Reference Standard

BAE 146-RJ SERIES REFERENCE STANDARD 53-30-02 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 53-30-01 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 53-30-01 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 53-30-03 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 53-30-04 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE REFERENCE STANDARD 146-RJ 53-238 53-40-06 PT 6 FIGURE 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance.

Airbus Reference standard 53-41-04-991-002-A Sheet 01 part 6 page 11. Includes Test Report and Certificate of Conformance.

BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-31-42 PG 7 FIG 3. Includes Test Report and Certificate of Conformance.

BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 55-31-43 PG 8 FIG 4. Includes Test Report and Certificate of Conformance.

BAE REFERENCE STANDARD 146-RJ 53-238 55-20-11 PT 6 FIGURE 5 PAGE 9. Includes Test Report and Certificate of Conformance.

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.

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.

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.

BAE JETSTREAM SERIES 4100 57-10-36 PT 6

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-12 PT 4 FIGURE 6&7 PAGES 11&12. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-12 PT 4 FIGURE 6&7 PAGES 11&12. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-52 PT 6 FIGURE 5&6 PAGES 11&12. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-52 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-55 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-55 PT 4 FIGURE 5&6 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-50 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-48 PT 6 FIGURE 3&4 PAGES 7&8. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-10-42 PT 6 FIGURES 4&5 PAGE 7&8. Material: 7075-T6 & 2014A-T6 Aluminum. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-20-24 PT 6 FIGURES 5&6 PAGE 9&10. Material: 2024-T3 & 2024-T6 Aluminum. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-20-28 PT 6 FIGURES 4&5 PAGE 9&10. Material: 2024-T3 & 2024-T6 Aluminum. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-20-10 PT 4 FIGURES 4 PAGE 8. Includes Test Report and Certificate of Conformance.

CUSTOM BOEING REFERENCE STANDARD 7075-T6 ALUMINUM

BOEING REFERENCE STANDARD 767 PT 4 32-10-01 FIG 2 Includes Test Report and Certificate of Conformance.

BOEING REFERENCE STANDARD 767 PT 4 55-10-01 FIG 1. Includes Test Report and Certificate of Conformance.

BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1

BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1

BOEING REFERENCE STANDARD 767 PT 6 22-10-01 FIG 2. Includes Test Report and Certificate of Conformance.

BOEING REFERENCE STANDARD 767 PT 6 22-10-01

Aluminum Block 110mm(3.937″) x 18mm(7.09″) x 15mm(.591″) Block. Material: 6061-T6 Aluminum. Includes Test Report and Certificate of Conformance.

BOEING REFERENCE STANDARD 767 PT 4 27-80-01 FIG 4 Includes Test Report and Certificate of Conformance.

TRANSDUCER WEDGE

TRANSDUCER WEDGE

BOEING REFERENCE STANDARD 767 PT 4 32-20-01 FIG 2. Includes Test Report and Certificate of Conformance.

Cessna Model 500 Calibration Standard 53-30-03-0 Rev. 14 Figure 4 Sheet 1 Inspection. Material: 2024-T3. Includes Test Report and Certificate of Conformance.

EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008″, .020″, .040″ +/-.001 DEEP, (MAX WIDTH .005″), 6AL-6V-2SNTi

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″)

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″)

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″)

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″)

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″)

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39

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″)

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″)

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″)

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39

717-200 REFERENCE STANDARD ISOLATOR LUG. FIG. 1.1 SHEET 1, PAGE 1. MATERIAL: 4340 NORMALIZED STEEL PER MIL-S-5000. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD FOR THE LOWER CENTER WING SKIN PANELS AT STRINGER 16 &18. PAGES 1-11. MATERIAL: 2024-T3, 7075-T6 &7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.16 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.4 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.21 SHEET 1-3, PAGES 1-3. MATERIAL: 2014-T6 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.8 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.12 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.13 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.14 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.15 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD FIGURE 1.17 SHEETS (1-4 ), PAGES 1-4. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.22 SHEET 1-7, PAGES 1-7. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.23 SHEET 1-6, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance.

BOEING 717-200 REFERENCE STANDARD FIGURE 1.24. MATERIAL: 6AL-4V. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.18 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

717-200 REFERENCE STANDARD…FIG. 1.19 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

A53-142 Douglas DC-9 7637987-9 Reference Standard Assembly 2024-T3 Clad Aluminum. Figure 1, Sheets 2&3

Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4″ x 7″ x 1.06″. Contains twenty (20) fastener holes with diameters from 0.156 to 0.750″, two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004″ for all notches. Material is 7075-T6 Aluminum. Finished standard is anodized per MIL-A-8625, Type II, Class I. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49. NSN 6635-01-092-5129, P/N 7947479-10. Includes Certification Report Traceable to NIST.

Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4″ x 7″ x 1.06″. Contains twenty (20) fastener holes with diameters from 0.156 to 0.750″, two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004″ for all notches. Material: 718 Inconell. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49. NSN 6635-01-092-5129, P/N 7947479-10. Includes Test Report and Certificate of Conformance. Includes Certification Report Traceable to NIST.

Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4″ x 7″ x 1.06″. Contains twenty (20) fastener holes with diameters from 0.156 to 0.750″, two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004″ for all notches. Material is 4340 Steel. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49.NSN 6635-01-512-4952, P/N 7947479-10. Includes Certification Report Traceable to NIST.

Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4″ x 7″ x 1.06″. Contains twenty (20) fastener holes with diameters from 0.156 to 0.750″, two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004″ for all notches. Material is 6AL-4V Titanium. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49. Includes Certification Report. Includes Certification Report Traceable to NIST.

Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4″ x 7″ x 1.06″. Contains twenty (20) fastener holes with diameters from 0.156 to 0.750″, two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004″ for all notches. Material: 17-4PH stainless steel alloy heat treated to TH1050. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49. NSN 6635-01-092-5129, P/N 7947479-10. Includes Certification Report Traceable to NIST.

Air Force General Purpose Eddy Current Standard. Standard is a three (3) plate assembly measuring 4″ x 7″ x 1.06″. Contains twenty (20) fastener holes with diameters from 0.156 to 0.750″, two (2) screw holes, and two (2) dowel pins holes. Standard also contains a total of 66 EDM notches in various locations. Notch depth and length vary. Width is 0.004″ for all notches. Material: 304 stainless steel. Manufactured in accordance with U.S.A.F. Tech Order 33B-1-1, Figures 4-47 through 4-49. NSN 6635-01-092-5129, P/N 7947479-10. Includes Test Report and Certificate of Conformance. Includes Certification Report Traceable to NIST.

MD-80 REFERENCE STANDARD SECTION 2-1 FIGURE13

MD-80 REFERENCE STANDARD 57.80.007

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD 57.80.012

717-200 REFERENCE STANDARD…FIG. 1.6 SHEET 1-4, PAGES 1-4. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance.

MD-80 REFERENCE STANDARD

717-200 REFERENCE STANDARD…FIG. 1.5 SHEET 1-5, PAGES 1-5. MATERIAL: 7075-T6 CLAD ALUMINUM, 2014-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.53.80.003

717-200 REFERENCE STANDARD…FIG. 1.2 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 or 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.

MD-80 REFERENCE STANDARD 54.80.002

BOEING REFERENCE STANDARD. MATERIALS: -3 DETAIL ALUMINUM SKIN 2024-T351, -5 DETAIL ALUMINUM STRINGER 2024-t351, -7 DETAIL ALUMINUM 7075-T6511, -9 DETAIL ALUMINUM 7075-T73 and -11 DETAIL ALUMINUM 7075-T73. Includes Test Report and Certificate of Conformance.

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…

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD

MD-80 REFERENCE STANDARD

MAIN WHEEL BEAD SEAT WHEELL PROBE FOR BOEING 707

AIRBUS REFERENCE STANDARD, 53-16-02 Part 6 FIGURE 603 PG. 605-606 . Includes Test Report and Certificate of Conformance.

AIRBUS REFERENCE STANDARD PT 6 57-10-33 PAGE 404 FIGURE 404. . Includes Test Report and Certificate of Conformance.

AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-46 Page 404 Figure 403. Material:7050. Includes Test Report and Certificate of Conformance.

AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-46 Page 404 Figure 404. Material:7050. Includes Test Report and Certificate of Conformance.

AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 13 FIGURE 8, SSI NO. 54-10-07. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance.

AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.41 FIGURE 29, SSI NO. 54-10-08. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance.

AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.25 FIGURE 16, SSI NO. 54-40-09. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance.

AIRBUS REFERENCE STANDARD A300-600 Part 4 54-50-23 Page 404 Figure 403. Material: 30NCD16 or Equivalent. Includes Test Report and Certificate of Conformance.