071/.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-.080/.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-.080/.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-.080/.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 PT 6 51-00-00. Includes Test Report and Certificate of Conformance. |
|
| NDT1042 |
BOEING REFERENCE STANDARD 737 PT 6 51-00-00. Includes Test Report and Certificate of Conformance. |
|
| NDT1043 |
BOEING REFERENCE STANDARD 737 PT 6 51-00-00. Includes Test Report and Certificate of Conformance. |
|
| NDT1044 |
BOEING REFERENCE STANDARD 737 PT 6 51-00-00. Includes Test Report and Certificate of Conformance. |
|
| NDT1045 |
BOEING REFERENCE STANDARD PT 6 51-10-17 FIG 3. 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-.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 |
|
| NDT1083-0.813 |
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 |
|
| NDT1084 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| 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. |
|
| NDT1084-0.125 |
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 |
|
| NDT1084-0.265 |
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 |
|
| NDT1084-0.562 |
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. |
|
| NDT1084-0.625 |
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. |
|
| NDT1084-0.688 |
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 |
|
| NDT1084-0.750 |
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. |
|
| NDT1084-0.938 |
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 |
|
| NDT1084-1.00 |
BOEING REFERENCE STANDARD ALL PT 6 51-00-02 FIGURE 3, PAGE 7 and 8, 1.0" DIAMETER HOLE |
|
| 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. |
|
| NDT1084-1.124 |
BOEING REFERENCE STANDARD 767 PT 6 51-00-16 PAGE 7 |
|
| 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 767 PT 6 51-00-16 PAGE 7 |
|
| 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. |
|
| NDT1084-1.312 |
BOEING REFERENCE STANDARD 767 PT 6 51-00-16 PAGE 7 |
|
| 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. |
|
| NDT1084-1.437 |
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. |
|
| NDT1084-2.000 |
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 |
|
| 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. |
|
| NDT1086-P1 |
TRANSDUCER POSITIONER USED WITH SUS 1020/AFS-1000A |
|
| NDT1086-P2 |
TRANSDUCER POSITIONER |
|
| 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, 777 PT6 53-30-09 .040/.040 |
|
| 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, 777 PT6 53-30-09 .036/.036 |
|
| 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-.626 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| NDT1089-.750 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| NDT1089-0.656 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| NDT1089-0.660 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| NDT1089-1.375 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| NDT1089-1.438 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| NDT1089-1.500 |
BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 16 |
|
| 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-A |
BOEING REFERENCE STANDARD B737 Part 4, 53-30-07 and 757 PT 4 53-00-02 FIG 2 FASTENER (BACR15GF5D-4, # 49) |
|
| NDT1094-050/010-A |
BOEING REFERENCE STANDARD 737 PT 4 53-30-07 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 |
BOEING REFERENCE STANDARD R&D |
|
| 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 |
|
| 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. |
|
| 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 |
|
| 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 |
|
| 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 |
NEED DRAWING TO QUOTE |
|
| 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 |
NEED DRAWING |
|
| 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 |
|
| 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 |
|
| 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) |
|
| NDT3050 |
BOEING REFERENCE STANDARD PT 6 53-30-20 FIG 2 FASTENER (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) |
|
| 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. 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) |
|
| NDT3075 |
NEED DRAWING |
|
| 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 |
|
| NDT3082B |
BOEING REFERENCE STANDARD 737 PT 6 53-10-70 |
|
| NDT3082C |
BOEING REFERENCE STANDARD 737 PT 6 53-10-70 |
|
| 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 |
|
| 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. |
|
| NDT3125P |
BOEING TRANSDUCER POSITIONER |
|
| 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 |
|
| 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 |
|
| NDT3146 |
BOEING REFERENCE STANDARD 737 PART 4 55-10-16 PAGE 8 FIGURE 4. MATERIAL: 7075-T6 ALUMINUM |
|
| NDT3147 |
BOEING REFERENCE STANDARD 737 PART 4 53-30-10 PAGE 7 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT3149 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-41 FASTENER (BACR15CE5) |
|
| NDT3151 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-46 PAGE 7 FIGURE2 FASTENER (BACR15GF6D6, BACR15F6D4). Includes Test Report and Certificate of Conformance. |
|
| NDT3152-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K4 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K5 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-C |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K6 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-D |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K7 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-E |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K8 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-F |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K9 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-G |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K10 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-H |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K10 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-I |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K10 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-J |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K11 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3152-K |
BOEING REFERENCE STANDARD 737 PT 6 57-10-55. FASTENER: BACB30YP10K12 and BACC30BP10 COLLARS. Includes test report and Certificate of Conformance. |
|
| NDT3153-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW6K4 and BACC30M6 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW6K5 and BACC30M6 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-C |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW6K6 and BACC30M6 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-D |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW8K8 and BACC30M8 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-E |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW8K9 and BACC30M8 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-F |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW8K10 and BACC30M8 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-G |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW10K11 and BACC30M10 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-H |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW10K14 and BACC30M10 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3153-J |
BOEING REFERENCE STANDARD 737 PT 6 57-10-54. FASTENER: BACB30NW12K8 and BACC30M10 COLLARS. Includes Test Report and Certificate of Conformance. |
|
| NDT3156 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP10*10 + BACC30BP10). Includes test report and Certificate of Conformance. |
|
| NDT3157 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP10*10 + BACC30BP10). Includes test report and Certificate of Conformance. |
|
| NDT3159 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP8*7 + BACC30BP8). Includes test report and Certificate of Conformance. |
|
| NDT3161 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP8*7 + BACC30BP8). Includes test report and Certificate of Conformance. |
|
| NDT3162 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP8*8 + BACC30BP8). Includes test report and Certificate of Conformance. |
|
| NDT3163 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP8*8 + BACC30BP8). Includes test report and Certificate of Conformance. |
|
| NDT3164 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-60 FASTENER (BACB30YP8*9 + BACC30BP8). Includes test report and Certificate of Conformance. |
|
| NDT3166-001 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-07. Includes Test Report and Certificate of Conformance. |
|
| NDT3166-002 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-07. Includes Test Report and Certificate of Conformance. |
|
| NDT3166-003 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-07. Includes Test Report and Certificate of Conformance. |
|
| NDT3166-004 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-07. Includes Test Report and Certificate of Conformance. |
|
| NDT3166-005 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-07. Includes Test Report and Certificate of Conformance. |
|
| NDT3166-006 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-09. Includes Test Report and Certificate of Conformance. |
|
| NDT3166-007 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-08. Includes Test Report and Certificate of Conformance. |
|
| NDT3167-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-C |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-D |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-E |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-F |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-G |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-H |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3167-J |
BOEING REFERENCE STANDARD 737 PT 6 57-10-58. Includes test report and Certificate of Conformance. |
|
| NDT3168 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-53 FASTENER (BACB30MY14K9 + BACC30M14). Includes test report and Certificate of Conformance. |
|
| NDT3169 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-48 FASTENER (BACB30YP10 + BACC30BL10). Includes test report and Certificate of Conformance. |
|
| NDT3170 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-06. Includes Test Report and Certificate of Conformance. |
|
| NDT3171 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-06. Includes Test Report and Certificate of Conformance. |
|
| NDT3172 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-05. Includes Test Report and Certificate of Conformance. |
|
| NDT3176-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-59 FASTENER (BACB30YP12*8 + BACC30BP12). Includes Test Report and Certificate of Conformance. |
|
| NDT3176-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-59 FASTENER (BACB30YP12*11 + BACC30BP12. Includes Test Report and Certificate of Conformance. |
|
| NDT3176-C |
BOEING REFERENCE STANDARD 737 PT 6 57-10-59 FASTENER (BACB30YP10*10 + BACC30BP10). Includes Test Report and Certificate of Conformance. |
|
| NDT3176-D |
BOEING REFERENCE STANDARD 737 PT 6 57-10-59 FASTENER (BACB30YP8*9 + BACC30BP8). Includes Test Report and Certificate of Conformance. |
|
| NDT3178-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NM8*7 + BACN11Z7). Test Report and Certificate of Conformance. |
|
| NDT3178-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NM8*7 + BACN11Z7). Test Report and Certificate of Conformance. |
|
| NDT3178-C |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NM9*7 + BACN11Z7). Test Report and Certificate of Conformance. |
|
| NDT3178-D |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NM11*7 + BACN11Z7). Test Report and Certificate of Conformance. |
|
| NDT3178-E |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NP12*7 + BACN11Z7). Test Report and Certificate of Conformance. |
|
| NDT3178-F |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NM 12*7 + BACN11Z7). Test Report and Certificate of Conformance. |
|
| NDT3178-G |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 FASTENER (BACB30NM16*8 + BACN11Z8). Test Report and Certificate of Conformance. |
|
| NDT3178-X |
BOEING REFERENCE STANDARD 737 PT 6 57-10-62 |
|
| NDT3179-A |
BOEING REFERENCE STANDARD 737 PT 6 53-30-39 FASTENER (BACR15GF6D-4) |
|
| NDT3179-B |
BOEING REFERENCE STANDARD 737 PT 6 53-30-39 FASTENER (BACR15GF6D-4) |
|
| NDT3179-C |
BOEING REFERENCE STANDARD 737 PT 6 53-30-39 FASTENER (BACR15GF6D-4) |
|
| NDT3180-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 FASTENER (BACB30NM7K6 + BACN11Z7 + BACW10BP7CD + BACW107DP) |
|
| NDT3180-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM7K6 + BACN11Z7 + BACW10BP7CD + BACW10BP7DP) |
|
| NDT3180-C |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM7K5 + BACN11Z7 + BACW10BP7CD + BACW10BP7DP) |
|
| NDT3180-D |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM7K6 + BACN11Z7 + BACW10BP7CD + BACW10BP7DP) |
|
| NDT3180-E |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM7K7 + BACN11Z7 + BACW10BP7CD + BACW10BP7DP) |
|
| NDT3180-F |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM8K6 + BACN11Z8 + BACW10BP8CD + BACW10BP8DP) |
|
| NDT3180-G |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM7K7 + BACN11Z7 + BACW10BP7CD + BACW10BP7DP) |
|
| NDT3180-H |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM8K7 + BACN11Z8 + BACW10BP8CD + BACW10BP8DP) |
|
| NDT3180-J |
BOEING REFERENCE STANDARD 737 PT 6 57-10-61 (BACB30NM8K9 + BACN11Z8 + BACW10BP8CD + BACW10BP8DP) |
|
| NDT3181-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 2 |
|
| NDT3181-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 2 |
|
| NDT3181G |
GUIDE FOR NDT3181 |
|
| NDT3182-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 3 |
|
| NDT3182-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 3 |
|
| NDT3182G |
GUIDE FOR NDT3182 |
|
| NDT3183 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 4 |
|
| NDT3183G |
GUIDE FOR NDT3183 |
|
| NDT3184 |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 5 |
|
| NDT3184G |
GUIDE FOR NDT3184 |
|
| NDT3185-A |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 6 |
|
| NDT3185-B |
BOEING REFERENCE STANDARD 737 PT 6 57-10-63 FIG 6 |
|
| NDT3185G |
GUIDE FOR NDT3185 |
|
| NDT3186 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-17. Includes Test Report and Certificate of Conformance. |
|
| NDT3187 |
BOEING REFERENCE STANDARD 737 PT 4 57-10-17. Includes Test Report and Certificate of Conformance. |
|
| NDT3189 |
BOEING REFERENCE STANDARD 737 PT 4 55-10-18 |
|
| NDT3190-A |
BOEING REFERENCE STANDARD 737 PT 6 55-10-45 FIG 2 FASTENER (BACB30VT10*8* + BACC30BP10) |
|
| NDT3190-B |
BOEING REFERENCE STANDARD 737 PT 6 55-10-45 FIG 2 FASTENER (BACB30VT8*4* + BACC30BP8) |
|
| NDT3190-C |
BOEING REFERENCE STANDARD 737 PT 6 55-10-45 FIG 2 |
|
| NDT3190-D |
BOEING REFERENCE STANDARD 737 PT 6 55-10-45 FIG 2 |
|
| NDT3191 |
BOEING REFERENCE STANDARD 737 PT 6 55-10-28 FIG 2 FASTENER (BACR15GF6*) |
|
| NDT3192 |
BOEING REFERENCE STANDARD 737, PART 6: 55-10-28 FIGURE 3 PAGE 7 |
|
| NDT3193 |
BOEING REFERENCE STANDARD 737 PT 6 51-30-28 FIG 1. Includes Certification Report and Certificate of Conformance. |
|
| NDT3194-36/36 |
BOEING REFERENCE STANDARD 737 PART 6 53-30-45 PAGE 7 FIGURE 1 TABLE 1. Includes Test Report and Certificate of Conformance. |
|
| NDT3194-40/40 |
BOEING REFERENCE STANDARD 737 PART 6 53-30-45 PAGE 7 FIGURE 1 TABLE 1. Includes Test Report and Certificate of Conformance. |
|
| NDT3194-45/40 |
BOEING REFERENCE STANDARD 737 PART 6 53-30-45 PAGE 7 FIGURE 1 TABLE 1. Includes Test Report and Certificate of Conformance. |
|
| NDT3194-50/40 |
BOEING REFERENCE STANDARD 737 PART 6 53-30-45 PAGE 7 FIGURE 1 TABLE 1. Includes Test Report and Certificate of Conformance. |
|
| NDT3195 |
BOEING REFERENCE STANDARD 737 PT 4 55-10-17 PAGE 18 FIGURE 4. MATERIAL: 7075-T6 or EQUIVALENT AIRCRAFT QUALITY ALUMINUM |
|
| NDT3196 |
BOEING REFERENCE STANDARD 737 PT 4 55-10-17 PAGE 19 FIGURE 5. MATERIAL: 7075-T6 or EQUIVALENT AIRCRAFT QUALITY ALUMINUM |
|
| NDT3197 |
BOEING REFERENCE STANDARD 737 PT 4 55-10-17 PAGE 20 FIGURE 6. MATERIAL: 7075-T6 or EQUIVALENT AIRCRAFT QUALITY ALUMINUM |
|
| NDT3202-A |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3202-B |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3202-C |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3202-D |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3202-E |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3202-F |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3202-G |
BOEING REFERENCE STANDARD 737, PART 6 55-10-56 FIGURE 2 PAGE 9 FASTENER (BACR15GF6*) |
|
| NDT3204 |
BOEING REFERENCE STANDARD 737 PT 4 53-10-08 FIG 2 |
|
| NDT3207 |
BOEING REFERENCE STANDARD 737 PT 6 55-10-50 FIG 2 FASTENER (BACR15FT5D*) |
|
| NDT3207A |
BOEING REFERENCE STANDARD PART 6 55-10-82 PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT3208-C |
BOEING REFERENCE STANDARD 737 PT 6 55-10-55 FASTENER (BACR15FP5*, BACR15GF5*) |
|
| NDT3209A |
BOEING REFERENCE STANDARD PART 6 55-10-74, PAGE 7 FIGURE 2 |
|
| NDT3209B |
BOEING REFERENCE STANDARD |
|
| NDT3210 |
BOEING REFERENCE STANDARD 737, PART 6: 57-10-81, PAGE 8 FIGURE 2 |
|
| NDT3211 |
BOEING REFERENCE STANDARD B737 NDTM P6, 57-10-81, PAGE 9 FIGURE 3 |
|
| NDT3212 |
BOEING REFERENCE STANDARD B737 NDTM P6, 57-10-81 PAGE 10 FIGURE 4 |
|
| NDT3214 |
BOEING REFERENCE STANDARD PT 4 53-10-09 FIGURE 2 PAGE 6 |
|
| NDT3217-A |
BOEING REFERENCE STANDARD 737, PART 6: 57-10-79 |
|
| NDT3217-B |
BOEING REFERENCE STANDARD 737, PART 6: 57-10-79 |
|
| NDT3218 |
BOEING REFERENCE STANDARD 737, PART 6 55-10-53 FIGURE 3 PAGE 10 |
|
| NDT3219 |
BOEING REFERENCE STANDARD 737 PART 4 57-10-19 PAGE 11 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT3220 |
BOEING REFERENCE STANDARD 737 PART 4 57-50-04 |
|
| NDT3220-P |
POSITIONER FOR NDT3220 |
|
| NDT3221 |
BOEING REFERENCE PART 4 55-10-19 FIGURE 2 PAGE 6 |
|
| NDT3223 |
BOEING 737 REFERENCE STANDARD PART 6, 53-11-34 PAGE 7 FIGURE 2. FASTENER = BACR15GF6D4 |
|
| NDT3224 |
BOEING REFERENCE STANDARD 737PT 4 54-40-01 |
|
| NDT3225 |
BOEING REFERENCE STANDARD PART 6 54-40-20 PAGE 6 FIGURE 2. |
|
| NDT3226 |
CBOEING REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. BACR15FT6D RIVETS BUCKED BETWEEN .250"Ø and .280"Ø. |
|
| NDT3226A |
BOEING REFERENCE STANDARD |
|
| NDT3227 |
BOEING REFERENCE STANDARD PART 4 54-40-09 PAGE 6 FIGURE 2. MATERIAL 15-5 PH STAINLESS STEEL. |
|
| NDT3228-A |
BOEING REFERENCE STANDARD |
|
| NDT3228-B |
BOEING REFERENCE STANDARD |
|
| NDT3228-C |
BOEING REFERENCE STANDARD |
|
| NDT3229 |
BOEING REFERENCE STANDARD 737 PT6 53-30-50 FIGURE 2 PAGE 21. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. |
|
| NDT322A |
BOEING REFERENCE STANDARD 737 PART 6 53-10-25 FIGURE 1 PAGE 4 |
|
| NDT3230 |
BOEING REFERENCE STANDARD 737 pt 4 53-30-11 page 8 figure 2. Includes test report and Certificate of Conformance. |
|
| NDT3231 |
BOEING REFERENCE STANDARD 737 PT 4 53-10-10 FIGURE 2 PAGE 10 |
|
| NDT3232-A |
BOEING REFERENCE STANDARD |
|
| NDT3232-B |
BOEING REFERENCE STANDARD |
|
| NDT3232-C |
BOEING REFERENCE STANDARD |
|
| NDT3233 |
BOEING REFERENCE STANDARD 737 pt 4 53-30-11 page 8 figure 2. Includes test report and Certificate of Conformance. |
|
| NDT3234 |
BOEING REFERENCE STANDARD |
|
| NDT3235 |
BOEING REFERENCE STANDARD 737 PT 4 54-40-05 |
|
| NDT3236 |
BOEING REFERENCE STANDARD 737 pt 6 57-10-85 FASTENER (BACR15FT8D3C, BACR15FTT8D4C) |
|
| NDT3237-0.040/0.010 |
BOEING REFERENCE STANDARD 737 PT 4 53-30-12 FASTENER (BACR15GF5*). Includes Test Report and Certificate of Conformance. |
|
| NDT3237-0.050/0.015 |
BOEING REFERENCE STANDARD 737 PT 4 53-30-12 FASTENER (BACR15GF5*). Includes Test Report and Certificate of Conformance. |
|
| NDT3237-0.130/0.020 |
BOEING REFERENCE STANDARD 737 PT 4 53-30-12 FASTENER (BACR15GF5*). Includes Test Report and Certificate of Conformance. |
|
| NDT3237-P1 |
BOEING PROBE POSITIONER 737 PT 4 53-30-12 |
|
| NDT3238 |
BOEING REFERENCE STANDARD PART 4, 55-10-23 PAGE 6 FIGURE 2 |
|
| NDT3239 |
BOEING REFERENCE STANDARD |
|
| NDT3239 .025 |
BOEING REFERENCE STANDARD |
|
| NDT3239G |
BOEING CALIBRATION GUIDE |
|
| NDT3240 |
BOEING REFERENCE STANDARD |
|
| NDT3241 |
BOEING REFERENCE STANDARD |
|
| NDT3242 |
BOEING REFERENCE STANDARD 737 PT 4 54-40-03 |
|
| NDT3243 |
BOEING REFRENCE STANDARD 737 PT 4 54-40-04 |
|
| NDT3244 |
BOEING REFERENCE STANDARD |
|
| NDT3245-A |
BOEING REFERENCE STANDARD |
|
| NDT3245-B |
BOEING REFERENCE STANDARD |
|
| NDT3246-A |
BOEING REFERENCE STANDARD |
|
| NDT3246-B |
BOEING REFERENCE STANDARD |
|
| NDT3246-C |
BOEING REFERENCE STANDARD |
|
| NDT3247-A |
BOEING REFERENCE STANDARD |
|
| NDT3247-B |
BOEING REFERENCE STANDARD |
|
| NDT3247-C |
BOEING REFERENCE STANDARD |
|
| NDT3248 |
BOEING REFERENCE STANDARD 737 PART 6 55-10-66 PAGE 5 FIGURE 2 |
|
| NDT3249 |
BOEING REFERENCE STANDARD 737 PT 6 55-10-64 Page 12 Figure 2. Includes Test Report and Certificate of Conformance. |
|
| NDT3250 |
BOEING REFERENCE STANDARD 737 PT 6 55-10-64 PAGE 13. Includes Test Report and Certificate of Conformance. |
|
| NDT3251 |
BOEING REFERENCE STANDARD PART 6 52-30-02 PAGE 5 FIGURE 2 |
|
| NDT3251-Rev2 |
BOEING REFERENCE STANDARD |
|
| NDT3252 |
BOEING REFERENCE STANDARD 737 PT 4 52-10-03 |
|
| NDT3253 |
BOEING REFERENCE STANDARD 737 PT 4 54-40-06 |
|
| NDT3254 |
BOEING REFERENCE STANDARD 737 pt 4 54-40-06 |
|
| NDT3255 |
BOEING REFERENCE STANDARD |
|
| NDT3257 |
BOEING REFERENCE STANDARD |
|
| NDT3258A |
BOEING REFERENCE STANDARD |
|
| NDT3258B |
BOEING REFERENCE STANDARD 737 PT 4 54-40-08 |
|
| NDT3259 |
BOEING REFERENCE STANDARD 737 PT 6 54-40-17 |
|
| NDT3260 |
BOEING REFERENCE STANDARD 737 PT 6 54-40-17 |
|
| NDT3261 |
BOEING REFERENCE STANDARD 737 PT 6 57-50-31 |
|
| NDT3262 |
BOEING REFERENCE STANDARD 737 PT 4 54-40-07 |
|
| NDT3263 |
BOEING REFERENCE STANDARD 737 PT 6 57-50-31 |
|
| NDT3264 |
BOEING REFERENCE STANDARD 737 PT 4 55-10-22 |
|
| NDT3265 |
BOEING REFERENCE STANDARD 737 PART 6 55-10-70 PAGE 8 FIGURE 2 |
|
| NDT3266 |
BOEING REFERENCE STANDARD |
|
| NDT3267-.040/.040 |
Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .040/.040. Includes C-SCAN, Test Report and Certificate of Conformance. |
|
| NDT3267-.050/.040 |
Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .050/.040. Includes C-SCAN, Test Report and Certificate of Conformance. |
|
| NDT3267-.063/.056 |
Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .063/.056. Includes C-SCAN, Test Report and Certificate of Conformance. |
|
| NDT3267-.063/.063 |
Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .063/.063. Includes C-SCAN, Test Report and Certificate of Conformance. |
|
| NDT3267-.080/.063 |
Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .080/.063. Includes C-SCAN, Test Report and Certificate of Conformance. |
|
| NDT3267-.080/.100 |
Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .080/.100. Includes C-SCAN, Test Report and Certificate of Conformance. |
|
| NDT3268 |
BOEING REFERENCE STANDARD 737 PT 4 53-10-11 |
|
| NDT3269 |
BOEING REFERENCE STANDARD, PT6, 54-40-19 PAGE 12 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT3270 |
BOEING REFERENCE STANDARD |
|
| NDT3270-REV2 |
BOEING REFERENCE STANDARD |
|
| NDT3271 |
BOEING REFERENCE STANDARD MATERIAL: 6AL-4v TITANIUM. |
|
| NDT3272 |
BOEING REFERENCE STANDARD |
|
| NDT3273 |
BOEING REFERNECE STANDARD |
|
| NDT3273A |
BOEING REFERENCE STANDARD |
|
| NDT3274 |
BOEING REFERENCE STANDARD 2024-T351 ALUMINUM |
|
| NDT3275 |
BOEING REFERENCE STANDARD 2024-T351 ALUMINUM |
|
| NDT3276 |
BOEING REFERENCE STANDARD 737 PART 4 53-20-02 FIGURE 2 PAGE 9. MATERIAL: 2024-T3 ALUMINUM WITH RUBBER FEET ON BOTTOM FOR SUPPORT. Includes Test Report and Certificate of Conformance. |
|
| NDT3276A |
BOEING REFERENCE STANDARD 737 PART 4 53-20-02 FIGURE 3 PAGE 10. MATERIAL: 2024-T3 ALUMINUM WITH RUBBER FEET ON BOTTOM FOR SUPPORT. Includes Test Report and Certificate of Conformance. . |
|
| NDT3277 |
BOEING REFERENCE STANDARD R&D. 2024-T351 ALUMINUM |
|
| NDT3278-A |
BOEING REFERENCE STANDARD 737 PART 6 53-30-50 FIGURE 3 PAGE 30. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT3278-B |
BOEING REFERENCE STANDARD 737 PART 6 53-30-50 FIGURE 3 PAGE 30. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT3278-C |
BOEING REFERENCE STANDARD 737 PART 6 53-30-50 FIGURE 3 PAGE 30. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT3279 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 2024-T3 ALUMINUM. |
|
| NDT3280 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 2024-T3 ALUMINUM. BACR15FT6D RIVETS. |
|
| NDT3281 |
BOEING REFERENCE STANDARD WITH 13 EDM FLAWS LOCATED THROUGH OUT THE STANDARD. MATERIAL: 7075-T6 ALUMINUM |
|
| NDT391 |
BOEING REFERENCE STANDARD PART 6 53-10-51 FIGURE 2 PAGE 7. |
|
| NDT392 |
BOEING REFERENCE STANDARD 737 53-30-03 PART 4 PAGE 7 FIGURE 2 |
|
| NDT394 |
BOEING REFERENCE STANDARD 737 PT 6 54-30-01. Includes Test Report and Certificate of Conformance. |
|
| NDT394P |
BOEING POSITIONER 737 PT 6 54-30-01. Includes Test Report and Certificate of Conformance. |
|
| NDT396 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-09 FIG 2.( Note: Material thickness for this standard is .036"/.036"). Includes Test Report and Certificate of Conformance. |
|
| NDT396-32/40 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. |
|
| NDT396-36/36 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. |
|
| NDT396-40/40 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. |
|
| NDT396-45/40 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. |
|
| NDT396-50/40 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. |
|
| NDT396-56/40 |
BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. |
|
| NDT398 |
BOEING REFERENCE STANDARD 737 PT 4 53-10-01. Includes Test Report and Certificate of Conformance. |
|
| NDT4064 |
BOEING REFERENCE STANDARD 747 PT 6 53-30-06 FIG 1 FASTENER (BACR15CE6D5, BACR15DS7D5) |
|
| NDT4116 |
BOEING REFERENCE STANDARD 747 PT 4 54-40-02 |
|
| NDT4152 |
BOEING 747 REFERENCE STANDARD PART 4 53-10-07 PAGE 6 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT4153 |
BOEING 747 REFERENCE STANDARD PART 4 57-30-08 PAGE 6 FIGURE 2. PROCEDURE FOR INSPECTING CRACKED RIVET PART NUMBER BACR15FH10DD17 |
|
| NDT4178 |
BOEING REFERENCE STANDARD 747 PT 4 53-40-05 |
|
| NDT4183 |
BOEING 747 REFERENCE STANDARD PART 4 53-30-03 FIGURE 2 PAGE 21. Includes Test Report and Certificate of Conformance. |
|
| NDT4208 |
BOEING REFERENCE STANDARD 747 PART 4 54-40-23 FIGURE 2 PAGE 8. Includes Certification Report and Certificate of Conformance. |
|
| NDT4209 |
BOEING REFERENCE STANDARD 747 PT 4 53-10-08 PAGE 12. Includes Test Report and Certificate of Conformance. |
|
| NDT4211 |
BOEING REFERENCE STANDARD 747 PT 4 53-10-08 PAGE 12. Includes Test Report and Certificate of Conformance. |
|
| NDT4226 |
BOEING REFERENCE STANDARD 747 pt 4 57-10-22 |
|
| NDT4228 |
BOEING 747 REFERENCE STANDARD PART 6 54-40-16 PAGE 11 FIGURE 2. MATERIAL: 15-5PH, 17-4 PH or 4130 STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT4232 |
Boeing Reference Standard 747 55-10-03 PART 4 Figure 2, Page 6. Material: 2024-T3 or 7075-T6 Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). |
|
| NDT4233 |
Boeing Reference Standard 747 55-10-03 PART 4 Figure 3, Page 7. Material: 2024-T3 or 7075-T6 Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). |
|
| NDT4234 |
Boeing Reference Standard 747 55-10-03 PART 4 Figure 4, Page 8. Material: 2024-T3 or 7075-T6 Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). |
|
| NDT4235 |
Boeing Reference Standard 747 55-10-03 PART 4 Figure 5, Page 9. Material: 2024-T3 or 7075-T6 Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). |
|
| NDT4240 |
BOEING 747 REFERENCE STANDARD PART 4, 27-20-01 PAGE 8 FIGURE 3 |
|
| NDT4243 |
BOEING REFERENCE STANDARD 747 PT 6 57-10-31 PAGE 4, FIGURE 1 |
|
| NDT4244 |
BOEING REFERENCE STANDARD 747 PT 4 53-10-12 |
|
| NDT4247 |
BOEING REFERENCE STANDARD 747 PART 4 27-60-01, PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT4250 |
BOEING REFERENCE STANDARD 747 PT 4 57-30-10 Page 6 Figure 2. Includes Test Report and Certificate of Conformance. |
|
| NDT4251 |
BOEING REFERENCE STANDARD 747 PT 4 57-30-11 |
|
| NDT4252 |
BOEING REFERENCE STANDARD 747 PT 4 57-10-23 |
|
| NDT4254 |
BOEING REFERENCE STANDARD 747 PT 4 57-10-24 |
|
| NDT4255 |
BOEING REFERENCE STANDARD |
|
| NDT4256 |
BOEING REFERENCE STANDARD |
|
| NDT4257 |
BOEING REFERENCE STANDARD |
|
| NDT4258 |
BOEING REFERENCE STANDARD |
|
| NDT4259 |
BOEING REFERENCE STANDARD |
|
| NDT4260 |
BOEING REFERENCE STANDARD |
|
| NDT4263 |
BOEING REFERENCE STANDARD 747 PT 4 57-10-25 PAGE 20 FIGURE 3. Includes Test Report and Certificate of Conformance. |
|
| NDT4264 |
BOEING REFERENCE STANDARD 747 PT 4 57-10-25 PAGE 21 FIGURE 4. Includes Test Report and Certificate of Conformance. |
|
| NDT504A |
BOEING REFERENCE STANDARD 757 PART 6 54-40-01, PG. 12 FIGURE 3 and PART 6 54-40-02, PG. 11 FIGURE 3 |
|
| NDT504B |
BOEING REFERENCE STANDARD 757 PART 6 54-40-01, PG. 12 FIGURE 3 and PART 6 54-40-02, PG. 11 FIGURE 3 |
|
| NDT504C |
BOEING REFERENCE STANDARD 757 PART 6 54-40-01, PG. 12 FIGURE 3 and PART 6 54-40-02, PG. 11 FIGURE 3 |
|
| NDT504D |
BOEING REFERENCE STANDARD 757 PART 6 54-40-01, PG. 12 FIGURE 3 and PART 6 54-40-02, PG. 11 FIGURE 3 |
|
| NDT504E |
BOEING REFERENCE STANDARD 757 PART 6 54-40-01, PG. 12 FIGURE 3 and PART 6 54-40-02, PG. 11 FIGURE 3 |
|
| NDT511 |
BOEING REFERENCE STANDARD 757 PT 6 57-10-02 FASTENER (BACB30VU10K12 + BACC30M10) |
|
| NDT512 |
BOEING REFERENCE STANDARD 757, PT 4 5710-01. Includes Test Report and Certificate of Conformance. |
|
| NDT514 |
BOEING REFERENCE STANDARD 757 PT 6 57-20-01. BOEING REFERENCE STANDARD 757 PT 6 57-20-01 FASTENER. Includes Test Report and Certificate of Conformance. FASTENER (BACB30VU12K14 + BACC30M12, BACBVU10K13 + BACC30M10) |
|
| NDT515 |
BOEING REFERENCE STANDARD 757 PT 4 57-21-01 FIG 3 PG 6. Includes Test Report and Certificate of Conformance. |
|
| NDT516 |
BOEING REFERENCE STANDARD 757 PT 6 57-23-01 FASTENER. Includes Test Report and Certificate of Conformance.(BACB30NW10*8) |
|
| NDT518 |
BOEING REFERENCE STANDARD 757 PT 4 57-21-02 FIG 2 PG 6. Includes Test Report and Certificate of Conformance... |
|
| NDT519 |
BOEING REFERENCE STANDARD 757 PT 6 52-30-01 FASTENER (BACB30NW6K3, BACB30NW6K5 + BACC30M6) |
|
| NDT521 |
BOEING REFERENCE STANDARD 757 PT.4, 55-10-02 PG.8 |
|
| NDT522 |
BOEING REFERENCE STANDARD 757 PT 4 53-80-01 FIGURE 4 PAGE 8. Includes Test Report and Certificate of Conformance. |
|
| NDT524 |
BOEING REFERENCE STANDARD 757 PART 6 53-10-06 PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT525 |
Boeing Reference Standard, 757 PT4 ..57-50-01 pg. 7&8 fig 3( sheet1 and sheet 2) |
|
| NDT527 |
BOEING REFERENCE STANDARD 757 PT 6 53-30-06 FASTENER (BACR15FV6KE5C) |
|
| NDT528 |
BOEING REFERENCE STANDARD 757 PT 4 55-10-04 |
|
| NDT531 |
BOEING REFERENCE STANDARD 757 PT 6 53-60-01 |
|
| NDT536 |
Boeing Positioner, 757 PT4 53-40-01..pg. 5 fig 2 |
|
| NDT537 |
BOEING REFERENCE STANDARD 757 PT 4 57-10-02 FIG 3 PG 8. Includes Test Report and Certificate of Conformance. |
|
| NDT542 |
BOEING REFERENCE STANDARD 757 PT 4 55-10-07 |
|
| NDT546 |
BOEING REFERENCE STANDARD 757 PT 4 57-20-02 FIGURE 2 PG. 7. Includes Test Report and Certificate of Conformance. |
|
| NDT549 |
BOEING REFERENCE STANDARD 757 PT 6 57-20-02 PAGE 6 FIGURE 2. |
|
| NDT552 |
BOEING REFERENCE STANDARD 757 PT 4 57-20-01. Includes Test Report and Certificate of Conformance. |
|
| NDT553 |
Boeing Reference Standard, 757 PT6 ..52-30-02 pg. 6 fig 2 |
|
| NDT558 |
BOEING REFERENCE STANDARD 757 PT 6 53-30-12 FASTENER (BACR15BB5AD-5, BACR15BB6AD-5). Includes Certification Report and Certificate of Conformance. |
|
| NDT562 |
BOEING REFERENCE STANDARD 757 PT 4 57-25-01 FIG 2 PG 11 |
|
| NDT564A |
BOEING REFERENCE STANDARD 757 PT 4 57-50-01 |
|
| NDT564B |
BOEING REFERENCE STANDARD 757 PT 4 57-50-01 |
|
| NDT567 |
BOEING REFERENCE STANDARD 757 PT4 54-50-02 FIGURE 3 PAGE 8. Includes Test Report and Certificate of Conformance. |
|
| NDT568 |
Boeing Reference Standard, 757 PT4 .. |
|
| NDT575 |
BOEING REFERENCE STANDARD 757 PT 6 53-60-12 FASTENER (BACB330MY6-3 + BACC30M6) |
|
| NDT578 |
BOEING REFERENCE STANDARD 757 PT 6 55-10-04 FASTENER (BACB30NX16 + BACC30X16) |
|
| NDT579 |
BOEING REFERENCE STANDARD 757 PT 6 54-40-05 |
|
| NDT595 |
BOEING REFERENCE STANDARD 757 PT 4 57-25-01 FIG 2 |
|
| NDT596 |
BOEING REFERENCE STANDARD 757 PT 4 52-30-01. Includes Test Report and Certificate of Conformance. |
|
| NDT6000-EC |
BOEING REFERENCE STANDARD 57-50-02 PT 4 FIG 3. Includes Test Report and Certificate of Conformance. |
|
| NDT6000A |
BOEING REFERENCE STANDARD 767 PT 4 57-50-02 FASTENER (BACB30MY10K5 + BACC30M1, BACB30MY10K6 + BACC30AG10) |
|
| NDT6000B |
BOEING REFERENCE STANDARD 767 PT 4 57-50-02 FASTENER (BACB30MY10K6 + BACC30M10) |
|
| NDT6000C |
BOEING REFERENCE STANDARD 767 PT 4 57-50-02 FASTENER (BACB30MY10K6 + BACC30M10) |
|
| NDT6000D |
BOEING REFERENCE STANDARD 767 PT 4 57-50-02 FASTENER (BACB30MY10K5 + BACC30M10, BACB30MY10K5 + BACC30AG10) |
|
| NDT6000E |
BOEING REFERENCE STANDARD 767 PT 4 57-50-02 FASTENER (BACB30MY10K9 + BACC30M10) |
|
| NDT6001 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-23 |
|
| NDT6002 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-24 |
|
| NDT6004 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-09 PAGE 11 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT6005 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-09 PAGE 12 FIGURE 3. Includes Test Report and Certificate of Conformance. |
|
| NDT6006 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-09 PAGE 13 FIGURE 4. Includes Test Report and Certificate of Conformance. |
|
| NDT6007 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-11 |
|
| NDT6008 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-11 |
|
| NDT6009 |
BOEING REFERENCE STANDARD 767 PT 4 52-30-03 |
|
| NDT6010 |
BOEING REFERENCE STANDARD 767 PT 4 52-30-02 |
|
| NDT6011 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-20 PAGE 6 FIGURE 2. MATERIAL: 6AL-4V TITANIUM |
|
| NDT6011G |
BOEING GUIDE 767 PT 4 57-50-20 PAGE 7 |
|
| NDT6013 |
BOEING REFERENCE STANDARD 767 PT 4 53-10-03 |
|
| NDT6014 |
BOEING REFERENCE STANDARD 767 PT4 57-50-16 |
|
| NDT6015 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-16 |
|
| NDT6016 |
BOEING REFERENCE STANDARD 767 PT 4 53-10-03 |
|
| NDT6017 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-22 PAGE 7&8 FIGURE 3 SHEET 1 of 2. MATERIAL: 6AL-4V TITANIUM |
|
| NDT6018 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-22 PAGE 9&10 FIGURE 3 SHEET 1 of 2. MATERIAL: 6AL-4V TITANIUM |
|
| NDT6019 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-20 PAGE 6 FIGURE 2. MATERIAL: 7075-T6 FOR LAYERS 1,2 and3. 2024-t3 FOR LAYER 4 |
|
| NDT6020 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-14 PAGE 11 FIGURE 4. Includes Certificate of Conformance. |
|
| NDT6021 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-14 PAGE 112 FIGURE 5. Includes Certificate of Conformance. |
|
| NDT6022 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-15 PAGE 5 FIGURE 2 |
|
| NDT6023 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-21 PAGE 5 FIGURE 2 MATERIAL: AIRCRAFT QUALITY ALUMINUM |
|
| NDT6023P |
BOEING TRANSDUCER POSITIONER 767 PT 4 57-50-21 PAGE 6 FIGURE 3 MATERIAL: PLEXIGLASS |
|
| NDT6024 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-10 PAGE 5 FIGURE 2. MATERIAL: 4330M STEEL. USE BACB30MY10K2 FASTENERS |
|
| NDT6025-1 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6025-2 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6025-3 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6025-4 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6025-5 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6025-6 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6027 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 9 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT6027P |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-10 PAGE 13 FIGURE 6. Includes Certificate of Conformance. |
|
| NDT6028 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 10 FIGURE 3. Includes Test Report and Certificate of Conformance. |
|
| NDT6029 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 11 FIGURE 4. Includes Test Report and Certificate of Conformance. |
|
| NDT6029P |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-10 PAGE 14 FIGURE 7. Includes Certificate of Conformance. |
|
| NDT6030 |
BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 12 FIGURE 5. Includes Test Report and Certificate of Conformance. |
|
| NDT6030P |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-10 PAGE 15 FIGURE 8. Includes Certificate of Conformance. |
|
| NDT6031-1 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-18 PAGE 5 FIGURE 2 |
|
| NDT6031-2 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-18 PAGE 5 FIGURE 2 |
|
| NDT6031-3 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-18 PAGE 5 FIGURE 2 |
|
| NDT6031-4 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-18 PAGE 5 FIGURE 2 |
|
| NDT6032-1 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-19 PAGE 5 FIGURE 2 |
|
| NDT6032-2 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-19 PAGE 5 FIGURE 2 |
|
| NDT6032-3 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-19 PAGE 5 FIGURE 2 |
|
| NDT6032-4 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-19 PAGE 5 FIGURE 2 |
|
| NDT6033-1 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-12 page 5 figure 2 |
|
| NDT6033-2 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-12 page 5 figure 2 |
|
| NDT6034 |
BOEING REFERENCE STANDARD PT 4 57-50-13 |
|
| NDT6035-1 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-13 page 8 figure 3 |
|
| NDT6035-2 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-13 page 8 figure 3 |
|
| NDT6036 |
BOEING REFERENCE STANDARD 767 PT 4 57-20-04 FIG 2. Includes Test Report and Certificate of Conformance. |
|
| NDT6036P1 |
TRANSDUCER POSITIONER FOR TEK-5086, 767 PT 4 57-20-04 FIG 2. Includes Certificate of Conformance. |
|
| NDT6036P2 |
TRANSDUCER POSITIONER FOR TEK-5086, 767 PT 4 57-20-04 FIG 2. Includes Certificate of Conformance. |
|
| NDT6038 |
BOEING REFERENCE STANDARD PT 4 57-50-25 |
|
| NDT6041 |
BOEING REFERENCE STANDARD 767 PT 4 57-20-03 |
|
| NDT6045 |
BOEING R&D REFERENCE STANDARD. MATERIAL: 7075-T6 or 7075-T7 ALUMINUM. |
|
| NDT6046 |
BOEING REFERENCE STANDARD 767 PART 4 53-30-02 PAGE 8 |
|
| NDT6047 |
BOEING REFERENCE STANDARD 767 PT 4 53-30-02 PAGE 9 FIG 1. Includes Test Report and Certificate of Conformance. |
|
| NDT6048 |
BOEING REFERENCE STANDARD 767 Part 4 27-40-02 horizontal stab inspection. Includes Test Report and Certificate of Conformance. |
|
| NDT6049 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-09 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. |
|
| NDT6050 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-09 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. |
|
| NDT6051 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-09 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. |
|
| NDT6052 |
BOEING REFERENCE STANDARD 767 P4, 57-50-27. UT INSPECTION OF MAIN LANDING GEAR FORWARD TRUNNION SUPPORT SIDE LOAD FITTING |
|
| NDT6052G |
BOEING 767 6052 REFERENCE STANDARD GUIDE. DELRIN |
|
| NDT6053 |
BOEING REFERENCE STANDARD 767 P4 57-50-28. MATERIAL: TITANIUM (6AL-4V). UT INSPECT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT SIDE LOAD STRAP. |
|
| NDT6054 |
BOEING REFERENCE STANDARD |
|
| NDT6055 |
BOEING REFERENCE STANDARD |
|
| NDT6056 |
BOEING REFERENCE STANDARD |
|
| NDT6057 |
BOEING CUSTOM MULTI-PLATE REFERENCE STANDARD STACK, 54-50-112b |
|
| NDT6058 |
BOEING 767 REFERENCE STANDARD PART 4 53-50-01 FIGURE 2 PAGE 10. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT6059 |
BOEING 767 REFERENCE STANDARD. PART 4 57-50-05 PAGE 8 FIGURE 3. MATERIAL: 15-5PH NORMALIZED. Includes Test Report and Certificate of Conformance. |
|
| NDT6060 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT6061 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT6062 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT6064 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT6065 |
BOEING R&D REFERENCE STANDARD. MATERIAL: 2024-T3 OR 7075 SERIES ALUMINUM. |
|
| NDT6066 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 11. LUG B 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6067 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 9. LUG A 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6068 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 15. LUG D 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6069 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 13. LUG C..4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT607 |
BOEING REFERENCE STANDARD 767 PT 6 53-80-02 |
|
| NDT6070 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 17. LUG E 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6071 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 19. LUG F 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6072 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 21. LUG H 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6073 |
BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 23. LUG G 4340M STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6074 |
BOEING REFERENCE STANDARD 767 PART 4 54-50-10 FIGURE 2 PAGE 7. MATERIAL: 15-5PH STEEL. Includes Test Report and Certificate of Conformance. |
|
| NDT6075 |
BOEING REFERENCE STANDARD 767 PART 6 53-10-22 FIGURE 2 PAGE 5. MATERIAL: 2024-T3 ALUMINUM. FASTENERS: BACR15FVKE & BACR15FV7KE. Includes Test Report and Certificate of Conformance. |
|
| NDT6076 |
BOEING REFERENCE STANDARD 767 ..P6 57-20-10 MATERIAL: 7075-T6 OR 2024-T3 ALUMINUM. EXTERNAL LFEC INSPECTION ON STRINGERS6,10,15 AT THE LOWER WING SKIN AT RIBS3, 5, 18 AND 31. Includes Test Report and Certificate of Conformance. |
|
| NDT6077 |
BOEING REFERENCE STANDARD 767 ..P6 57-20-10 MATERIAL: 7075-T6 OR 2024-T3 ALUMINUM. EXTERNAL LFEC INSPECTION ON STRINGERS6,10,15 AT THE LOWER WING SKIN AT RIBS3, 5, 18 AND 31. Includes Test Report and Certificate of Conformance. |
|
| NDT6078 |
BOEING REFERENCE STANDARD 767 ..P6 57-20-10 MATERIAL: 7075-T6 OR 2024-T3 ALUMINUM. EXTERNAL LFEC INSPECTION ON STRINGERS6,10,15 AT THE LOWER WING SKIN AT RIBS3, 5, 18 AND 31. Includes Test Report and Certificate of Conformance. |
|
| NDT6079 |
BOEING REFERENCE STANDARD 767 ..P6 57-20-10 MATERIAL: 7075-T6 OR 2024-T3 ALUMINUM. EXTERNAL LFEC INSPECTION ON STRINGERS6,10,15 AT THE LOWER WING SKIN AT RIBS3, 5, 18 AND 31. Includes Test Report and Certificate of Conformance. |
|
| NDT607A |
BOEING REFERENCE STANDARD 767 PT 6 53-80-02 |
|
| NDT6080 |
BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT6081 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 15-5PH STEEL. |
|
| NDT6082 |
BOEING 767 PART 4 54-50-13 REFERENCE STANDARD WITH GRAIN DIRECTION. 7075-T6 OR 2024-T3 ALUMINUM |
|
| NDT6083 |
BOEING 767 PART 4 54-50-13 REFERENCE STANDARD WITH GRAIN DIRECTION. 7075-T6 OR 2024-T3 ALUMINUM |
|
| NDT6084 |
BOEING 767 PART 4 54-50-13 REFERENCE STANDARD WITH GRAIN DIRECTION. 7075-T6 OR 2024-T3 ALUMINUM |
|
| NDT6085 |
BOEING 767 PART 4 54-50-13 REFERENCE STANDARD WITH GRAIN DIRECTION. 7075-T6 OR 2024-T3 ALUMINUM |
|
| NDT6086 |
BOEING 767 PART 4 54-50-13 REFERENCE STANDARD WITH GRAIN DIRECTION. 7075-T6 OR 2024-T3 ALUMINUM |
|
| NDT6087 |
BOEING 767 PART 4 54-50-13 REFERENCE STANDARD WITH GRAIN DIRECTION. 7075-T6 OR 2024-T3 ALUMINUM |
|
| NDT6088 |
BOEING REFERENCE STANDARD R&D...MATERIAL: 15-5PH CRES |
|
| NDT6089 |
BOEING 767 REFERENCE STANDARD R&D BAY 1 STRUT CHORD. |
|
| NDT6090 |
BOEING 767 REFERENCE STANDARD R&D BAY 3 STRUT CHORD. |
|
| NDT6091 |
BOEING 767 R&D REFERENCE STANDARD. MATERIAL: 15-5PH STAINLESS STEEL |
|
| NDT6092 |
BOEING 767 R&D REFERENCE STANDARD. MATERIAL: 15-5PH STAINLESS STEEL |
|
| NDT6093 |
BOEING 767 REFERENCE STANDARD R&D. MATERIAL:15-5PH |
|
| NDT6094 |
BOEING 767 R&D REFERENCE STANDARD. MATERIAL: 15-5PH STAINLESS STEEL |
|
| NDT6096 |
BOEING REFERENCE STANDARD 767 PART 4 53-60-02 FIGURE 2 PAGE 6. MATERIAL: 2024-T3 ALUMINUM WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT6097 |
BOEING REFERENCE STANDARD R&D FIGURE 2 . MATERIAL: 2024-T351 ALUMINUM. |
|
| NDT6098 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 2024-T3 ALUMINUM. |
|
| NDT6099 |
BOEING REFERENCE STANDARD PER MARKUP 767 PT 4 57-20-01 PAGE 4 FIGURE 2 |
|
| NDT6100 |
BOEING R&D REFERENCE STANDARD. MATERIAL: 2024-T351 ALUMINUM. |
|
| NDT6101 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 4340M. |
|
| NDT6102 |
BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM. Includes Test Report Traceable to NIST. |
|
| NDT6103 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 2024-T3. |
|
| NDT6104 |
BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM. Includes Test Report Traceable to NIST. |
|
| NDT611 |
BOEING REFERENCE STANDARD 767 PT 6 54-51-01 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. |
|
| NDT612 |
BOEING REFERENCE STANDARD 767 PT 6 54-51-01 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. |
|
| NDT613 |
BOEING REFERENCE STANDARD 767 PT 6 54-51-01 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. |
|
| NDT614 |
BOEING REFERENCE STANDARD 767 PT 4 57-20-01 PAGE 4 FIGURE 2 |
|
| NDT615 |
BOEING REFERENCE STANDARD 767 PT 4 53-80-01 FIG 2. Includes Test Report and Certificate of Conformance. |
|
| NDT616 |
BOEING REFERENCE STANDARD 767 PT 4 27-40-01 |
|
| NDT616P |
BOEING 767 CONVEX TRANSDUCER POSITIONER PART 4 27-40-01 FIGURE 3 PAGE 5 |
|
| NDT617 |
BOEING REFERENCE STANDARD 767 PT 6 53-80-03 |
|
| NDT618 |
BOEING REFERENCE STANDARD 767 PT 6 53-80-03 |
|
| NDT618A |
BOEING REFERENCE STANDARD 767 PT 6 53-80-03 |
|
| NDT619 |
BOEING REFERENCE STANDARD 767 PT4 55-10-04 |
|
| NDT619P |
BOEING TRANSDUCER POSITIONER 767 PT4 55-10-04 |
|
| NDT620 |
BOEING REFERENCE STANDARD 767 PT 4 53-60-01 |
|
| NDT621 |
BOEING REFERENCE STANDARD 767 PT 4 57-10-01 page 4 fig.1 |
|
| NDT622 |
BOEING REFERENCE STANDARD 767 PT 6 57-20-01 FASTENER (BACB30TY10K12 + BACC30BE10). Includes Test Report and Certificate of Confromance. |
|
| NDT623 |
BOEING REFERENCE STANDARD 767 PT 4 57-10-03 FASTENER (BACB30NW12K, BACB30NW10K) |
|
| NDT624 |
BOEING REFERENCE STANDARD 767 PT 4 53-80-02 |
|
| NDT625 |
BOEING REFERENECE STANDARD 767 PT4 55-10-03 |
|
| NDT627 |
BOEING REFERENCE STANDARD 767 PT 4 57-10-02 |
|
| NDT628 |
BOEING REFERENCE STANDARD 767 PT 4 53-50-01. Includes Test Report and Certificate of Conformance. |
|
| NDT630 |
BOEING REFERENCE STANDARD 767 PT 4 55-10-02 |
|
| NDT631 |
BOEING REFERENCE STANDARD 767 PT 4 71-20-01 |
|
| NDT632 |
BOEING REFERENCE STANDARD 767 PT4 71-20-01 |
|
| NDT633 |
BOEING REFERENCE STANDARD 767 PT 6 54-51-02. Includes Test Report and Certificate of Conformance. |
|
| NDT634 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-02 |
|
| NDT636 |
BOEING REFERENCE STANDARD 767 PT 4 32-10-03 |
|
| NDT637 |
BOEING REFERENCE STANDARD 767 PT 4 32-10-04 |
|
| NDT637P1 |
POSITIONER FOR NDT637 |
|
| NDT637P2 |
POSITIONER FOR NDT637 |
|
| NDT637P3 |
POSITIONER FOR NDT637 |
|
| NDT638 |
BOEING REFERENCE STANDARD 767 PT 4 57-40-02 PAGE 5 FIG.2 |
|
| NDT638G |
POSITIONER GUIDE 767 PT 4 57-40-02 PAGE 7 FIG.4 |
|
| NDT638PL |
POSITIONER 767 PT 4 57-40-02 PAGE 6 FIG.3 |
|
| NDT638PR |
POSITIONER 767 PT 4 57-40-02 PAGE 6 FIG.3 |
|
| NDT639 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-02 |
|
| NDT640 |
BOEING REFERENCE STANDARD 767 PT4 54-50-01 |
|
| NDT641 |
BOEING REFERENCE STANDARD 767 PT4 54-50-01 |
|
| NDT642 |
BOEING REFERENCE STANDARD 767 PT 4 53-50-02 |
|
| NDT643 |
BOEING REFERENCE STANDARD 767 PT 6 57-20-03 |
|
| NDT644 |
BOEING REFERENCE STANDARD 767 PT 4 57-20-02 |
|
| NDT648 |
BOEING REFERENCE STANDARD 767 PT 6 53-30-06 FIGURE 3 PAGE 32. FASTENERS: (BACR15CE8D). Includes Test Report and Certificate of Conformance. |
|
| NDT650 |
BOEING REFERENCE STANDARD |
|
| NDT651 |
BOEING REFERENCE STANDARD 767 |
|
| NDT652 |
BOEING REFERENCE STANDARD 767 PT 6 57-20-07 FASTENER (BACB30YP10K6) |
|
| NDT655 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-03 |
|
| NDT656 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-03 |
|
| NDT657 |
BOEING REFERENECE STANDARD 767 PT 6 53-10-09 FASTENER (BACB30NW6K5X + BACC30M6, BACB30NW8K + BACC30M8) |
|
| NDT658 |
BOEING REFERENCE STANDARD 767 PT 4 53-10-01 |
|
| NDT660 |
BOEING REFERENCE STANDARD 767 PT 6 53-80-04 FASTENER (BACB30NW8K7 + BACC30M8) |
|
| NDT661 |
BOEING REFERENCE STANDARD 767 PT 4 53-30-01 |
|
| NDT662 |
BOEING REFERENCE STANDARD 767 PT 4 57-20-03 |
|
| NDT663A |
BOEING REFERENCE STANDARD 767 PT 6 53-10-13 FIG 3 FASTENER (BACB30NW8K + BACC30M8) |
|
| NDT663B |
BOEING REFERENCE STANDARD 767 PT 6 53-10-13 FIG 3 FASTENER (BACB30NW8K + BACC30M8) |
|
| NDT664 |
BOEING REFERENCE STANDARD 767 PT 6 57-20-06 FIG 2 |
|
| NDT665 |
BOEING REFERENCE STANDARD 767 PT 6 53-10-06 PAGE 4 FIGURE 2. Includes Test Report and Certificate of Conformance. |
|
| NDT666A |
BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FIG 3 FASTENER (BACB30PT5K13 + BACN10WM) |
|
| NDT666B |
BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FIG 4 FASTENER (BACB30PT5K12 + BACN10WM) |
|
| NDT666C |
BOEING REFERENCE STANDARD 767 PT 6 57-20-08 FIG 5 FASTENER (BACB30PT4K9 + BACN10WM) |
|
| NDT667 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-05 |
|
| NDT668 |
BOEING REFERENCE STANDARD 767 PT 6 57-50-01. |
|
| NDT669 |
BOEING REFERENCE STANDARD 767 PT 4 32-10-05 FIG 2 |
|
| NDT669P |
POSITIONER |
|
| NDT670 |
BOEING REFERENCE STANDARD 767 PT 4 53-10-02 FASTENER (BACB30NW8K + BACC30M8) |
|
| NDT671 |
BOEING REFERENCE STANDARD 767 PT 6 53-30-12 FIG 2 FASTENER (BACB30MY8K + BACC30M8) |
|
| NDT672 |
BOEING REFERENCE STANDARD 767 PT 6 54-50-01 FASTENER (BACB30NX6K2 + BACC30X6S) |
|
| NDT674 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-06 PAGE 14 FIGURE 3. Includes Certification Report. |
|
| NDT675 |
BOEING REFERENCE STANDARD 767 PT 4 54-50-006 |
|
| NDT676 |
BOEING REFERENCE STANDARD FOR PW4000 and JT9D-7R4D/E STRUTS FIGURE 2 PART 4 54-50-07 PAGE 9 |
|
| NDT679 |
BOEING REFERENCE STANDARD 767 53-50-05 PT 4 FIG 3. Includes.Test Report and Certificate of Conformance. |
|
| NDT680 |
BOEING REFERENCE STANDARD 767 PT 4 32-10-06 FIG 2 |
|
| NDT682 |
BOEING REFERENCE STANDARD 767 PT 6 53-80-02 FIG 2 FASTENER (BACR15FT5D4) |
|
| NDT684 |
BOEING REFERENCE STANDARD 767 PT6 53-32-02 |
|
| NDT685 |
BOEING REFERENCE STANDARD 767 PT 6 53-10-18 FASTENER (BACR15FV6KE5, BACR15BB6AD5) |
|
| NDT686 |
BOEING REFERENCE STANDARD 767 PT 6 5-50-09 FIG 3 |
|
| NDT687 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-08 PAGE 6 FIGURE 3 |
|
| NDT688 |
BOEING REFERENCE STANDARD PT 4 57-50-03 FASTENER (BACB30MY10K4, BACB30NW10K4 + BACC30M10) |
|
| NDT689 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-06 |
|
| NDT689P |
TRANSDUCER POSTIONER 767 PT 4 57-50-06 |
|
| NDT690 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-04 PAGE 8 FIGURE 3. Includes Test Report and Certificate of Conformance. |
|
| NDT690-P1 |
POSITIONER PT 4 57-50-04. MATERIAL: ACETAL(DELRIN). Includes Certificate of Conformance. |
|
| NDT690-P2 |
POSITIONER PT 4 57-50-04. MATERIAL: ACETAL(DELRIN). Includes Certificate of Conformance. |
|
| NDT690-P3 |
POSITIONER PT 4 57-50-04. MATERIAL: ACETAL(DELRIN). Includes Certificate of Conformance. |
|
| NDT691 |
BOEING REFERENCE STANDARD 767 PT 6 -57-50-08 PAGE 6 FIGURE 2 |
|
| NDT691P |
TRANSDUCER POSITIONER |
|
| NDT693 |
BOEING REFERENCE STANDARD 767 PT 4 53-50-04 |
|
| NDT694 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-05 PAGE 8 FIGURE 3 |
|
| NDT695 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-05 PAGE 8 FIGURE 3 |
|
| NDT697 |
BOEING REFERENCE STANDARD 767 PT 4 57-50-07 PAGE 5 FIGURE 2 |
|
| NDT697P |
SUPPORT COLLAR FOR TEK-5005F PT 4 57-50-07 FIG 3. This item is included at no additional charge with the purchase of TEK-5005F(AFC-0510F). Includes Certificate of Conformance. |
|
| NDT698 |
BOEING REFERENCE STANDARD PT 4 57-50-03 FASTENER (BACB30MY10K4 + BACC30M10) |
|
| NDT700A |
DO NOT USE, REPLACED WITH NDT6000A-E FASTENER (BACB30MY10K5 + BACC30M10, BACB30MY10K6 + BACC30AG10) |
|
| NDT700B |
DO NOT USE, REPLACED WITH NDT6000A-E FASTENER (BACB30MY10K6 + BACC30M10) |
|
| NDT700C |
DO NOT USE, REPLACED WITH NDT6000A-E FASTENER (BACB30MY10K8 + BACC30M10) |
|
| NDT700D |
DO NOT USE, REPLACED WITH NDT6000A-E FASTENER (BACB30MY10K5 + BACC30M10, BACB30MY10K6 + BACC30AG10) |
|
| NDT700E |
DO NOT USE, REPLACED WITH NDT6000A-E FASTENER (BACB30MY10K9 + BACC30M10) |
|
| NDT702 |
|
|
| NDT706 |
BOEING REFERENCE STANDARD 777-200/300 PT 6 53-10-01 page 5. Includes Test Report and Certificate of Conformance. |
|
| NDT706P |
BOEING REFERENCE STANDARD 777 PT 6 53-10-01 |
|
| NDT710 |
BOEING REFERENCE STANDARD 777 PT 6 54-51-01. IncludesTest Report and Certificate of Conformance. |
|
| NDT711 |
BOEING REFERENCE STANDARD 777 PT 6 54-51-01. IncludesTest Report and Certificate of Conformance. |
|
| NDT712 |
BOEING REFERENCE STANDARD 777 PT 6 54-51-01 PAGE 11 FIGURE 4. HOLE DIAMETER= 1.63"(41.4mm) IncludesTest Report and Certificate of Conformance. |
|
| NDT713 |
BOEING REFERENCE STANDARD 777 PT 6 53-10-02 FASTENER (BACR15FT6D-5, BACR30VT6K-3, BACB30VT6K-3 + BACC30BL6). IncludesTest Report and Certificate of Conformance. |
|
| NDT714 |
BOEING REFERENCE STANDARD 777 53-10-03 PT 6 FIG 2 FASTENER (BACB30VU6K3, BACR15FV6KE7, BACR15CE6D7). IncludesTest Report and Certificate of Conformance. |
|
| NDT720 |
BOEING REFERENCE STANDARD 777 FIG 2 |
|
| NDT723 |
MUST PURCHASE FROM BOEING. CONTACT JOHN LINN 562 797-3792 OR 425 246-9245 |
|
| NDT725 |
BOEING REFERENCE STANDARD 777 PT 4 55-17-01 |
|
| NDT726 |
BOEING REFERENCE STANDARD PART 6 54-51-04 PAGE 5 FIGURE 2. MATERIAL: 15-5PH STAINLESS STEEL |
|
| NDT727G |
BOEING PROBE GUIDE 777 PT 54-51-06 |
|
| NDT728 |
BOEING REFERENCE STANDARD 777 PT 6 57-20-05 |
|
| NDT729 |
BOEING REFERENCE STANDARD 777 PT 4 53-10-03 |
|
| NDT730 |
BOEING REFERENCE STANDARD 777 PART 4 57-54-01 PAGE 6 FIGURE 2 |
|
| NDT731 |
BOEING REFERENCE STANDARD 777 PT 4 53-40-01 |
|
| NDT732A |
BOEING REFERENCE STANDARD 777 PT 6 55-17-03 FIG 2 FASTENER (BACB30US9K10, BACN10HR9CS, BACW10BPACU. IncludesTest Report and Certificate of Conformance. |
|
| NDT733 |
BOEING REFERENCE STANDARD 777 PT 4 53-40-03 |
|
| NDT735 |
BOEING REFERENCE STANDARD 777 P 4 53-40-02 |
|
| NDT736 |
BOEING 777 REFERENCE STANDARD PART 4 53-60-02 FIGURE 2 PAGE 6. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| NDT736A |
BOEING REFERENCE STANDARD 777 PT6 57-10-04 |
|
| NDT736B |
BOEING REFERENCE STANDARD 777 PT6 57-10-04 |
|
| NDT737 |
BOEING REFERENCE STANDARD 777 PT 6 53-50-03 FIG 2 FASTENER (BACB30NX12K15, BACB30NX12K13 + BACC30BH12S) |
|
| NDT738 |
BOEING REFERENCE STANDARD 777 PT 4 53-10-02 |
|
| NDT739 |
BOEING REFERENCE STANDARD 777 PT 4 53-10-02 |
|
| NDT740 |
BOEING REFERENCE STANDARD 777 PT 4 53-10-01 |
|
| NDT741 |
BOEING REFERENCE STANDARD 777 PT 4 57-12-01 PAGE 7 FIGURE 2. Includes Test Report and Certificate of Conformance |
|
| NDT744 |
BOEING REFERENCE STANDARD 777 PT 6 53-10-09 FIG 2 FASTENER (BACR15FV6KE) |
|
| NDT745 |
BOEING REFERENCE STANDARD 777 PT 4 57-20-01 FASTENER (BACB30WQ7K15L + BACN10TN7K) |
|
| NDT746 |
BOEING REFERENCE STANDARD 777 PT 6 53-60-07 |
|
| NDT747-1 |
BOEING REFERENCE STANDARD 777 PT 6 53-00-11 FASTENER (BACR15FVKE). Includes Test Report and Certificate of Conformance. |
|
| NDT747-2 |
BOEING REFERENCE STANDARD 777 PT 6 53-00-11 FASTENER (BACR15FV8KE). Includes Test Report and Certificate of Conformance. |
|
| NDT747-R&D-V2 |
BOEING REFERENCE STANDARD SET R&D THICKNESS .100 , .130 , .160 , .200 , .250 |
|
| NDT747 R&D |
BOEING REFERENCE STANDARD R&D |
|
| NDT748 |
BOEING REFERENCE STANDARD 777 PT 4 54-51-01 |
|
| NDT749 |
BOEING REFERENCE STANDARD 777 pt 6 57-20-03 |
|
| NDT753 |
BOEING REFERENCE STANDARD 777 PT 4 57-20-04 |
|
| NDT755 |
BOEING REFERENCE STANDARD 777 PT 6 53-60-07 |
|
| NDT756 |
BOEING REFERENCE STANDARD PT 6 53-60-07 |
|
| NDT757 |
BOEING REFERENCE STANDARD 777 PT 4 57-20-03 |
|
| NDT760 |
BOEING REFERENCE STANDARD 777 PT 6 53-60-06 FASTENER (BACB30WR6K*L + BACN10HY6M). IncludesTest Report and Certificate of Conformance. |
|
| NDT761 |
BOEING 777 REFERENCE STANDARD PART 4 53-80-01 FIGURE 2 PAGE 9. Includes Test Report and Certificate of Conformance. |
|
| NDT762 |
BOEING 777 REFERENCE STANDARD PART 4 54-51-02 FIGURE 2 PAGE 8. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. |
|
| NDT763 |
BOEING REFERENCE STANDARD 777 PT 4 54-51-04. IncludesTest Report and Certificate of Conformance. |
|
| NDT766 |
BOEING REFERENCE STANDARD 777 PT 4 57-10-02 PAGE 9 FIGURE 2. IncludesTest Report and Certificate of Conformance. |
|
| NDT767 |
BOEING REFERENCE STANDARD 777 PT 4 57-10-02 PAGE 11 FIGURE 3. IncludesTest Report and Certificate of Conformance. |
|
| NDT768 |
BOEING 777 REFERENCE STANDARD PART 4 57-10-01 PAGE 6 FIGURE 2. IncludesTest Report and Certificate of Conformance. |
|
| NDT769 |
BOEING 777 REFERENCE STANDARD PART 4 57-10-01 PAGE 7 FIGURE 3. IncludesTest Report and Certificate of Conformance. |
|
| NDT771 |
BOEING 777 REFERENCE STANDARD PART 4 57-10-05 PAGE 7 FIGURE 2 |
|
| NDT772 |
BOEING REFERENCE STANDARD 777 PT 4 57-10-04 FIGURE 4 PAGE 18. Includes Test Report and Certificate of Conformance. |
|
| NDT773 |
BOEING REFERENCE STANDARD 777 PT 4 57-10-04 FIGURE 5 PAGE 19. Includes Test Report and Certificate of Conformance. |
|
| NDT774 |
BOEING 777 REFERENCE STANDARD PART 4 57-10-05 PAGE 8 FIGURE 3 |
|
| NDT778 |
BOEING 777 REFERENCE STANDARD. PART 4, 78-30-05 pg.8 |
|
| NDT779 |
BOEING REFERENCE STANDARD 777 PT 4 54-51-01 |
|
| NDT780-A |
BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 |
|
| NDT780-B |
BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 |
|
| NDT780-C |
BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 |
|
| NDT780-D |
BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 |
|
| NDT780-E |
BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 |
|
| NDT780-F |
BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 |
|
| NDT781 |
BOEING REFERENCE STANDARD 777 PT 6 57-40-02 PAGE 6 FIGURE 2. FASTENER (BACR15CE6). Includes Test Report and Certificate of Conformance... |
|
| NDT782 |
BOEING REFERENCE STANDARD R&D |
|
| NDT783 |
BOEING REFERENCE STANDARD R&D |
|
| NDT784 |
BOEING REFERENCE STANDARD R&D |
|
| NDT785-EXT |
12" WORKING LENGTH FLEXABLE EXTENSION HANDLE |
|
| NDT785-T1 |
45° SHORTWAVE TRANSDUCER |
|
| NDT785-T2 |
45° SHORTWAVE TRANSDUCER |
|
| NDT785-T3 |
45° SHORTWAVE TRANSDUCER |
|
| NDT786-A |
BOEING REFERENCE STANDARD 777 PAT 6 57-10-04 PAGE 6 FIGURE 2. |
|
| NDT786-B |
BOEING REFERENCE STANDARD 777 PAT 6 57-10-04 PAGE 6 FIGURE 2. |
|
| NDT786R&D |
BOEING REFERENCE STANDARD R&D |
|
| NDT787 |
BOEING REFERENCE STANDARD 777 PT 6 53-80-06 FASTENER (BACR15FT6D4) |
|
| NDT789 |
BOEING REFERENCE STANDARD 777 PT 6 57-20-03 |
|
| NDT790 |
BOEING REFERENCE STANDARD 777 PT 6 57-20-03 |
|
| NDT791 |
BOEING REFERENCE STANDARD 777 PT 6 57-20-03, FASTENER (BACB30XT8K6 + BACC30BK8) |
|
| NDT792 |
BOEING REFERENCE STANDARD 777 PT 6 57-20-03 |
|
| NDT796 |
BOEING REFERENCE STANDARD |
|
| NDT797 |
BOEING REFERENCE STANDARD 777-200/300 PART 4 53-40-06 PG.11 FIGURE 2. MATERIAL: 7075-T7 ALUMINUM WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. |
|
| NDT801 |
BOEING REFERENCE STANDARD 787-8 51-13-02-00A-280A-A |
|
| NDT803A |
BOEING REFERENCE STANDARD ABS PLASTIC THICKNESS MEASUREMENT. PART 4 51-00-07 page 11 figure 2 |
|
| NDT803B |
BOEING REFERENCE STANDARD ABS PLASTIC THICKNESS MEASUREMENT. PART 4 51-00-07 page 11 figure 2 |
|
| NDT811 |
BOEING CALIBRATION STANDARD FIGURE 3 DETAIL II. MATERIAL: 2024-T351 ALUMINUM or 7075-T651 ALUMINUM. |
|
| NDT813 |
BOEING REFERENCE STANDARD |
|
| NDT814 |
BOEING REFERENCE STANDARD |
|
| NDT815 |
BOEING 787 REFERENCE STANDARD. PT 4 57-10-01 PAGE 10. MATERIAL 2024 or 7075 ALUMINUM. 6 EDM NOTCHES .007"W x .100" x .100" CORNER |
|
| NDT816 |
BOEING REFERENCE STANDARD R&D. MATERIAL: 6AL-4V TITANIUM. INCLUDES DELRIN PLUG. |
|
| NDTt3276 |
BOENING R&D REFERENCE STANDARD 2024-T3 ALUMINUM. |
|
| NRK-3A/2024-T3 |
CUSTOM NAVY BLOCK 2024-T3 ALUMINUM. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Confromance. |
|
| NRK-3AL |
CUSTOM NAVY BLOCK 7075-T6,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Confromance. |
|
| NRK-3AL-6061 |
CUSTOM NAVY BLOCK 6061-T6,20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Confromance. |
|
| NRK-3AST |
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... |
|
| NRK-3S |
CUSTOM NAVY BLOCK 4340 WITH 20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES |
|
| NRK-3S/17-4 |
CUSTOM NAVY REFERENCE STANDARD. MATERIAL: 17-4PH TH1050 STAINLESS STEEL. CONTAINS 20 FASTENER HOLES (.156-.750) WITH A TOTAL OF 71 EDM NOTCHES. Includes Test Report and Certificate of Conformance. |
|
| NRK-3S/17-7 |
CUSTOM NAVY REFERENCE STANDARD. 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-3ST |
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-3T |
CUSTOM NAVY BLOCK, 6AL-4V TITANIUM ,WITH 20 FASTENER HOLES (.156-.750) CONTAINING A TOTAL OF 71 EDM NOTCHES NOTCHES |
|
| P564A |
BOEING TRANSDUCER POSITIONER PT 4 57-50-01 |
|
| P564B |
BOEING TRANSDUCER POSITIONER PT 4 57-50-01 |
|
| P6020A |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 9 FIGURE 2. Includes Certificate of Conformance. |
|
| P6020B |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 9 FIGURE 2. Includes Certificate of Conformance. |
|
| P6021A |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 10 FIGURE 3. Includes Certificate of Conformance. |
|
| P6021B |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 10 FIGURE 3. Includes Certificate of Conformance. |
|
| P6021C |
BOEING TRANSDUCER POSITIONER 767 PART 4 57-50-14 PAGE 10 FIGURE 3. Includes Certificate of Conformance. |
|
| P8-STD-031A |
BOEING REFERENCE STANDARD FASTENER (BACB30NN3K7 + BACN10YR3CD + NAC1149D0363J, BACR15GD6D4) |
|
| P8-STD-031B |
BOEING REFERENCE STANDARD FASTENER (BACB30NN3K7 + BACN10YR3CD + NAS1149D0363J, BACR15FP6E6R, BACR15GF6D6, BACR15FP5E6R) |
|
| P8-STD-031C |
BOEING REFERENCE STANDARD FASTENER (BACR15FP6E7R) |
|
| P8-STD-031D |
BOEING REFERENCE STANDARD FASTENER (BACR15GF5D6, BACR15FP5E6R, BACB30NN3K7 + BACN10YR3CD + NAC1149D0363J) |
|
| P8-STD-031E |
BOEING REFERENCE STANDARD FASTENER (BACR15GF5D6, BACR15FP5E6R, BACR15GF5D5) |
|
| P8-STD-031F |
BOEING REFERENCE STANDARD FASTENER (BACB30NN3K3 + BACN10YR3CD3 + NAS1149D0363J) |
|
| P8-STD-031G |
BOEING REFERENCE STANDARD FASTENER (BACR15FP6E7R, BACR15FP6E6R) |
|
| P8-STD-P010 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P011 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P022A |
BOEING REFERENCE STANDARD |
|
| P8-STD-P022B |
BOEING REFERENCE STANDARD |
|
| P8-STD-P022C |
BOEING REFERENCE STANDARD |
|
| P8-STD-P031DEV3 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P031DEV4 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P031DEV5 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P031DEV6 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P033 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P034 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P035 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P036 |
BOEING REFERENCE STANDARD |
|
| P8-STD-P037-AL |
BOEING REFERENCE STANDARD |
|
| P8-STD-P037-TI |
BOEING REFERENCE STANDARD |
|
| P8-STD-P038A |
BOEING REFERENCE STANDARD |
|
| P8-STD-P038B |
BOEING REFERENCE STANDARD |
|
| P8-STD-P039 |
BOEING REFERENCE STANDARD |
|
| P8A-STD-P028A |
BOEING REFERENCE STANDARD |
|
| PDL 1030J |
HERCULES C-130 UT CALIBRATION STANDARD FIGURE 17 SHEETS 1&2 20-40-00. FASTENER (HL18PB6-8, HL18PB6-6, HL70-6). Includes Test Report Traceable to NIST and Certificate of Conformance. |
|
| PDL 1034J/1040J |
CALIBRATION STANDARD 20-40-00 FIG 18 7075-T6 ALUMINUM |
|
| PDL 1035J |
KINGPIN RISER TRANSDUCER, C130 SMP-C-NDI 20-40-00: FIG 19, PG.28 |
|
| PDL 1036 |
C-130 TRUSS MOUNT UPPER LUG INSPECTION TRANSDUCER, 5MHz., "A" & "B" SMP 515-C INSPECTION PROCEDURE FOR WINGS CHAPTER 57. Includes Test Report and Certificate of Conformance. |
|
| PDL 1037AJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 PAGE 30 FIG 20, 7075-T6 ALUMINUM |
|
| PDL 1037BJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 PAGE 31 FIG 21, 7075-TG ALUMINUM |
|
| PDL 1155 |
CALIBRATION STANDARD FIGURE 3 FASTENER (BACB30NX12K11, BACB30NX14K8, HL1012-12) |
|
| PDL 1214J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 22 |
|
| PDL 1215J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 23 PAGE 33, 7075-T6 ALUMINUM |
|
| PDL 1217AJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 24 PAGES 34, 7075-T6 ALUMINUM |
|
| PDL 1217BJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 25 PAGE 35, CAST ACRYLIC SHEET |
|
| PDL 1217CJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 26 PAGE 36, CAST ACRYLIC SHEET |
|
| PDL 1253 |
CALIBRATION STANDARD FIGURE 20-49 FASTENER (HLT114-6-8 + KFN542-3) |
|
| PDL 1254J |
HERCULES C-130 UT CALIBRATION STANDARD FIGURE 21 SHEETS 1-4 20-40-00. FASTENER (HLT116 HI-LOCK FASTENERS WITH SELF LOCKING NUTS). Includes Test Report Traceable to NIST and Certificate of Conformance. |
|
| PDL 1256 |
NEED DRAWING |
|
| PDL 389J |
LOCKHEED C-130 CALIBRATION STANDARD 7075-T6 ALUMINUM FIGURE 1 |
|
| PDL 419J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 2 PAGE 4, 2024-T3 ALUMINUM |
|
| PDL 447J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 4, 7075-T6 ALUMINUM |
|
| PDL 449J |
LOCKHEED C-130 CALIBRATION STANDARD FIGURE 5, 7075-T6 ALUMINUM |
|
| PDL 457AJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 6 PAGES 8&9 SHEET 1&2, 7075-T6 ALUMINUM |
|
| PDL 457SJ |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 6 PAGES 8&9 SHEET 1&2, 4340 STEEL |
|
| PDL 457SS |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 6 PAGES 8&9 SHEET 1&2 304 STAINLESS STEEL |
|
| PDL 459J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 7 PAGE 10, 7075-T6 ALUMINUM |
|
| PDL 601J |
CALIBRATION STANDARD FIGURE 20-29 |
|
| PDL 843J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 9 FASTENER (HL21-6-4 + TLN 1030.3) |
|
| PDL 874 |
CALIBRATION STANDARD 20-40-00 FIG 10 |
|
| PDL 917 |
LOCKHEED C 130 CALIBRATION STANDARD FIGURE 2 PAGE 14. 7075-T6 ALUMINUM OR EQUIVALENT. |
|
| PDL 919J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 11 SHEET 1&2, 7075-T6 ALUMINUM, FASTENERS (HL64PB-10-9, HLT114-6-8, HLT18PB-12, HL70) |
|
| PDL 920J |
CALIBRATION STANDARD FIGURE 12 FASTENER (HLT114-6-8, HLPB8-8, HL18PB10-8, HL 206-4) |
|
| PDL 941J |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 FIGURE 13 PAGE 19, 7075-T6 ALUMINUM |
|
| PDL 943J |
CALIBRATION STANDARD FIGURE 14 PG.20 FASTENER (HL54-6-6, HL54-6-5, COLLAR (HL70-6) SMP-515-C NDI; 20-40-00, 7075-T6 ALUMINUM |
|
| PDL 944-2J |
CALIBRATION STANDARD FIGURE 15 FASTENER (HL40-6-5 + HL70-6, NAS6208-11 + KFN5428), 7075-T6 ALUMINUM |
|
| PDL 958 |
LOCKHEED C-130 CALIBRATION STANDARD 20-40-00 PAGE 23 FIGURE 16 2024-T3 ALUMINUM |
|
| PDL 980 |
C-130 Lower Engine Mount Longeron-Fwd End Calibration Standard. 7075-T6 Aluminum... |
|
| PWA28403B |
PRATT & WHITTNEY ENGINE BLADE REFERENCE STANDARD |
|
| QO-QTS-TI-03-001 |
Air Force reference standard Detail#1. Material 7075-T6 Aluminum. EDM Notch size: .050" x .050" x .005" Max Width, 10 Flaws total. Includes Test Report and Certificate of Conformance. |
|
| QQI-519630 |
TEST BLOCK STANDARD QQI FLAW DEPTH OF 30% SHIM THICKNESS, .002" PACK OF 5EA |
|
| QQI TEST BAR |
QQI Test Bar. 6.0" x 2.0" x .25" Material: 4130 or 4340 CRES Steel |
|
| R&D BOND/DISBOND SKIN |
.074 2024-T3 TOP PLATE W/36 HOLES |
|
| RD11-02 |
MD REFERENCE STANDARD MDC-K5225 SECTION 2-1 FIG 1.6 |
|
| RD11-03 |
MD11 REFERENCE STANDARD MDC-K5225 SECTION 2-1 |
|
| RM2-117-1603 |
Custom IAI Calibration Standard. Material: Top/Bottom plates 7075-T651 Aluminum, 1 each surface plate 4340 Steel and 7075-T651 Aluminum, steel bushing Includes Test Report and Certificate of Conformance. |
|
| RM8-331-1603 |
Custom IAI Calibration Standard. Material: Top plate 7075-T651 Aluminum, Bottom Plate 4340 Steel. Includes Test Report and Certificate of Conformance. |
|
| RS-502 |
ASTRA G100 REFERENCE STANDARD, PG.613: 04-00-00 FIG.605 |
|
| RS-502-C |
ASTRA G100 REFERENCE STANDARD, 2 EDM FATIGUE CRACKS 2.4mm X 1.2mm (PG.613: 04-00-00 FIG.605) |
|
| RS9000-1 |
DC9 REFERENCE STANDARD PER BOEING SB DC9-54A031 PAGE 16 FIGURE 1. Includes Test Report and Certificate of Conformance. |
|
| SAAB 5341-151-01I |
REFERENCE STANDARD SAAB 340 FIG.1 5341-151-01I PART 4 PAGE 5. MATERIAL: 4140 CRES STEEL. Includes Test Report and Certificate of Conformance. |
|
| SAAB 5512-332-03I |
SAAB 340 REFERENCE STANDARD 5512-332-03I FIGURE 1 PAGE 2, 55-10-00 PART 6 PAGE 3. MATERIAL: 2024-T351 ALUMINUM WITH 4 HL10 VAP-6-7 HI-LOK FASTENERS.. Includes Test Reprort and Certificate of Conformance. |
|
| SB 146/53-167/2 |
BAE SYSTEMS REFERENCE STANDARD, AVRO 146-RJ, ISB.53-167AP2 |
|
| SB 57-3329 FIG.9 |
Raytheon 12 Hole Standard Calibration Block Figure 9 Page 20, Service Bulletin SB 57-3329. Hole sizes 9/64, 11/64,3/16 and 13/64. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. |
|
| SB09530016-5/303SS |
DOUGLAS REFERENCE STANDARD 53-253, 303/SS |
|
| SB09530016-5/AL |
DOUGLAS REFERENCE STANDARD 53-253, 7075-t651 |
|
| SB09530016-5/TI |
DOUGLAS REFERENCE STANDARD 53-253, TITANIUM |
|
| SB09540030-5 |
DC9 SURFACE REFERENCE REFERENCE STANDARD DC9-54-030. MATERIAL: 17-7 PH STAINLESS STEEL. EDM NOTCH: 0.002"-0.010" WIDE x 0.030" DEEP. |
|
| SB09550023-17 |
Douglas Reference Standard Assembly 55-23 Figure1 sheets 1-5, Pages 31-35. Material: 2024-T3 Aluminum. Includes Test Report Traceable to NIST and Certificate of Conformance. |
|
| SB10270203-5 |
Douglas Reference Standard Inboard Slat Drive Arm. Bulletin A27-203. Figure1 sheet 11, Pages 31-35. Material: HY-TUF or 4000 Series Steel CAD Plated. Includes Test Report Traceable to NIST and Certificate of Conformance. |
|
| SB11530001-5 |
DOUGLAS MD-11 REFERENCE STANDARD. MD11-53-001 FIGURE 1 SHEET 1. MATERIAL: 7075-T6 ALUMINUM |
|
| SE.4.44 |
328JET CALIBRATION STANDARD (SE.4.44); 51-60-01 PAGE 9/10 FIG.605 EDDY CURRENT |
|
| SO111-7 |
Custom FOKKER F28 Horizontal Stab. Drive Junction Fitting Eddy Current Standard per drawing # 28. 0-3210/2610-Material: 7075-T6. Includes Test Report and Certificate of Conformance. |
|
| SORFIT 146/164/1 |
BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-19 PG 9 FIG 5. Includes Test Report and Certificate of Conformance. |
|
| SORFIT 146/166/1 |
BAE REFERENCE STANDARD 146-RJ 53-238 PG 10 FIG 5 |
|
| SP-078 |
CALIBRATION STANDARD BATS |
|
| SP-096 |
CALIBRATION STANDARD BATS 53-30-30 |
|
| SP-115 |
CALIBRATION STANDARD BATS |
|
| SP-265 |
LOCKHEED C-130 STEP BLOCK. PROCEEDURE SMP 515-C. PAGE 9 MATERIAL: 7075-T6 ALUMINUM. |
|
| SS TYPE 301 |
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" |
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| SS TYPE 304 |
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: 304 STAINLESS STEEL. SIZE: 1.5"W x 3.75"L x .25" |
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| SSI 55-11-115/1 |
BAE 146-RJ SERIES REFERENCE STANDARD 55-11-10 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance. |
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| SSI 57-20-151/152A/153A/1 |
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-50 PT 6 FIGURE 6&7 PAGES 10&11. Includes Test Report and Certificate of Conformance. |
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| SSI57-20-151/152A/153A/2 |
BAE 146-RJ SERIES REFERENCE STANDARD 57-20-50 PT 6 FIGURE 8&9 PAGES 12&13. Includes Test Report and Certificate of Conformance. |
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| ST 4340 |
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: 4340 STEEL. SIZE: 1.5"W x 3.75"L x .25". Includes certification Report ... |
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| ST4130 |
BOMBARDIER / CANADAIR EDDY CURRENT SURFACE REFERENCE STANDARD PART 6 55-20-001, NOTCHES .008", .020", .040" (.005" Wide +000 / - .002 and +/- .001" Depth), MATERIAL: 4130 STEEL. Includes certification Report and Certificate of Conformance(COC)... |
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| ST8809C-1-A |
BOEING TOOL ST8809C LETTER CODE A 7075-T73 ALUMINUM |
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| ST8809C-1-B |
BOEING TOOL ST8809C LETTER CODE B 2024-T3 ALUMINUM |
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| ST8809C-1-C |
BOEING TOOL ST8809C LETTER CODE C 6AL-4V TITANIUM |
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| ST8809C-1-D |
BOEING TOOL ST8809C LETTER CODE D 17-7 PH ANNEALED STAINLESS STEEL |
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| ST8809C-1-E |
BOEING TOOL ST8809C LETTER CODE E 4340CRES STEEL |
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| TI-6AL-4V |
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: 6AL-4V TITANIUM. SIZE: 1.5"W x 3.75"L x .25" |
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| TI-6AL-6V-2SN |
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: TI-6AL-6V-2SN TITANIUM. SIZE: 1.5"W x 3.75"L x .25" |
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| TP54 |
AIRBUS REFERENCE STANDARD A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. |
|
| TP54-07-1 |
AIRBUS SPLIT CALIBRATION REFERENCE STANDARD A318-A321 51-63-07-991-002 PB1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. |
|
| TRS-6-12A |
Custom 6 Step Wedge .020", .040", .080", .150" ,0.300", 0.600" +/-.001", Per Drawing Specification TXX003503. Material: 2219-T81 Aluminum. Includes Teflon Base. |
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| TRS-6-12I |
Custom 6 Step Wedge .040", .050", .060", .075" ,0.090", 0.110" +/-.001", Per Drawing Specification TXX003461. Material: 718 Inconel. Includes Teflon Base. |
|
| USAFNDT-169 |
Air Force modified reference standard of Boeing 171 Outboard Wing Spanwise Splice Stringers. 57-10-07 Figure 4 Sheet 2 page 30. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. |
|
| USAFNDT-171 |
Air Force modified reference standard of Boeing 171 Outboard Wing Spanwise Splice Stringers. 57-10-07 Figure 4 Sheet 2 page 30. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. |
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| USAFNDT-172 |
Air Force modified reference standard of Boeing 171 Outboard Wing Spanwise Splice Stringers. 57-10-07 Figure 4 Sheet 2 page 30. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. |
|
| UT-010-057 |
Bell Hellicopter ASB-212-02-116 Blade Grip UT Inspection Reference Standard. Material: 2024-T6 or Equivalent Conductivity of 2124-T8 Aluminum. |
|
| V2-AL |
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-CS |
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 |
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| V2-SS |
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). ..304 Stainless Steel with case |
|
| 317 |
BOEING REFERENCE STANDARD PART 6 53-10-16 PAGE 5 FASTENERS (BACB30MR5C10 + BACN10GW5) |
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