| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| NDT3021 | REFERENCE STANDARD B | 6 | |
| NDT396 | REFERENCE STANDARD B | 6 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| (CALIB) 98S54305001202 | CALIBRATION REFERENCE STANDARD | 1 | |
| (CALIB) 99A51107299001 | STANDARD, REFERENCE (CALIBRATION) (CALIBRATION) | 1 | |
| (CALIB) 99A57204436000 | STANDARD STANDARD, REFERENCE - INCLUDING (CALIBRATION) (CALIBRATION) | 1 | |
| (CALIB) 99A57504296000 | REFERENCE STANDARD (CALIBRATION) | 2 | |
| (CALIB) 99D54403001002 | REFERENCE STANDARD (CALIBRATION) (CALIBRATION) | 1 | |
| (CALIB) C12-PCS-3C1N | REFERENCE STANDARD COMPOSITE (CALIBRATION) | 1 | |
| (CALIB) CREF5-04174559100 | CONDUCTIVITY REFERENCE STANDARD (CALIBRATION) | 1 | |
| (CALIB) HORIZONTAL STAB SLINGS | CALIBRATE AND RE-CERTIFY THIS TOOL (HORIZONTAL STAB SLINGS) IN ACCORDANCE WITH BOEING DWG C55007 REV. D (OR LATER) AND LOLER 1998 (OR LATER). TEST/CALIBRATION CERTIFICATE MUST REFERENCE MAINTENANCE DATA (MANUAL/STANDARD) AND REVISION USED. ADDITIONAL REFE | 1 | |
| (CALIB) NDT3282 | REFERENCE STANDARD (CALIBRATION) | 2 | |
| (CALIB) NDT3305B | REFERENCE STANDARD (CALIBRATION) | 1 | |
| 019 | BOEING REFERENCE STANDARD 7075-T6 ALUMINUM 7075 57-10-07 PART 6 PG.216. | 1 | |
| 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 | 1 | |
| 039 | BOEING 707 REFERENCE STANDARD 2024-T3 ALUMINUM DETAIL 3 FIGURE 8 SHEET 9 BBL 70.5 SPLICE 707-300/400..PART 6, 57-30-07 PG.73 | 1 | |
| 1 H-STAB REF STD | Boeing Reference standard | 1 | |
| 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. | 2 | |
| 10RS.01.1 | BOEING REFERENCE STANDARD KC10 Page 1-6 MATERIAL: 2024-T3, 7075-T6, 6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| 10RS.02 | BOEING REFERENCE STANDARD KC10 53.10.001, 53.10.013/.014 Page 1-8 Material: 2024-T3 and 7075-T6, 6AL-4V or Phenolic. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 10RS.20aFN | Reference Standard, Bolt (Facimile), H-11 Steel, DC-10 SID, 8.25" Length, 1.25" Diam., An, Bn, & Cn Notches | 1 | |
| 10RS.20bFN | Reference Standard, Bolt (Facimile), H-11 Steel, DC-10 SID, 9.5" Length, 1.25" Diam., An, Bn, & Cn Notches | 1 | |
| 10RS.48 | BOEING REFERENCE STANDARD - KC10. Page 1-23. Material: 2024-T3, 7075-T6, and 7150-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| 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 | 1 | |
| 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 | 1 | |
| 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 | 1 | |
| 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 | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 126 | BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4. Includes Test Report and Certificate of Conformance. | 7 | |
| 127-0.032 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.036 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.040 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.050 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.063 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.071 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.080 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.090 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.100 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.110 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-0.125 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127-XXX | Corrosion reference standard Calibration Block | 1 | |
| 127A | BOEING REFERENCE STANDARD - 0.032” AL | 1 | |
| 127A-.032 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 2 | |
| 127A-.036 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.036/2024 | Boeing reference standard | 1 | |
| 127A-.040 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.050 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.063 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.072 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.072/2024 T3 CALD | Boeing reference standard | 1 | |
| 127A-.080 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.090 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.100 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.110 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-.125 | BOEING REFERENCE STANDARD 737 / 747 PT 6 51-00-00 FIG.12 PG. 2-3. Includes Test Report and Certificate of Conformance. | 1 | |
| 127A-032 | Boeing reference standard | 2 | |
| 128 | BOEING REFERENCE STANDARD 767 PT 6 51-00-06 PAGE 4 FIGURE 1, MATERIAL: Aluminum Alloy. Includes Test Report and Certificate of Conformance. | 1 | |
| 130C | BOEING REFERENCE STANDARD Part 6 53-50-00 Page 13 Figure 1. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| 134 | Boeing Reference Standard 707 Part 4 53-40-07 Page 12 Figure 2 (Sheet 6) Detail 3. Material: 4330M or Equivalent. Includes Test Report and Certificate of Conformance. | 4 | |
| 1409-00-2 | KIT REFERENCE STANDARD NDI- TORQUE BOX. NDI WING ASSY. | 11 | |
| 145-15998-001 | EMBRAER REFERENCE STANDARD 54-50-00 FIG 603, 4340 STEEL | 3 | |
| 145-44130-401 | KIT REFERENCE STANDARD NDI- TORQUE BOX. NDI WING ASSY. | 3 | |
| 145-44131-001 | EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Aluminum(7050-T745) Includes Test Report and Certificate of Conformance. | 6 | |
| 145-44131-003 | EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Steel(15-SPH 5/8") Includes Test Report and Certificate of Conformance. | 3 | |
| 145-44131-005 | EMBRAER REFERENCE STANDARD 57-26-00 PT 2 FIG 601, Titanium(Titanium Galy US AMS2631 CLAI 1/2") Includes Test Report and Certificate of Conformance. | 3 | |
| 145-54-0008 | EMBRAER REFERENCE STANDARD 54-50-00 FIG 606, 4340 STEEL | 1 | |
| 145T09065-401 | EMBRAER LEGACY REFERENCE STANDARD. GSE 606 54-00-00 Page 8&9. Includes Test Report and Certificate of Conformance. | 1 | |
| 15-5 PH | CALIBRATION REFERENCE STANDARD, 15-5 PH STAINLESS STEEL, CONTAINING 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES, (MHIRJ OR EQUIVALENT) | 1 | |
| 15-5PH | CALIBRATION REFERENCE STANDARD 15-5 PH STAINLESS S | 1 | |
| 15−5 PH | Calibration reference standard 15−5 PH stainless steel containing 0.008 in. (0.20 mm)0.020 in. (0.51 mm) and 0.040 in. (1.02 mm) deep electrical discharge machined notches (Bombardier Inc. or equivalent) | 1 | |
| 171-00844-601 16E1 | EMBRAER REFERENCE STANDARD 7075-T7 ALUMINUM.Includes Test Report and Certificate of Conformance. | 1 | |
| 171T17969-401 | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance. | 3 | |
| 17P9M2007 | Douglas Reference Standard Assembly For the Ultrasonic Calibration of Upper Wing Skin to common Stringer, Figure24-4 sheets 253. Material: 7075 Aluminum. Includes Test Report Traceable to NIST and Certificate of Conformance. | 1 | |
| 181 | BOEING REFERENCE STANDARD 707 PART 6 55-10-07 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 182 | BOEING REFERENCE STANDARD 707 PART 6 55-10-07 PAGE 17. Includes Test Report and Certificate of Conformance. | 1 | |
| 185 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 & 777-200/300 51-00-04 PROCEDURE 1 PAGE 8. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 3 | |
| 186ABCDEF | BOEING CUSTOM COMBINATION REFERENCE STANDARD 777 PT 6 51-00-02 Figures 1&2, Pages 6-7, HOLE SIZE 0.1875", .2500", .3125", .3750", .4375", .500. Each hole size marked with the corresponding Boeing Part number 186A-186F Includes Test Report and Certific... | 1 | |
| 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. | 3 | |
| 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. | 4 | |
| 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. | 4 | |
| 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. | 4 | |
| 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. | 3 | |
| 188A | BOEING REFERENCE STANDARD PT 651-00-00-1 FIG 6. Includes Test Report and Certificate of Conformance. | 5 | |
| 189 | BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4 PG.13 & 737 PT 6 51-00-00 PROCEDURE 23 PG.11 FIG.7. Includes Test Report and Certificate of Conformance. | 7 | |
| 192 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13. Includes Test Report and Certificate of Conformance. | 4 | |
| 194 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 FIGURE 1., BOEING 757 PART 6 53-30-02 PAGE 5 FIGURE 2 | 9 | |
| 194A | BOEING REFERENCE STANDARD 767 PT 6 53-30-02 FIG 3 PAGE 5. Includes Test Report and Certificate of Conformance. | 4 | |
| 1TD1133D07001-2001 | Seyer Industries reference standard. Material: 2024-T351 Aluminum...Chamfer EDM Notch Size: .030" x .030" x .005" +/- .002"...Bore EDM Notch Size: .030" x .030" x .005" +/- .002". Includes Test Report and Certificate of Conformance. Part Serial Number:... | 1 | |
| 2-164-551 | REFERENCE STANDARD BLOCK | 2 | |
| 2-887-01-9314S | SPLIT CONICAL BLOCK (AIRBUS REFERENCE STANDARD) | 5 | |
| 2-887-01-9315S | SPLIT CONICAL BLOCK (AIRBUS REFERENCE STANDARD) | 4 | |
| 2-887-01-9316S | SPLIT CONICAL BLOCK (AIRBUS REFERENCE STANDARD) | 3 | |
| 2-887-01-9319S | SPLIT CONICAL BLOCK (AIRBUS REFERENCE STANDARD) | 3 | |
| 2-887-01-9321S | SPLIT CONICAL BLOCK (AIRBUS REFERENCE STANDARD) | 3 | |
| 20134E | CALIBRATION REFERENCE STANDARD | 1 | |
| 203026-101 | TGB BEVEL GEAR - REFERENCE STANDARD, CALIBRATION RING EWR | 1 | |
| 204-94034-1 | Boeing Reference Standard- Lower Lug APE-1 Primary , D204-12769-6 ASIP Inspection Program. Material: 4340 Steel. Includes Test Report and Certificate of Conformance. | 1 | |
| 206 | BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 19. MATERIAL 2024 ALUMINUM (FASTENERS: BACR15DG10DD14)Includes Test Report and Certificate of Conformance. | 3 | |
| 208 | BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 19. MATERIAL 2024 ALUMINUM (FASTENERS: BACB30PT5-10, BACN10TN5)Includes Test Report and Certificate of Conformance. | 1 | |
| 212-A1325-01 | AIRBUS MILITARY REFERENCE STANDARD COM 212-266 PG 13 | 1 | |
| 239 | BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 18. MATERIAL 2024 ALUMINUM (FASTENERS: BACR15DG10DD)Includes Test Report and Certificate of Conformance. | 1 | |
| 240 | BOEING REFERENCE STANDARD 727 PT 6 57-10-27 FIG 18. MATERIAL 2024 ALUMINUM (FASTENERS: BACR15DG10DD)Includes Test Report and Certificate of Conformance. | 1 | |
| 2506F | S/B 57-200 Douglas DC-9 Reference Standard 7075-T6 Aluminum. Figure 5, 6,7 | 1 | |
| 262 | BOEING REFERENCE STANDARD 727 PT 6 53-10-27 | 1 | |
| 262A | BOEING REFERENCE STANDARD 727 PT 6 53-10-27 | 1 | |
| 263 | BOEING REFERENCE STANDARD 727 PT 6 53-10-27 PAGE 4 FIG 1. Includes Test Report and Certificate of Conformance. | 1 | |
| 2683301-1 | Cessna reference standard 55-10-02-0 (Rev 1).Model 208 Inspection of Horizontal Stabilizer Spars. | 4 | |
| 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. | 2 | |
| 272 | BOEING REFERENCE STANDARD 727, PT 6 55-10-27 FIG. 2 Includes Test Report and Certificate of Conformance. | 1 | |
| 285 | BOEING REFERENCE STANDARD 727 PART 6 57-10-27 FASTENER (BACB30NM7K23). Includes Test Report and Certificate of Conformance. | 1 | |
| 286 | BOEING REFERENCE STANDARD 727 PART 6 57-10-27 FASTENER (BACB30NM7K21). Includes Test Report and Certificate of Conformance. | 1 | |
| 296 | BOEING REFERENCE STANDARD 727 PT 6 53-30-27 Includes Test Report and Certificate of Conformance. | 1 | |
| 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..... | 4 | |
| 29A029 | AIRBUS REFERENCE STANDARD 3 EDM NOTCH AL | 5 | |
| 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. | 3 | |
| 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. | 5 | |
| 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. | 2 | |
| 29A49 | AIRBUS REFERENCE STANDARD 3 EDM NOTCH STEEL | 1 | |
| 301 GUIDE | BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION | 1 | |
| 302 GUIDE | BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION | 1 | |
| 305 | BOEING REFERENCE STANDARD 737 PART 6 57-10-18 FIGURE 2 PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 312 | BOEING REFERENCE STANDARD 737 PART 6 53-10-17 PAGE 6 FIGURE 2. 2024-T3 ALUMINUM Includes Test Report and Certificate of Conformance. | 7 | |
| 313A/313B | BOEING REFERENCE STANDARD 737 PART 6 53-10-17 PAGE 7 FIGURE 3. 2024-T3 ALUMINUM | 1 | |
| 315 | BOEING REFERENCE STANDARD 737 PART 4 55-30-01 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance. | 4 | |
| 316 | BOEING REFERENCE STANDARD 737 PART 4 55-30-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 31A008 | AIRBUS REFERENCE STANDARD 51-63-01 PT 6 FIG 601. MATERIAL: 4340 STEEL. 3 EDM SLOTS (0.2mm, 0.5mm,1.0mm DEEP) x (0.05-0.25mm WIDE). Includes Test Report and Certificate of Conformance... | 1 | |
| 320 | BOEING REFERENCE STANDARD 737 PART 6 55-10-19 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 321 | BOEING REFERENCE STANDARD 737 PART 6 53-10-19 FIGURE 3 PAGE 6. Includes Test Report and Certificate of Conformance. | 7 | |
| 323A | BOEING REFERENCE STANDARD 737 PART 4 55-50-01 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 323B | BOEING REFERENCE STANDARD 737 PART 4 53-10-38 FIGURE 2 PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 326 | BOEING REFERENCE STANDARD 737 PART 6 53-10-28 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance. | 1 | |
| 328A | Boeing Reference standard 737 pt 6 53-10-38 | 1 | |
| 328A/328B | BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 2 PAGE 7. | 1 | |
| 328AB | Boeing Reference Standard 737 PT6 53-10-38 | 1 | |
| 328B | Boeing Reference standard, 737, pt 6 53-10-38 | 1 | |
| 328C | Boring Reference Standard, PT6 53-10-38 | 1 | |
| 328C/328D | BOEING REFERENCE STANDARD 737 PART 6 53-10-38 FIGURE 3 PAGE 8. | 1 | |
| 328CD | Boeing Reference Standard, 737 pt 6 53-10-38 | 1 | |
| 328D | Boeing Reference Standard, PT6 53-10-38 | 1 | |
| 335 | BOEING REFERENCE STANDARD 737 PT 6 53-10-31. Includes Test Report and Certificate of Conformance. | 10 | |
| 336A | BOEING REFERENCE STANDARD 737 PART 6 57-30-02 FIGURE 2 PAGE 5. | 1 | |
| 336B | BOEING REFERENCE STANDARD 737 PART 6 57-30-02 FIGURE 2 PAGE 5. | 1 | |
| 338A | BOEING REFERENCE STANDARD 737 PART 6 53-10-35 FIGURE 1 PAGE 6. MATERIAL: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 341 | BOEING REFERENCE STANDARD 737 PART 4 53-10-40 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance. | 1 | |
| 345 | BOEING REFERENCE STANDARD 737 PART 6 57-40-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 349 | BOEING REFERENCE STANDARD 737 PART 4 32-10-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 350 | BOEING REFERENCE STANDARD 737 PT 4 32-20-01 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 351A | BOEING REFERENCE STANDARD 737 PT 6 53-10-01 | 1 | |
| 351B | BOEING REFERENCE STANDARD 737 PT 6 53-10-01 | 1 | |
| 353ABC | BOEING REFERENCE STANDARD 737 PT6 53-10-12 | 1 | |
| 353D | BOEING REFERENCE STANDARD 737 PT 6 53-10-12 | 2 | |
| 354A | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | 4 | |
| 354B | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | 1 | |
| 354C | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | 1 | |
| 355A | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | 1 | |
| 355B | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | 1 | |
| 355C | BOEING REFERENCE STANDARD 737 PT 6 57-30-04 | 1 | |
| 356 | BOEING REFERENCE STANDARD 737 53-30-04 PART 6 PAGE 4 FIGURE 1. Includes test report and Certificate of Conformance. | 9 | |
| 363 | BOEING REFERENCE STANDARD PART 6 53-30-03 FIGURE 1 PAGE 6. Includes Test Report and Certificate of Conformance. | 5 | |
| 365 | BOEING REFERENCE STANDARD 737 PART 4 71-20-01 PG.4 FIGURE 1 DETAIL I. Includes Test Report and Certificate of Conformance. | 6 | |
| 367 | BOEING REFERENCE STANDARD 737 PT 6 71-20-01 Figure 4, PG. 10-12 (Sheets 1-3) Includes Test Report and Certificate of Conformance. | 4 | |
| 369 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 & 737 Part 6 53-30-05. Includes Test Report and Certificate of Conformance. | 2 | |
| 370 | BOEING REFERENCE STANDARD 737 PT 4 53-30-02 FIG 1. Includes Test Report and Certificate of Conformance. | 1 | |
| 375 | BOEING REFERENCE STANDARD 737 PT 4 55-10-02. Includes Test Report and Certificate of Conformance. | 3 | |
| 378 | BOEING REFERENCE STANDARD 737 PT 6 53-10-44 PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 383 | BOEING REFERENCE STANDARD 737 PART 6 53-30-07 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | 2 | |
| 401 | BOEING REFERENCE STANDARD 747 PT 4 57-10-01 Page 4 Figure 1. Includes Test Report and Certificate of Conformance. | 2 | |
| 402 | BOEING REFERENCE STANDARD 747 PT 4 57-10-04 Page 5 Figure 1. Includes Test Report and Certificate of Conformance. | 2 | |
| 403 | BOEING REFERENCE STANDARD PT 4 57-10-04 FIG 2, PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 403A/403B | BOEING REFERENCE STANDARD 747 PT 4 57-10-04 Page 6 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 404 | BOEING 747 REFERENCE STANDARD PART 6 57-10-08 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 5 | |
| 405 | BOEING REFERENCE STANDARD 747 PT 4 57-10-02 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 406 | BOEING REFERENCE STANDARD 747 PT 6 57-10-09 Page 6 Figure 2. Includes Test Report and Certificate of Conformance. | 12 | |
| 408 | BOEING REFERENCE STANDARD PT 4 57-10-03 FIG 2, PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 410 | BOEING REFERENCE STANDARD 747 PT 4 57-10-05 Page 6 Figure 3. Includes Test Report and Certificate of Conformance. | 4 | |
| 411 | BOEING REFERENCE STANDARD PT 6 55-10-04 FIG 1, PAGE 4. Includes Test Report and Certificate of Conformance. | 1 | |
| 412 | BOEING REFERENCE STANDARD PT 6 55-10-01 FIG 1, PAGE 3. Includes Test Report and Certificate of Conformance. | 1 | |
| 412B5MHZ35R80FE | CUSTOM 5MHz 35° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR WIT A 80mm RADIUS. USED WITH AIRBUS REFERENCE STANDARD PART NUMBER 98A54003096 Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-20 | 1 | |
| 412B5MHZ40R75FE | CUSTOM 5MHz 40° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR WIT A 75mm RADIUS. USED WITH AIRBUS REFERENCE STANDARD PART NUMBER 98A54003069 Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-20 | 1 | |
| 412E5MHZ60FE | CUSTOM 5MHz 60° IN FE TRANSVERSE WAVE BACKSHOOTING TRANSDUCER WITH A SIDE MOUNTED MICRODOT CONNECTOR. CASE SIZE: .690" x .354" x .354 Includes Test Report and Certificate of Conformance. REFERENCE STANDARD: 98A54003077 | 1 | |
| 423 | BOEING 747 REFERENCE STANDARD PART 6 57-10-17 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. | 3 | |
| 424 | BOEING 747 REFERENCE STANDARD PART 6 57-10-17 FIGURE 3 PAGE 9. Includes Test Report and Certificate of Conformance. | 3 | |
| 426 | BOEING REFERENCE STANDARD PT 4 55-10-01 FIG 1, PAGE 4. Includes Test Report and Certificate of Conformance. | 1 | |
| 431 | BOEING REFERENCE STANDARD PT 6 53-10-19 FIG 1, PAGE 6. Includes Test Report and Certificate of Conformance. | 3 | |
| 432 | BOEING REFERENCE STANDARD 747 PT 6 57-30-02 Page 4 Figure 1. Includes Test Report and Certificate of Conformance. | 1 | |
| 4340-3-0050 | DC9 REFERENCE STANDARD S/B 57-118 SERVICE SKETCH 2671 SHEET 4 OF 7. MATERIAL: 4340 STEEL. | 1 | |
| 435 | BOEING 747 REFERENCE STANDARD PART 6 57-10-20 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| 436 | BOEING 747 REFERENCE STANDARD PART 6 57-10-20 FIGURE 4 PAGE 8. Includes Test Report and Certificate of Conformance. | 3 | |
| 437 | BOEING REFERENCE STANDARD 747 53-10-01 PART 4 PAGE 11 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 438 | BOEING REFERENCE STANDARD 747 53-10-01 PART 4 PAGE 11 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 439 | BOEING 747 REFERENCE STANDARD PART 6 57-10-22 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 2 | |
| 440 | BOEING REFERENCE STANDARD 747 PT 4 57-10-11 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 441 | BOEING REFERENCE STANDARD 747 PT 4 57-10-10 Page 9 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 442 | BOEING REFERENCE STANDARD PT 4 53-10-02 FIG 2, PAGE 5. Includes Test Report and Certificate of Conformance. | 2 | |
| 443 | BOEING REFERENCE STANDARD PT 4 53-10-02 FIG 2, PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 446 | BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 447 | BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 448 | BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 3 | |
| 449 | BOEING REFERENCE STANDARD 747 PT 4 57-10-13 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 460 | BOEING REFERENCE STANDARD 747 PART 6 57-10-28, PAGE 3 FIGURE 1. Includes Test Report and Certificate of Conformance. | 1 | |
| 471 | BOEING REFERENCE STANDARD 747 PT 4 57-30-02 Page 4 Figure 1. Includes Test Report and Certificate of Conformance. | 5 | |
| 474 | BOEING REFERENCE STANDARD PT 6 53-10-20 FIG 1, PAGE 5. Includes Test Report and Certificate of Conformance. | 2 | |
| 475 | BOEING 747 REFERENCE STANDARD PART 6 57-10-27 FIGURE 1 PAGE 4. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 5 | |
| 476 | BOEING REFERENCE STANDARD PT 6 53-10-18 FIG 3, PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 477 | BOEING REFERENCE STANDARD PT 6 53-10-18 FIG 3, PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 478 | BOEING REFERENCE STANDARD PT 6 5-10-18 FIG 3 PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 482 | BOEING 747 REFERENCE STANDARD PART 6 55-10-08 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| 483 | BOEING 747 REFERENCE STANDARD PART 6 55-10-08 FIGURE 3 PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| 484 | BOEING 747 REFERENCE STANDARD PART 6 55-10-25 FIGURE 1 PAGE 4. Includes Test Report and Certificate of Conformance. | 2 | |
| 490 | BOEING REFERENCE STANDARD 747 PT 4 57-30-06 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 497 | BOEING REFERENCE STANDARD 767 PT 6 53-00-05 FIG 1. Includes Test Report and Certificate of Conformance. | 2 | |
| 506 | BOEING REFERENCE STANDARD 757 PT 4 57-40-01 FIG 3 Includes Test Report and Certificate of Conformance. | 4 | |
| 1002 | BOEING REFERENCE STANDARD PT 6 51-00-00 Part 6 FIG 4. Includes Test Report and Certificate of Conformance. | 4 | |
| 1003 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 14 and 51-00-06. Includes Test Report and Certificate of Conformance. | 6 | |
| 1004 | BOEING REFERENCE STANDARD PT 6 51-00-0 FIG 14 PARAGRAPPH 2.C. Includes Test Report and Certificate of Conformance. | 6 | |
| 1005 | Reference Standard Boeing | 6 | |
| 2006 | BOEING REFERENCE STANDARD 727 PART 6 57-10-27 FASTENER (BACB30NM7K19). Includes Test Report and Certificate of Conformance. | 1 | |
| 3230 | REFERENCE BLOCK (BOEING BONDED STANDARD 737) | 1 | |
| 3233 | REFERENCE BLOCK (BOEING BONDED STANDARD 737) | 4 | |
| 4004 | BOEING REFERENCE STANDARD 747 PART 4 53-40-01 PAGE 10 FIGURE 6. Includes Test Report and Certificate of Confromance. | 4 | |
| 4028 | BOEING REFERENCE STANDARD 747 PART 4 57-40-03 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance. | 4 | |
| 4029 | BOEING REFERENCE STANDARD 747 PART 4 55-50-01 FIGURE 1 PAGE 4.MATERIAL: 2024-T3 or 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| 4036 | BOEING REFERENCE STANDARD 747 PART 4 57-40-05 FIGURE 3 PAGE 6.MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance. | 7 | |
| 4057 | BOEING REFERENCE STANDARD 747 PT 6 53-30-03 | 2 | |
| 4059 | BOEING 747 REFERENCE STANDARD PART 4 57-10-12 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | 2 | |
| 4070 | BOEING REFERENCE STANDARD 747, PT 6 53-30-07. Includes Test Report and Certificate of Conformance. | 1 | |
| 4072 | BOEING REFERENCE STANDARD 747 PT 6 53-30-05. Material 2024-T3 Aluminum. Fasteners BACR15CE5D5, BACR15CE6D5. Includes Test Report and Certificate of Conformance. | 1 | |
| 11638 | REFERENCE STANDARD SB190-57-0031/02 | 1 | |
| 235502 | CASA CN-235 EDDY CURRENT REFERENCE STANDARD PART 5 57-10-05 PAGE 510 FIGURE 504b. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| 5290024-1 | CESSNA CALIBRATION REFERENCE STANDARD | 1 | |
| 53-10-126/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-0126/1 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 53-10-137 | BAE 146-RJ SERIES REFERENCE STANDARD SET OF 8 UNITS, 53-10-12 PT 6 FIGURE 7 PAGES 907-910. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 53-10-192/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-25 PT 6 FIGURES 6&7 PAGES 10&11. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 53-20-149/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-65 PT 6 FIGURE 11&12 PAGES 16&17. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 53-20-157/2 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-84 PT 6 FIGURE 8 PAGE 12. Includes Test Report and Certificate of Conformance. | 1 | |
| 53-20-165/2 | RADIUSED ULTRASONIC PROBE SHOE USED WITH K5K AND REFERENCE STANDARD 53-20-165/1 (BAe 146 Series) | 1 | |
| 53-20-167/1 | BAE REFERENCE STANDARD 146-RJ 53-238 53-20-21 PT 4 FIGURE 4 PAGE 519. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 53-20-169/2 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-21 PT 4 FIGURE 3 PAGES 505. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 53-20-171/2 | RADIUSED ULTRASONIC PROBE SHOE USED WITH K5K(AFC-525-7S) AND REFERENCE STANDARD 53-20-165/1 (BAe 146 Series). Includes Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 53-20-180/3 | BAE REFERENCE STANDARD 146-RJ 53-20-88 FIG 4&5, PAGES 8&9. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 53-30-131/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-30-01 PT 6 FIGURE 4&5 PAGES 8&9. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 53-40-125/1 | BAE REFERENCE STANDARD 146-RJ 53-238 53-40-06 PT 6 FIGURE 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance. | 1 | |
| 53-41-04-991-002-A | Airbus Reference standard 53-41-04-991-002-A Sheet 01 part 6 page 11. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 55-31-NDT 1 | BAE REFERENCE STANDARD 146-RJ 53-238 55-20-11 PT 6 FIGURE 5 PAGE 9. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 55-36-01 | UT CALIBRATION REFERENCE STANDARD , STEP WEDGE, 7000 SERIES ALUMINUM, GENERIC AS PER ATR 72 NTM 55-36-01 | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 57-10-119/1 | 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. | 1 | |
| 57-20-148A/1 | 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. | 1 | |
| 57-20-163/1 | 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. | 1 | |
| 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. | 1 | |
| 57-54-103C | CUSTOM BOEING REFERENCE STANDARD 7075-T6 ALUMINUM | 1 | |
| 602 | BOEING REFERENCE STANDARD 767 PT 4 32-10-01 FIG 2 Includes Test Report and Certificate of Conformance. | 1 | |
| 603 | BOEING REFERENCE STANDARD 767 PT 4 55-10-01 FIG 1. Includes Test Report and Certificate of Conformance. | 1 | |
| 604A | BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1 | 1 | |
| 604B | BOEING REFERENCE STANDARD 767 PT 6 53-60-01 FIG 1 | 1 | |
| 605 | BOEING REFERENCE STANDARD 767 PT 6 22-10-01 FIG 2. Includes Test Report and Certificate of Conformance. | 4 | |
| 605A | BOEING REFERENCE STANDARD 767 PT 6 22-10-01 | 1 | |
| 608 | BOEING REFERENCE STANDARD 767 PT 4 27-80-01 FIG 4 Includes Test Report and Certificate of Conformance. | 1 | |
| 610 | BOEING REFERENCE STANDARD 767 PT 4 32-20-01 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| 6583102-1 | BLOQUE PATRON CESSNA REFERENCE STANDARD | 1 | |
| 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") | 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") | 1 | |
| 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") | 1 | |
| 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") | 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") | 1 | |
| 71658-18-53/2&3 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39 | 1 | |
| 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") | 1 | |
| 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") | 1 | |
| 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") | 1 | |
| 71658-7-35/1&4 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39 | 1 | |
| 717RS9 | BOEING 717-200 REFERENCE STANDARD FIGURE 1.24. MATERIAL: 6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| 7637987-19 | CUSTOM SPO-2664 SLIDING PROBE FIXTURE USED WITH DC-10 REFERENCE STANDARD 7637987-15 Includes Certificate of Conformance | 1 | |
| 7637987-9 | A53-142 Douglas DC-9 7637987-9 Reference Standard Assembly 2024-T3 Clad Aluminum. Figure 1, Sheets 2&3 | 1 | |
| 787-EC57-70-01A | Boeing 787 Reference Standard | 1 | |
| 787-FT-ET-18B | REFERENCE STANDARD 787-FT-ET-18B, | 1 | |
| 787-FT-ET-26C | BOEING REFERENCE STANDARD | 1 | |
| 787-FT-UT-14 | BOEING METAL REFERENCE STANDARD | 1 | |
| 7947479-10 | REFERENCE STANDARD - AL 7075-T6, SPEC USAF T.O. 33-B-1-1 | 3 | |
| 7947479-10-304 | PH TOOL REFERENCE STANDARD STAINLESS SPEC USAF TO 33-B-1-1 | 1 | |
| 7947479-10-T | PH TOOL REFERENCE STANDARD TITANIUM SPEC USAF TO 33-B-1-1 | 2 | |
| 80RS24 | BOEING REFERENCE STANDARD. MATERIALS: -3 DETAIL ALUMINUM SKIN 2024-T351, -5 DETAIL ALUMINUM STRINGER 2024-t351, -7 DETAIL ALUMINUM 7075-T6511, -9 DETAIL ALUMINUM 7075-T73 and -11 DETAIL ALUMINUM 7075-T73. Includes Test Report and Certificate of Conformanc | 1 | |
| 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... | 1 | |
| 98A53803014001 | AIRBUS REFERENCE STANDARD, 53-16-02 Part 6 FIGURE 603 PG. 605-606 . Includes Test Report and Certificate of Conformance. | 3 | |
| 98A53803018000 | AIRBUS REFERENCE STANDARD PT 6 57-10-33 PAGE 404 FIGURE 404. . Includes Test Report and Certificate of Conformance. | 2 | |
| 98A53803019000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-46 Page 404 Figure 403. Material:7050. Includes Test Report and Certificate of Conformance. | 3 | |
| 98A5380302000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-46 Page 404 Figure 404. Material:7050. Includes Test Report and Certificate of Conformance. | 1 | |
| 98A54003019 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 13 FIGURE 8, SSI NO. 54-10-07. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 1 | |
| 98A54003069 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.41 FIGURE 29, SSI NO. 54-10-08. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 1 | |
| 98A54003072 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.25 FIGURE 16, SSI NO. 54-40-09. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 1 | |
| 98A54003072000 | 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. | 2 | |
| 98A54003073 | IRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.28 FIGURE 21, SSI NO. 54-40-09. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 1 | |
| 98A54003073000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 54-50-23 Page 404 Figure 403. Material: Titanium. Includes Test Report and Certificate of Conformance. | 3 | |
| 98A54003074 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG.19 FIGURE 12, SSI NO. 54-40-07. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 1 | |
| 98A54003075 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 5 FIGURE 3, SSI NO. 54-10-03 Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 2 | |
| 98A54003077 | AIRBUS A300 REFERENCE STANDARD PART 4 54-40-00 PG. 5 FIGURE 3, SSI NO. 54-10-03. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance. | 2 | |
| 98A54003096 | AIRBUS A310 REFERENCE STANDARD PART4 54-50-20 PAGE 402 FIGURE 401. Includes Test Report and certificate of Conformance. | 1 | |
| 98A57103016001 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-04 PAGE 404 FIGURE 403. Includes Test Report and Cerificate of Conformance. | 2 | |
| 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... | 4 | |
| 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... | 4 | |
| 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... | 3 | |
| 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... | 3 | |
| 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... | 4 | |
| 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... | 3 | |
| 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... | 4 | |
| 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... | 3 | |
| 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... | 3 | |
| 98S53005021-000 | LFEC CALIBRATION REFERENCE STANDARD | 3 | |
| 98S53305004-000 | UT BOND TESTER REFERENCE STANDARD | 5 | |
| 98S53305005-000 | UT BOND TESTER REFERENCE STANDARD | 5 | |
| 98S53505006-000 | UT CALIBRATION REFERENCE STANDARD | 4 | |
| 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. | 6 | |
| 98S54305002-200 | UT CALIBRATION REFERENCE STANDARD | 5 | |
| 98S57105004-200 | UT CALIBRATION REFERENCE STANDARD | 4 | |
| 98S57105006-200 | UT CALIBRATION REFERENCE STANDARD | 3 | |
| 98S57105015-200 | UT CALIBRATION REFERENCE STANDARD | 3 | |
| 98S57205030.004 | UT CALIBRATION REFERENCE STANDARD , STEP WEDGE, 7000 SERIES ALUMINUM, GENERIC | 5 | |
| 999-6807-02 | US REFERENCE STANDARD, EQUIPMENT CALIBRATION PART | 1 | |
| 999-6807-03 | US REFERENCE STANDARD, EQUIPMENT CALIBRATION | 1 | |
| 99A51003000000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-00-02 Page 603/604 Figure 602. Includes Test Report an Certificate of Conformance. | 2 | |
| 99A51107299001 | AIRBUS REFERENCE STANDARD A300-600 51-10-13 FIG 4. Includes Test Report and Certificate of Conformance. | 5 | |
| 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... | 5 | |
| 99A51107300000-7075 | AIRBUS REFERENCE STANDARD A330 Part 6 51-10-16 Page 615 Figure 610. Material: 7075. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53003001100 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 6AL-4V TITANIUM. Includes Test Report an Certificate of Conformance. | 4 | |
| 99A53003001101 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM.. Includes Test Report an Certificate of Conformance. | 8 | |
| 99A53003001101/A1 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. Note: Holes A1-A6 | 2 | |
| 99A53003001101/A13 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. Note: Holes A13-A18 | 1 | |
| 99A53003001101/A7 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. Note: Holes A7-A12 | 1 | |
| 99A53003001102 | AIRBUS MULTI HOLE REFERENCE STANDARD A-318- A321 51-63-04 PART 6 FIGURE 601, PAGE 601/602. MATERIAL: STEEL Includes Test Report an Certificate of Conformance. | 5 | |
| 99A53003001103 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A 2024-T3 ALUMINUM. Includes. Includes Test Report and Certificate of Conformance. | 4 | |
| 99A53003001104 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A. MATERIAL: 6AL-4V (AMS4911)TITANIUM. Includes Test Report anc Certificate of Conformance... | 4 | |
| 99A53003001105 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A MATERIAL: AISI4130 STEEL. Includes Test Report and Certificate of Conformance... | 4 | |
| 99A53003001106 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A . MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 4 | |
| 99A53003001107 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A. MATERIAL: 6AL-4V(AMS4911) TITANIUM. Includes Test Report anc Certificate of Conformance. | 4 | |
| 99A53003001108 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A330, A340_500_600 51-63-05-991-001-A MATERIAL: AISI4130 STEEL. Includes Test Report and Certificate of Conformance... | 4 | |
| 99A53003005001 | AIRBUS REFERENCE STANDARD A300-600/ A310 PT 4 53-12-52 PG.404 FIGURE 404. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53103002000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 53-12-50 Page 407/408 Figure 403 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53107215000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 53-31-81 99A53107215000. Includes Test Report and Certificate of Conformance. | 5 | |
| 99A53107251000 | AIRBUS REFERENCE STANDARD A300-600 PT 4 53-19-14 FIGURE 402, PG. 403 . Includes Test Report and Certificate of Conformance. | 2 | |
| 99A53107265001 | AIRBUS REFERENCE STANDARD A300-600 PT 6 53-19-21 Page 606 Figure 604, Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53107282000 | AIRBUS REFERENCE STANDARD A300 Part 6 53-30-00 Page 6A/6B Figure 3A Material: 2024-T4 and 17-4PH Includes Test Report and Certificate of Conformance. | 1 | |
| 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... | 2 | |
| 99A53107287000 | AIRBUS REFERENCE STANDARD A318-A321 52-31-16. Includes Test Report and Certificate of Conformance. | 7 | |
| 99A53107290000 | AIRBUS REFERENCE STANDARD A300-600 PT6 53-19-24 FIGURE 604, PG. 604 . Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53203005000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 53-12-11 Page 407/408 Figure 403. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53203007000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 53-12-23 Paghe 404 Figure 403, Material: 2024 ro Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53307203000 | AIRBUS A300 REFERENCE STANDARD PART 4 53-30-10; PG. 5, FIG. 2 ALSO USED FOR PART 6; 53-30-20 | 1 | |
| 99A53307225000 | AIRBUS A300 REFERENCE STANDARD PART 6; 53-30-20 | 1 | |
| 99A53307236000 | AIRBUS REFERENCE STANDARD A330 53-21-36 FIG 618. Includes Test Report and Certificate of Conformance. Includes Test Report and Certificate of Conformance. | 4 | |
| 99A53307244000 | AIRBUS REFERENCE STANDARD PART 5 RESONANCE FREQUENCY A300 53-30-30 Page 9 Figure 3. Material: 2024-T3 Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 5 | |
| 99A53307274000-7075 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 6 51-10-16 Page 7 Figure 51-10-16-991-005-A. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53307292001 | AIRBUS REFERENCE STANDARD A318-A321 51-10-15-991-004-A. Includes Test Report and Certificate of Conformance. | 4 | |
| 99A53403003001 | AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance. | 3 | |
| 99A53403005001 | AIRBUS REFERENCE STANDARD PT 6 53-12-25 PAGE 605 FIGURE 604. . Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53403007000 | AIRBUS REFERENCE STANDARD A300-600 Part 6 53-15-78 Part 8 Page 604 Figure 603. Material: 2024-T3. Inlcudes Test Report and Certificate of Conformance. | 2 | |
| 99A53407285000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Part 6 53-30-01 Pate 605 Figure 604, Material: 2024-T3 Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53507286000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-51-09. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A53803004001 | AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53803009000 | Airbus Reference Standard. A300-600, Part 4 53-15-76 Page 401, Figure 403 | 2 | |
| 99A53803019 | AIRBUS REFERENCE STANDARD A300-600ST 53-15-43 FIGURE 403 PAGE 404 . Includes Test Report and Certificate of Conformance. | 1 | |
| 99A53803024000 | AIRBUS REFERENCE STANDARD A300-600 53-12-98 FIGURE 403, PG. 404 . Includes Test Report and Certificate of Conformance. | 1 | |
| 99A54403004000 | AIRBUS REFERENCE STANDARD A300-600 A300-54-6015. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A55107288000 | AIRBUS REFERENCE STANDARD A300-600 PT4 55-10-14 FIGURE 404, PAGE 406 . Includes Test Report and Certificate of Conformance. | 2 | |
| 99A55107289000 | AIRBUS REFERENCE STANDARD A300-600 PT4 55-10-14 FIGURE 405, PAGE 407 . Includes Test Report and Certificate of Conformance. | 2 | |
| 99A55109003000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 55-10-72 Page 407/408 Figure 403, Material: 7050-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 5 | |
| 99A55407322000 | AIRBUS REFERENCE STANDARD A330 Part 9 - Visual 55-40-00 Page 906 Figure 904 Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A55507262000 | Airbus Reference Standard, ..A310 51-60-90, Pg4, Fig 2 | 1 | |
| 99A57004001291 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-53-05 Page 405 Figure 403. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57004001320 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-25-37 Page 404 Figure 403 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57004101000 | AIRBUS REFERENCE STANDARD 57-21-25-270-801-A01 use green primer and silver metallic top coat for paint | 6 | |
| 99A57004101000-MOD | AIRBUS REFERENCE STANDARD WITH CERTIFICATE | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 99A57103005002 | AIRBUS REFERENCE STANDARD A310 PART 4 57-10-47 PAGE 406 FIGURE 403 Material: 2024-T351 ALUMINUM Includes Test Report and Certificate of Conformance. | 3 | |
| 99A57103009000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-44 Page 405 Figure 403. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103010000 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-41 FIGURE 403 PAGE 404. Material: 2024-T3 Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103011000 | AIRBUS A300-600 REFERENCE STANDARD PART 4, 57-10-41 FIGURE 404 PAGE 405 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103012000 | AIRBUS A300-6-- REFERENCE STANDARD PART 4, 57-10-41 FIGURE 405 PAGE 406 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103025001 | AIRBUS A300-600 REFERENCE STANDARD PART 4 57-10-10 PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. | 3 | |
| 99A57103028000 | AIRBUS REFERENCE STANDARD A300-600, Part 4 57-10-22 Page 404 Figure 403, Material: 2024-T3 or Equivalent. Includes Test Report and Certificate of Conformance. | 3 | |
| 99A57103031000 | AIRBUS REFERENCE STANDARD A310 Part 4 53-15-42 Page 408 Figure 403 Material: 2024 or Equivalent Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103033000 | AIRBUS REFERENCE STANDARD A310 Part 4 57-10-26 Page 405 Figure 403 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103036000 | AIRBUS REFERENCE STANDARD A310 Part 4 57-10-67 Page 404 Figure 403 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57103044000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-53 Page 406 Figure 403 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 1 | |
| 99A57103048001 | Airbus A300-600 Reference Standard Part 4 57-10-68 Page 409/410 figure 403. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57103050000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-64 Page 407/408 Figure 403 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57103051000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-26 Page 411/412 Figure 403 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57103053000 | AIRBUS REFERENCE STANDARD A310 Part 4 57-10-07 Page 409/410 Figure 403 Material: 7175 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57103054000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-10-24 Page 411/412 Figure 403 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 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) | 1 | |
| 99A57104329000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-21-04 Page 405 Figure 403. Material: L97(2024-T3) and BAEM1102(7075-T6). Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57104330000 | AIRBUS REFERENCE STANDARD A300-600 Part 4 57-21-04 Page 406 Figure 404. Material: L97(2024-T3) and BAEM1102(7075-T6). Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57104353000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-08 Page 409 Figure 404(Sheet 2) Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57104353001 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-08 Page 410 Figure 404 (Sheet 3) MATERIAL:2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| 99A57104354000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-08 Page 406/407 Figure 403 (Sheet 2 and 3) Material: Delrin. lncludes Test Report and Certificate of Conformance. | 2 | |
| 99A57104355000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-08 Page 406/407 Figure 403 (Sheet 2 and 3) Material: Delrin. lncludes Test Report and Certificate of Conformance. | 3 | |
| 99A57204387000 | AIRBUS A310 REFERENCE STANDARD PART 4 57-25-02 PAGE 405 FIGURE 404 2024-T351 or Equivalent. lncludes Test Report and Certificate of Conformance. | 3 | |
| 99A57204388000 | AIRBUS REFERENCE STANDARD A300-600 Part 6 57-21-58 Page 606 Figure 603. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57204390001 | AIRBUS REFERENCE STANDARD A300-600 PT4 57-21-30 FIGURE 405, PG. 406 . Includes Test Report and Certificate of Conformance. | 1 | |
| 99A57204391001 | AIRBUS REFERENCE STANDARD A310 Part 6 57-25-26 Page 305 Figure 604. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57204394000 | AIRBUS REFERENCE STANDARD A310 Part 4 57-25-65 Page 406 Figure 404 Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 4 | |
| 99A57204401000 | AIRBUS REFERENCE STANDARD A310 Part 4 57-25-49 Page 406 Figure 405 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 3 | |
| 99A57204402000 | AIRBUS REFERENCE STANDARD A300 PT 4 57-23-07-991-003-A . MATERIAL 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 3 | |
| 99A57204403001 | REFERENCE STANDARD - CALIBRATION BLOCK | 5 | |
| 99A57204425000 | AIRBUS REFERENCE STANDARD A300-600 57-21-25 FIGURE 402, PAGE 403 . Includes Test Report and Certificate of Conformance. | 2 | |
| 99A57204438001 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 406 FIGURE 403. Includes Test Report and certificate of Conformance. | 2 | |
| 99A57204453000 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 406 FIGURE 403. Includes Test Report and certificate of Conformance. | 1 | |
| 99A57204454000 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 407/408 FIGURE 404. Includes Test Report and certificate of Conformance. | 2 | |
| 99A57204455000 | AIRBUS A310 REFERENCE STANDARD PART4 57-29-01 PAGE 407/408 FIGURE 404. Includes Test Report and certificate of Conformance. | 2 | |
| 99A57504296000 | AIRBUS REFERENCE STANDARD A300 57-42-11, A300-600 57-51-34 and A310 57-51-11 PART PAGE 404 FIGURE 403. Includes Test Report and Certificate of Conformance. | 3 | |
| 99D34403001000 | AIRBUS REFERENCE STANDARD | 1 | |
| 99D51103001000 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, FIGURE 51-10-04-991-014-A. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D51103004000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Page 9 Figure 51-10-04-270-803-A-01. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D51103016000 | AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, FIGURE 51-10-31-991-004-A. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D51107295000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Part 6 51-10-11 Page 605 Figure 604 Material 2024-T3. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D51307001000 | AIRBUS REFERENCE STANDARD (WIFI BROADBAND) | 1 | |
| 99D51407291000 | AIRBUS REFERENCE STANDARD | 2 | |
| 99D51407291001 | AIRBUS CARBON LAMINATE THICKNESS REFERENCE STANDARD SET A318-A321 51-10-06-PB4 Multidirectional Fabric Material, BLOCKS 01-06 includes waterproof case. Nominal Thicknesses of 1mm, 3mm, 5mm, 9mm, 15mm, 19mm. Includes Test Report and Certificate of Con... | 7 | |
| 99D52041757000 | AIRBUS REFERENCE STANDARD | 1 | |
| 99D52103001000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Figure 52-13-04-991-003-A Material: 2024-T4. Includes Test Report and Certificate of Conformance. | 3 | |
| 99D52809004000 | Airbus reference standard, 52-81-06, Page6 | 7 | |
| 99D53003001108 | AIRBUS REFERENCE STANDARD | 1 | |
| 99D53103000000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Part 4 53-11-04 Page 404 Figure 404 Material: 2024. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D53103001000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Part 4 53-11-82 Page 404 Figure 403 Material: 7010-T7451. Oncludes Test Report and Certificate of Conformance. | 2 | |
| 99D53103002000 | AIRBUS Reference standard A318/319/320/321 NTM 57-11-85, Part 4 Page 405/405A, Figure 403. Includes Test Report and Certificate of Conformance... | 1 | |
| 99D53203000002 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 6 53-21-86 Page 604A/604B Figure 603 Material: 2024. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D53203001000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 53-00-13-PB6 Page 6 Figure 53-00-13-991-003-A Sheet 1 Material 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D53207304000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 6 53-41-45 Page 607/608 Figure 604 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D53409001000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 6 53-41-37 Page 605 Figure 602 Material: 2024 and 7075, Fasteners: NAS1097D5-6. Includes Test Report and Certificate of Conformance... | 5 | |
| 99D54403000004 | AIRBUS REFERENCE STANDARD A320 PT4 54-51-02-PB4:PG12..FIG54-51-02-991-004-A SHEET01. Includes Test Report and Certificate of Conformance. | 7 | |
| 99D54403001000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Part 6 54-51-01 Page 606 Figure 604 Material 35NCD16. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 4 | |
| 99D54403002000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 54-51-23 Page 407 Figure 406 Material TA6V. Includes Test Report and Certificate of Conformance. | 4 | |
| 99D54403003000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 54-51-23 Page 407 Figure 407 Material TA6V. Includes Test Report and Certificate of Conformance. | 4 | |
| 99D54403004000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 54-51-15 Page 405 Figure 404 Material 35NCD16. Includes Test Report and Certificate of Conformance. | 6 | |
| 99D54403005000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 54-51-15 Page 406 Figure 405. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 3 | |
| 99D57004001001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 51-63-03-PB1 Page 4 Figure 51-63-03-991-002-A Sheet 1 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57004001002 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 51-63-03-PB1 Page 5 Figure 51-63-03-991-002-A Sheet 1 Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57103002001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-11-85-PB4 Page 13 Figure 57-11-85-991-003-A Sheet 1 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D57103004000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-11-81 Page 406 Figure 403 Material: 7175T73. Includes Test Report and Certificate of Conformance. | 4 | |
| 99D57103005001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-11-83 Page 405 Figure 403 Material: 7175T73. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D57103006000 | AIRBUS REFERENCE STANDARD PT 4 57-11-83. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D57103007000 | AIRBUS REFERENCE STANDARD , A318/A319/A320/A321 Part 4 57-11-81 Page 417 Figure 408. Material: 7175T73. Includes Test Report and Certificate of Conformance. | 3 | |
| 99D57103008000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-11-82 Page 422 Figure 408 Material 7175T73. Includes Test Report and Certificate of Conformance. | 6 | |
| 99D57103009000 | AIRBUS REFERENCE STANDARD. MATERIAL: 7175-T7 ALUMINUM ANODIZED. PAINT WITH PRIMER | 4 | |
| 99D57103010000 | AIRBUS REFERENCE STANDARD 57-11-82 PT 4 FIG 403. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D57103011000 | Airbus Reference Standard w/Certs | 5 | |
| 99D57103012000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-82. Includes Test Report and Certificate of Conformance. | 6 | |
| 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. | 6 | |
| 99D57103014000 | AIRBUS REFERENCE STANDARD W/CERTS | 5 | |
| 99D57103015000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-47 FIG 412. Includes Test Report and Certificate of Conformance. | 4 | |
| 99D57103016000 | AIRBUS REFERENCE STANDARD A318-A321 PT 4 57-11-47 FIG 417. Includes Test Report and Certificate of Conformance. | 7 | |
| 99D57103017000 | Airbus Reference Standard | 5 | |
| 99D57103018000 | Airbus Reference Standard | 4 | |
| 99D57103019000 | Airbus Reference Standard | 4 | |
| 99D57103020000 | Airbus Reference Standard w/certs | 3 | |
| 99D57103021000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-11-47 Page 421 Figure 411 Material 7075-T7. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D57103023000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-12-04-PB4 Page 47 Figure 57-12-04-991-013-A Sheet 1. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57103024000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-12-04-PB4 Page 11 Figure 57-12-04-991-003-A Sheet 1. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57103027000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-12-03-PB4 Page 73 Figure 57-12-03-991-015-A Sheet1 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57103028000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-12-03-PB4 Page 99 Figure 57-12-03-991-020-A Sheet 1 Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57103032000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-82-991-003-A SHEET 01 PG.6. Includes Test Report and certificate of Conformance. | 2 | |
| 99D57103033000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-82-991-008-A PAGE 406 MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and certificate of Conformance. | 2 | |
| 99D57103034000 | REFERENCE STANDARD AIRBUS | 2 | |
| 99D57103035000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-81-991-003-A PAGE 1. Includes Test Report and certificate of Conformance. | 2 | |
| 99D57103036000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD PART4 57-11-47-991-003-A . Material: 7075 Aluminum Includes Test Report and certificate of Conformance. | 2 | |
| 99D57204105000 | Reference Standard, A320 PT4 57-26-54-PB4:PG12 - CAA + PRIMER | 5 | |
| 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. | 6 | |
| 99D57204125000 | AIRBUS REFERENCE STANDARD A318/319/320/321 Part 4 57-29-04 PAGE 405 FIGURE 403. Material: 2014-T652. Includes Test Report and Certificate of Conformance. | 5 | |
| 99D57204164000 | Airbus Reference Standard, A320 NTM 57-29-07-PB4:PG17 FIG 57-29-07-991-003-A - CAA, PRIMER, TOPCOAT | 4 | |
| 99D57204164001 | Airbus Reference Standard, A320 NTM 57-29-07-PB4:PG18 FIG 57-29-07-991-003-A SHEET 01- CAA, PRIMER, TOPCOAT | 4 | |
| 99D57204169000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.9. MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includest Certification and COC. | 3 | |
| 99D57204169001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.9. MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includest Certification and COC. | 1 | |
| 99D57204170000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11. MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includest Certification and COC. | 3 | |
| 99D57204170001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11. Includes Test Report and Certificate of Conformance | 1 | |
| 99D57204171000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-29-09-PB4 Page 12 Figure 57-29-09-991-003-A Sheet 1. Material: 2014-T652. Includes Test Report and Certificate of Conformance. | 2 | |
| 99D57204175000 | AIRBUS REFERENCE STANDARD A318-A321, 57-29-13-003-A | 4 | |
| 99D57204175000/S | AIRBUS REFERENCE STANDARD A318-A321, 57-29-13-003-A, 4340 | 1 | |
| 99D57204186000 | AIRBUS REFERENCE STANDARD Part 4 57-20-54 Figure 57-20-54-991-018-A. Material:2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99D57204196000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11. MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57204197000 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 57-29-11-PB6 PG.11. MATERIAL: ABM3-1031(7150-T6 AL), ABM3-1029(7050-T7 AL). Includes Test Report and Certificate of Conformance. Note: Repair Plate = .236" | 1 | |
| 99D57504100000 | AIRBUS REFERENCE STANDARD INBOARD LUG A318/A319/A320/A321 PART 4: 57-52-50 FIGURE 403 PAGE 404 Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 2 | |
| 99D57504102000 | AIRBUS REFERENCE STANDARD OUTBOARD LUG A318/A319/A320/A321 PART 4: 57-52-50 FIGURE 403 PAGE 404 Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 4 | |
| 99D57504103001 | AIRBUS REFERENCE STANDARD A318/A319/A320/A321 Part 4 57-51-01 Page 405 Figure 403. Material 2024. Includes Test Report and Certificate of Conformance. | 3 | |
| 99D57504107000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD INBOARD LUG 2024-T351 ALUMINUM. PART 4: 57-53-50 FIGURE 403 PAGE 404. Includes Test Report and Certificate of Conformance. | 2 | |
| 99D57504108000 | AIRBUS A318/A319/A320/A321 REFERENCE STANDARD OUTBOARD LUG 2024-T351 ALUMINUM. PART 4: 57-53-50 FIGURE 404 PAGE 405. Includes Test Report and Certificate of Conformance. | 2 | |
| 99D57504109000 | AIRBUS REFERENCE STANDARD | 3 | |
| 99D57704100000 | AIRBUS REFERENCE STANDARD A318/319/320/321 57-70-06, PG. 404, FIGURE 402. Includes Test Report and Certificate of Conformance. | 2 | |
| 99D7204125000 | Airbus/FIL/EDSWNU/0824Reference Standard | 1 | |
| 99F53103000000 | AIRBUS REFERENCE STANDARD A300 SERIES Part 6 53-12-25 Page 605/606 Figure 603 Material: 2024 or Equivalent. Annodize per(13-002) Primer(16-006) top coat(16-008) sealant(09-002) | 3 | |
| 99F53103003000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-11-65-PB4 Page 9 Figure 53-11-65-991-00-A Sheet 1. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53103004000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 53-11-08-991-004-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53103005000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 53-11-09-991-003-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53103006000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 53-11-48-991-004-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53103007000 | AIRBUS REFERENCE STANDARD A330, FIGURE 53-11-82-991-003-A MATERIAL: 2024. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53103009000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-11-08-009-A. MATERIAL: 2024 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53103010000 | AIRBUS REFERENCE STANDARD A330 53-11-79-991-003-A PB4. MATERIAL: 2024-T3 ALUMINUM. lncludes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 99F53207310000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-21-56-PB6 Page 12 Figure 53-21-56-991-004-A Sheet 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F53207313000 | AIRBUS REFERENCE STANDARD A330 53-21-36 FIG 619. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F53303005000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-31-09 Page 607/608 Figure 603. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303008000 | AIRBUS REFERENCE STANDARD A330 PT 4 53-31-07 FIGURE 403 PAGE 407/408, MATERIAL 7075 ALUMINUM. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53303008001 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-07 Figure 53-31-07-991-005-A Material: 7075 or Equivalent. lncludes Test Report and Certificate of Conformance. | 2 | |
| 99F53303009000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-30-10-PB6 Page 12 Figure 53-30-10-991-004-A Sheet 1. Material: 2024-T3. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53303010000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-14 Page 405 Figure 403. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303011000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-56 Page 405 Figure 403. Material: 7175-T7351. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303012000 | AIRBUS REFERENCE STANDARD A330 Figure 53-31-61-991-010-A. Material: 7175-T7351. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303013000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-61 Page 404 Figure 403. Material: 7475-T7351. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303015000 | AIRBUS REFERENCE STANDARD A340-200/-300 53-31-13-PB4. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303017000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-11-84-PB6 Page 7 Figure 53-11-84-991-003-A Sheet 1, Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F53303018000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-11-88 Page 607/608 Figure 604. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F53303019000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-11-30 Page 404 Figure 403. Material: 7175-T7351. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F53303020000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-11-44 Page 404 Figure 403. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F53303021000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-11-44 page 412 Figure 408. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F53303023000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-30-16 Page 607/608 Figure 603. Material: 2024-T3 Bare and Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303026000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-30-18-PB6 Page 10 Figure 53-30-18-991-003-A Sheet1. Material: 2024-T3 Bare and Clad. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53303027000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-30-18-PB6 Page 11 Figure 53-30-18-991-004-A Sheet 1. Material: 2024-T3 Bare and Clad. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53303029000 | AIRBUS REFERENCE STANDARD A330 53-31-45-991-003-A, Material: 2024 or Equivalent, Fasteners: ASNA-2391-3 + ASNA-2025-3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303030000 | AIRBUS REFERENCE STANDARD A330 Part 6 53-30-19 Page 605/606 Figure 603. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303080000 | AIRBUS REFERENCE STANDARD A340-500/600 FIGURE 403. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303085000 | AIRBUS REFERENCE STANDARD A330 Part 4 Figure 53-31-62-991-013-A. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303086000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-87-PB4 Page 14 Figure 53-31-87-991-004-A Sheet1. Material: 2024 or Equivalent. lncludes Test Report and Certificate of Conformance. | 5 | |
| 99F53303087000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-87 Page 422 Figure 408, Material: 2024-T3. lncludes Test Report and Certificate of Conformance. | 4 | |
| 99F53303088000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-11 PB4 Page 31 Figure 53-31-11-991-010-A Sheet 1, Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303090000 | AIRBUS REFERENCE STANDARD A340-200/-300 53-31-12-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303091000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-12-PB4 Page 10 Figure 53-31-12-991-015-B Sheet1, Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303092000 | AIRBUS REFERENCE STANDARD Figure 53-31-96-991-003-A. Material: 2024-R3 or Equivalent. Includes Test Report and Certificate of Conformance | 1 | |
| 99F53303094000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-30-22-PB4 Page 10 Figure 53-30-22-991-003-A Sheet 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303095000 | AIRBUS REFERENCE STANDARD A340-200/-300 53-30-24-PB4 FASTENER (ASNA2391). Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303096000 | AIRBUS REFERENCE STANDARD A330/A340-200/-300 53-30-29-PB4. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303097000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-70-PB4 Page 6 Figure 57-11-70-991-009-A Sheet 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303098000 | AIRBUS A340 REFERENCE STANDARD | 1 | |
| 99F53303099000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-30-42 Figure 53-30-42-991-003-A, Page 9, Material: 2024 or Equivalent. lncludes Test Report and Certificate of Conformance. | 3 | |
| 99F53303103000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-31-89-PB4 Page 10 Figure 53-31-89-991-009-A Sheet 1. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303104000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-30-65 Figure 53-30-65-991-008-A. Material: 2024. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303107000 | AIRBUS REFERENCE STANDARD A340-500/-600 53-39-08-22-23. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303108000 | AIRBUS REFERENCE STANDARDS A340-500/-600 53-39-08-22-23. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303109000 | AIRBUS REFERENCE STANDARD A340-500/-600 53-39-19-270-801-A-01. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 99F53303115000 | AIRBUS REFERENCE STANDARD A330 | 3 | |
| 99F53303118000 | AIRBUS REFERENCE STANDARD A330-A340/200-300 Part 4 53-30-23 Page 407 Figure 403 Sheet 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 1 | |
| 99F53303119001 | AIRBUS A330 REFERENCE STANDARD PART 4 53-30-70 PAGE 9. MATERIAL: 7050 or EQUIVALENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53303121000 | AIRBUS A330 REFERENCE STANDARD PART 4 53-30-71-991-004-A SHEET 1, 7175-T7351 ALUMINUM. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F53303125000 | ARIBUS REFERENCE STANDARD A330 Part 6 53-30-72 Figure 53-30-72-991-012-A. Material: 2024-T3 and 7075-T7. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F53303127000 | AIRBUS REFERENCE STANDARD Part 4 53-30-09 Figure 53-30-09-991-015-A. Material: 2024-T4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F53307305001 | AIRBUS REFERENCE STANDARD A330 51-31-80 PB6 PAGE 12. A340 53-31-81 PB6 PAGES 609-610. Includes Certification Report traceable to NIST and Certificate of Conformance. | 5 | |
| 99F53507256000 | AIRBUS REFERENCE STANDARD A330 Part 4 53-51-09-PB4 Page 12 Figure 53-51-09-991-004-A Sheet 1. Material: 7075-T7. lncludes Test Report and Certificate of Conformance. | 2 | |
| 99F54403000001 | AIRBUS REFERENCE STANDARD A330 Part 4 54-51-38 Page 404 Figure 403. Material: 40CDV12. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F54403001001 | AIRBUS REFERENCE STANDARD A330 Part 4 54-51-39 Page 404 Figure 403 Material: 40CDV12. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F54403002001 | AIRBUS REFERENCE STANDARD A330 Part 4 54-51-40 Page 405/406 Figure 403 Material: E-40CDV12. Includes Test Report and Certificate of Conformance. | 5 | |
| 99F54403002002 | AIRBUS REFERENCE STANDARD A330 54-51-40-991-008-A Page 15. Material 15-5PH. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F54503000000 | AIRBUS REFERENCE STANDARD A330 54-51-04 Page 1 Figure 54-51-04-991-020-A. Material: 13-8. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F54503009000 | AIRBUS REFERENCE STANDARD A330 54-51-40-PB4 PAGE 46 FIGURE 54-51-40-991-014-A SHEET 01. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F54503010000 | AIRBUS REFERENCE STANDARD A330 FIGURE 54-51-40-991-019-A .FASTENER (NAS5415-36). Includes Test Report and Certificate of Conformance. | 2 | |
| 99F54503011000 | AIRBUS REFERENCE STANDARD A330 54-51-40-PB4. MATERIAL 15-5PH STEEL. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F54503012000 | AIRBUS REFERENCE STANDARD A330 Part 6 54-51-04-PB6 Page 28 Figure 54-51-04-991-061-A Sheet 1. Material: 40CDV12. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F54503015000 | AIRBUS REFERENCE STANDARD A330 54-54-19-991-003-A. MATERIAL: TA6V TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F55109001000 | AIRBUS REFERENCE STANDARD A330 PT 4 55-10-09. Includes Test Report and Certificate of Conformance | 2 | |
| 99F57004100001 | AIRBUS REFERENCE STANDARD A340-500/-600 57-00-11-PB4. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57004101001 | AIRBUS REFERENCE STANDARD A330 57-00-11 FIG 403. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57103006000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-48. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103007000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-44. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57103008000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-11-07. PAGE 404 FIGURE 403. Includes test Report and Certificate of Conformance(COC). | 2 | |
| 99F57103009000 | AIRBUS REFERENCE STANDARD A340-200/*-300 57-11-38-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103010000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-52 Page 415 Figure 408. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57103011000 | AIRBUS REFERENCE STANDARD 330 57-11-00-200-822A A340-200/-300 57-11-52-PB4. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57103012001 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-22. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103016001 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-46 Page 411/412 Figure 403. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103017000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-59 Page 404 Figure 403. Material: 2024. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57103018000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-45 Page 409/410 Figure 403. Material: 7175-T7. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57103019000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-25 Page 404 Figure 403. Material: 2024 or equivalent. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57103026000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-11-62-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103028000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-11-63-PB4. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57103029000 | Airbus A330 Reference Standard, PT4, 57-11-57, PG13 | 1 | |
| 99F57103030000 | Airbus A330 Reference Standard, PT4, 57-11-58, PG11 | 1 | |
| 99F57103031000 | AIRBUS REFERENCE STANDARD Figure 57-11-10-991-033-A. Includes Test Report and Certificate of Conformance | 2 | |
| 99F57103032000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-11-22 Page7 Figure 57-11-22-991-003-A. Material: Aluminum Alloy. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57103040000 | AIRBUS REFERENCE STANDARD A340 part 4 57-18-12 Figure 57-18-12-991-003-A. Material: 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 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) | 2 | |
| 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) | 2 | |
| 99F57103046000 | AIRBUS REFERENCE STANDARD A340 57-18-11-991-036-A FASTENER (EN6115V6-11 + NSA5050-6). Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103048000 | AIRBUS REFERENCE STANDARD A340-200/300 57-11-63-PB4 FASTENER (NSA5359-6-8 + NSA5050-6). Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57103051000 | AIRBUS REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. APPLY TOP COAT 16-008 | 1 | |
| 99F57103052000 | AIRBUS REFERENCE STANDARD 57-11-71-PB4 Figure 57-11-71-991-005-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103054000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-20-96 Figure 57-20-96-991-003-A. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57103056000 | AIRBUS REFERENCE STANDARD A340-500/600 57-18-25-991-004-A . Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103057000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-11-79-991-003-A. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57103059000 | AIRBUS REFERENCE STANDARD 57-11-68-991-007-A. MATERIAL: 7175 or 7075 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57203000000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-20-84 Page 409 Figure 403. Material: 7175-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57203001000 | AIRBUS A340 REFERENCE STANDARD FIGURE 57-20-84-991-008-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57203002000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-20-86-991-003-A. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204102000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-20-16-PB4. Includes Test Report and Certificate of Conformance. | 7 | |
| 99F57204105000 | AIRBUS REFERENCE STANDARD Part 4 57-20-49 Figure 57-20-49-991-006-A. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57204106000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-20-52 Page 424 Figure 413 Material: 2024. lncludes Test Report and Certificate of Conformance. | 4 | |
| 99F57204108000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-10-PB4 Page 12 Figure 57-26-10-991-003-A Sheet 1. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57204109001 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-10 Page 405 Figure 404. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57204110000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-11-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204111000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-11-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204114000 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-10 PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204115000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-10. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204120000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-26-12 Page 404 Figure 403. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57204124000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-08. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57204124001 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-08-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204128000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-09. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204128001 | AIRBUS REFERENCE STANDARD A340-200/-300 57-26-09-PB4. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204130000 | AIRBUS REFERENCE STANDARD A330 57-20-47 FIG 405. Includes Certification Report and Certificate of Conformance. | 4 | |
| 99F57204134000 | AIRBUS REFERENCE STANDARD A340 PT 4 57-26-08. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204135000 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403 SHEET 1 PAGE 407. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57204136000 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403 SHEET 1 PAGE 407. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57204137000 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57204138001 | AIRBUS REFERENCE STANDARD A330 57-20-52 FIG 403. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57204140000 | AIRBUS REFERENCE STANDARD A330 Part 6 57-20-02 Page 604 Figure 603. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57204144000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-20-93 page 405 Figure 403. Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57204145000 | AIRBUS REFERENCE STANDARD A330 57-20-15 FIG 402 Includes Certification Report and Certificate of Conformance. | 4 | |
| 99F57204146000 | AIRBUS REFERENCE STANDARD A330 57-20-49 FIG 403 SHEET 1 PAGE 406. Includes Test Report and Certificate of Conformance. | 4 | |
| 99F57204171000 | AIRBUS REFERENCE STANDARD A340-500/-600 57-26-59-PB6. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204172000 | AIRBUS NDT REFERENCE STANDARD | 2 | |
| 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. | 3 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| 99F57244001000 | AIRBUS A330 REFERENCE STANDARD PART 4 57-24-04-991-010-A SHEET 1, 2024-T351 ALUMINUM. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99F576030004000 | Airbus Reference Standard | 1 | |
| 99F57603001000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-61-16 page 404 Figure 403. Material: 7175-T7351. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57603002000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-61-06 Page 404 Figure 403. Material: Aluminum Alloy. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57603004000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-61-14-PB4 Page 6 Figure 57-61-14-991-003-A Sheet 1. Material: 2024. Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57603005000 | AIRBUS REFERENCE STANDARD A330 Part 4 57-61-14-PB4 Page 17 Figure 57-61-14-991-008-A Sheet1. Material: 2024. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57603006000 | AIRBUS REFERENCE STANDARD A330-200F PT 4 57-61-21-991-003-A PAGE 1. Material 2024 Aluminum. lncludes Test Report and Certificate of Conformance. | 1 | |
| 99L52103000000 | AIRBUS REFERENCE STANDARD A380 52-81-01-991-012-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L52107325000 | AIRBUS REFERENCE STANDARD A380 52-11-01-01. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 99L53303000000 | AIRBUS REFERENCE STANDARD A380 53-31-37-991-006-A. Material: 2024-T3 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303001000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-36-991--003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303003000 | AIRBUS REFERENCE STANDARD A380-800 53-31-22-991-009-A (SHEET 02). Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303004000 | AIRBUS REFERENCE STANDARD A380-800 53-31-22-991-009-A (SHEET 03). Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303005000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-21-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303008000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-19-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303019000 | AIRBUS A380 REFERENCE STANDARD FIGURE 53-31-11-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303024000 | AIRBUS REFERENCE STANDARD A380-800 53-31-22-991-009-A (SHEET 01). Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303027000 | AIRBUS REFERENCE STANDARD A380-800 53-31-37-991-013A. MATERIAL: 7475 OR EQUIVALENT 7050 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303030000 | AIRBUS REFERENCE STANDARD A380-800 53-31-62-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303031000 | AIRBUS REFERENCE STANDARD A380-800 53-31-60-991-015-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303033000 | AIRBUS REFERENCE STANDARD A380-800 53-31-63-991-003-A. MATERIAL: 7175-T73 OR EQUIVALENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303035000 | AIRBUS REFERENCE STANDARD A380 53-31-27-991-021-A PAGE 23. MATERIAL: 7175 OR 7075 ALUMINUM. Includes Certificate of Conformance. | 1 | |
| 99L53303037000 | AIRBUS REFERENCE STANDARD A380 53-31-27-991-020-A PAGE 22. MATERIAL: TEFLON. Includes Certificate of Conformance. | 1 | |
| 99L53509001000 | AIRBUS A380 REFERENCE STANDARD 7050-T7 OR 2024 ALUMINUM; FIGURE:53-51-02-991-008-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53509002000 | AIRBUS REFERENCE STANDARD A380-800 53-51-36-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53509003000 | AIRBUS REFERENCE STANDARD A380-800 53-51-08-991-004-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53509006000 | AIRBUS REFERENCE STANDARD A380-800 53-51-37-270-801-A-01. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53509008000 | AIRBUS A380-800 REFERENCE STANDARD TITANIUM 6AL 4V; FIGURE:53-51-58-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L54503000000 | AIRBUS A380 REFERENCE STANDARD FIGURE:54-51-04-991-012-A. MATERIA L: 600/700 SERIES INCONEL. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L54503003000 | AIRBUS A380 REFERENCE STANDARD 7050-T7 OR 2024 ALUMINUM; FIGURE:54-51-06-991-010-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L54503005000 | AIRBUS REFERENCE STANDARD A380-800 54-51-03-991-004-A. MATERIAL: TA6V B Includes Test Report and Certificate of Conformance. | 1 | |
| 99L54503006000 | AIRBUS REFERENCE STANDARD A380-800 54-52-02-991-022-A, MATERIAL:TA6VB Includes Test Report and Certificate of Conformance. | 1 | |
| 99L55209001000 | AIRBUS REFERENCE STANDARD 55-21-03-991-003-1. 7050-T7451 ALUMINUM | 1 | |
| 99L57203000000 | AIRBUS REFERENCE STANDARD A380 FIGURE 57-21-10-991-003-A. MATERIAL: 7175 OR EQUIVALENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L57203001000 | AIRBUS REFERENCE STANDARD A380 FIGURE 57-21-10-991-009-A. MATERIAL: 7175 OR EQUIVALENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L57203002000 | AIRBIS REFERENCE STANDARD A380-800, 57-21-05. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L57203003000 | AIRBUS A380 REFERENCE STANDARD FIGURE 57-21-02-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L57203006000 | AIRBUS REFERENCE STANDARD A380-800 7075 ALUMINUM; FIG.57-21-10-991-016-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 99L57603000000 | AIRBUS REFERENCE STANDARD A330-200F 57-61-21-991-006-A PAGE 1. . lncludes Certificate of Conformance. | 1 | |
| 99N28207315000 | AIRBUS REFERENCE STANDARD A318-A321 28-28-03-PB6. Includes Test Report and Certificate of Conformance. | 4 | |
| 99N51107332000 | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT BLOCK SET. Includes Test Report and Certificate of Conformance. | 2 | |
| 99N51107332000-A | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99N51107332000-B | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99N51107332000-C | AIRBUS REFERENCE STANDARD A380-800 51-10-30-991-003-A FOR CLADDING MEASUREMENT. Includes Test Report and Certificate of Conformance. | 1 | |
| 99N51109009000 | CALIBRATION REFERENCE STANDARD (CRS) | 2 | |
| 99N51109010000 | CALIBRATION REFERENCE STANDARD (CRS) | 2 | |
| 99PNF54503009000 | AIRBUS REFERENCE STANDARD A330 54-51-40-991-014-A FASTENER (NSA5415-36). lncludes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 99V52307336000 | AIRBUS REFERENCE STANDARD A380 52-31-01 FIGURE 5-52-31-01-005-A.MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| A266 | Boeing Reference Standard, 727 57-50-27:FIG1 | 1 | |
| A27288 | Eddy Current Inspection Reference standard SB DC9-27A235 R03 | 3 | |
| A305 | BOEING REFERENCE STANDARD PART 6 57-30-03 pg. 3 Fig 1 & 57-10-18. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| A306 | BOEING REFERENCE STANDARD 737 PART 6 57-10-07 FIGURE 1 PAGE 4. | 1 | |
| A352 | BOEING REFERENCE STANDARD 737 PART 6 53-10-04 PAGE 4 FIGURE 1. 2024-T3 CLAD ALUMINUM OR 7075-T6 BARE. Includes Test Report and Certificate of Conformance. | 11 | |
| A376 | BOEING REFERENCE STANDARD 737 PT 6 53-10-45 | 1 | |
| A386 | BOEING REFERENCE STANDARD 737 PT 6 53-10-45 | 2 | |
| A389A | BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. | 3 | |
| A389B | REFERENCE STANDARD A389B | 2 | |
| A389C | BOEING REFERENCE STANDARD 737 PT 6 53-10-41 FIG 3. Includes Test Report and Certificate of Conformance. | 2 | |
| A4010 | BOEING REFERENCE STANDARD PT 6 53-10-33 FIG 2, PAGE8. Includes Test Report and Certificate of Conformance. | 1 | |
| A4024 | BOEING REFERENCE STANDARD PT PT. 6, 53-10-33 . Includes Test Report and Certificate of Conformance. | 1 | |
| A428 | BOEING REFERENCE STANDARD PT 6 53-10-15 FIG 2, PAGE11. Includes Test Report and Certificate of Conformance. | 1 | |
| A429 | BOEING REFERENCE STANDARD PT 6 53-10-15 FIG 2, PAGE11. Includes Test Report and Certificate of Conformance. | 1 | |
| A430 | BOEING REFERENCE STANDARD PT 6 53-10-15 FIG 2, PAGE11. Includes Test Report and Certificate of Conformance. | 2 | |
| A607 | Boeing Reference Standard, 767 PT6 53-80-02: PG6 FIG2 Sheet1 | 4 | |
| A607A | Boeing Reference Standard, 767 PT6 53-80-02: PG7 FIG2 Sheet2 | 3 | |
| ACRS3-172942 | CALIBRATED CONDUCTIVVITY REFERENCE STANDARD SET OF 3. KIT CONSISTS OF MAGNESIUM, 6061-T6 AL AND 2024-T3 AL ( IACS Nominal values of 17%, 29% and 42% respectively) | 1 | |
| ACWM-E175-IB | Inner Wheel Standard, Embraer..175 90000582: 1. Contains a Total of 3 EDM Flaws in the Bead Seat Area of the Reference Standard. Flaw sizes: 1.52mm Long x 0.76mm Deep x 0.10mm Wide Tolerance= +/- 0.05mm. Includes Test Report and Certificate of Confor... | 1 | |
| ACWM-E175-OB | Outer Wheel Standard, Embraer..175 90000582-1. Contains a Total of 3 EDM Flaws in the Bead Seat Area of the Reference Standard. Flaw sizes: 1.52mm Long x 0.76mm Deep x 0.10mm Wide Tolerance= +/- 0.05mm. Includes Test Report and Certificate of Conform... | 1 | |
| AF- 4120 | LOW FREQUENCY RING PROBE, 10KHZ-100KHZ, REFLECTION, .405"ID, .800"OD, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. USED WITH REFERENCE STANDARD: NDT1102-100 TI | 1 | |
| AF-4041 | LOW FREQUENCY DIFFERENTIAL PROBE , 1-40KHZ. Maximum height of .50" inches and diameter of .300" to .320" inches. Flat at the end. Used with ANDT3016-B reference standard. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4041/4F | LOW FREQUENCY DIFFERENTIAL PROBE , 1-40KHZ. Maximum height of .50" inches and diameter of .300" to .320" inches, 4 Pin Fischer Connector. Flat at the end. Used with ANDT3016-B reference standard. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4084 | LOW FREQUENCY REFLECTION RING PROBE, 800HZ-10KHZ, .320"Ø ID,.600"Ø OD x .700"H, WITH TRIAX FISCHER CONNECTOR. REFERENCE: 767 PART 6 53-10-22, NDT6075 REFERENCE STANDARD. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4092 | LOW FREQUENCT RING PROBE, 500Hz-3KHz. REFLECTION, 1.00" OD, .510" ID, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT3255 | 1 | |
| AF-4101 | LOW FREQUENCT RING PROBE, 1-10KHz. REFLECTION, .700" OD, .350" ID, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT3255 | 1 | |
| AF-4102 | LOW FREQUENCT RING PROBE, 50Hz-5KHz. REFLECTION, .700" OD, .350" ID, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT3255 | 1 | |
| AF-4109/TI | LOW FREQUENCY REFLECTION RING PROBE, ID .470, OD.900, 3-10KHZ. For reference standard NDT 3259. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4120 | LOW FREQUENCY RING PROBE, 10KHz-100KHz, REFLECTION, .405"ID, .800"OD, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. USED WITH REFERENCE STANDARD: NDT1102-100 Ti | 1 | |
| AF-4124/300H | REFLECTION RING PROBE TRIAX FISHER CONNECTOR, 1.25"OD .75" ID(19.6mm) 300HZ-1KHZ. 737 PART 6 57-10-53, pg.2, USED WITH REFERENCE STANDARD NDT3168 AND NDT3176-X. Includes test report and Certificate of Conformance. | 1 | |
| AF-4125/100H | CUSTOM REFLECTION RING PROBE 1.2" OD, .605" ID, 50Hz-3KHz TRIAX FISHER CONNECTOR. 737 PART 6 57-10-58, pg.2. and 737 PART 6 57-10-54, pg.2 USED WITH NDT3153-X AND 3167-X SERIES REFERENCE STANDARDS. Includes Test Report and Certificate of Conform... | 1 | |
| AF-4144 | LOW FREQUENCY DIFFERENTIAL PROBE , 1-40KHZ. Maximum height of .50" inches and diameter of .300" to .320" inches. 10 inches long Flat at the end. Used with ANDT3016-B reference standard. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4153/TI | LOW FREQUENCY RING PROBE 1-15KHz, REFLECTION, ID.565" OD.910",SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT 3225. | 1 | |
| AF-4202 | LOW FREQUENCY REFLECTION RING PROBE, 500HZ-5KHZ, ID 0.325", OD 0.790" (MAX). 1.05" HEIGHT. TRIAX FISCHER CONNECTOR. USED WITH NDT6097 REFERENCE STANDARD Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4334 | Low Frequency Reflection Ring Probe, 40Hz-500Hz. 1.3"Ø I.D. 2.0"Ø O.D., supplied with a Triax Fischer Connector. REFERENCE STANDARD: NDT7035. Includes test report and Certificate of Conformance. | 1 | |
| AF-4335 | LOW FREQUENCY REFLECTION RING PROBE, 300Hz-1KHz .425"Ø ID SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes test report and Certificate of Conformance.....USED WITH 717-200 REFERENCE STANDARD P/N: 717RS10-C | 1 | |
| AF-5098RS/.875 | BOEING DC9 REFERENCE STANDARD -57-225 FIG 6 | 1 | |
| AF-5272 | CUSTOM COUNTERBORE ROTARY ADJUSTABLE X STYLE PROBE WITH THE COIL LOCATED AT THE EDGE OF THE PROBE TIP, .936'-1.0" 2.0"WL, SUPPLIED WITH A 4 PIN FICHER CONNECTOR, 100 KHz-2MHz Includes Test Report and Certificate of Conformance REFERENCE STANDARD - NDT3117 | 1 | |
| AF-5278/TF | HIGH FREQUENCY SURFACE PROBE, Twin Coil Differential 50-500KHZ. 4.0" Long 0.375" Diameter with Triax Fischer connector. For use with Boeing Reference Standard 497 767 Part 6 53-00-04. IncludesTest Report and Certificate of conformance. | 1 | |
| AF-6006 | SLIDING PROBE, REFLECTION, 1-40KHZ TRIAX FISHER CONNECTOR. REFERENCE STANDARD USED ( NDT1099) 757 PT. 6, 53-30-14. Includes Certification Report and COC. | 1 | |
| 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.... | 1 | |
| AFC-169 | BOEING REFERENCE STANDARD TRANSDUCER POSITIONER TRANSDUCER POSITIONER TRANSDUCER POSITIONER CONTACT TRANSDUCER | 1 | |
| AFK-1002 | CUSTOM BRITISH AIRWAYS KIT 1. Contains one each of Boeing 1002 Reference Standard, ATPN-92-12.5FX , ATPN-93-5B, ABNC-MD6, in a waterproof storage case. Includes test reports and Certificate of Conformance. | 1 | |
| AFK-1011 | CUSTOM BRITISH AIRWAYS KIT 2. Contains one each of Boeing 1004 Reference Standard, ATPN-92-12.5FX , ATPN-93-5B, ABNC-MD6, in a waterproof storage case. Includes test reports and Certificate of Conformance. | 1 | |
| AFK-1014 | Custom Ultrasonic Kit, PART 4 53-10-13 for the WING REAR SPAR - STA 663.75 REAR SPAR BULKHEAD SIDE FRAME FITTING FAIL SAFE STRAP. Kit includes 1 of each AFM-560AT & AFS-0541 Transducers, 1 NDT3312 Reference Standard and 1 ABNC-MD6. Supplied with a waterpr | 1 | |
| AFK-1016 | CUSTOM BRITISH AIRWAYS KIT 3. Contains one each of Boeing 1005 Reference Standard, ATPN-92-12.5FX , ATPN-93-5B, ABNC-MD6, in a waterproof storage case. Includes test reports and Certificate of Conformance. | 1 | |
| AFK-1017 | Custom Eddy Current Inspection Kit. Includes the following probes, Reference Standard and cables.AUR-.125SE/1.75WL-LF, AUR-.156SE/1.75WL-LF, AUR-.187SE/1.75WL-LF, AUR-.250SE/2.0WL-LF, AUR-.312SE/2.0WL-LF, AUR-.375SE/2.0WL-LF, AUR-.437SE/2.0WL-LF, AUR-... | 1 | |
| AFK-1030 | Cusom Ultrasonic Inspection Kit for Boeing 787. Kit contents include: NDT815 reference standard. Transducer part numbers: AFS-0570-1R, AFS-0570-1L, AFS-0570-2R, AFS-0570-2L, AFS-0570-3R, AFS-0570-3L, AFS-0570-4R, AFS-0570-4L, AFS-0570-5R, AFS-0570-5L | 1 | |
| AFK-SS | PH TOOL REFERENCE STANDARD STAINLESS SPEC USAF TO 33-B-1-1 | 1 | |
| 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". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-1016-6S-TI | CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6, 51-00-02 PROCEDURE 1..... Hole Sizes: .188", .250", .313", .375" .438" .500". MATERIAL: 6AL-4V Titanium. Inc... | 1 | |
| 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... | 1 | |
| AFNDT-2008/2024-T6 | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15 ALUMINUM 2024-T6 .. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2008/C | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 CAST ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 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.. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| AFNDT-2008/SS | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 & 32-42-05 FIGURE 11 PROCEDURE 1 PAGE 15. MATERIAL: 304 STAINLESS STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2010AL | Custom McDonnell Douglas 15 bolt hole reference standard with a .060"L x .030Dx .005" max width mid-wall notch, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (.156", .172", .188", .203", .250", .266", .281", .297", .313", .328"... | 1 | |
| 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. Includes Te | 1 | |
| AFNDT-2054AL-2 | CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. WITH HOLE DIAMETERS: .125" .156", .187", .250",.375",.500". CORNER... | 1 | |
| AFNDT-2054CS-1 | CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .156",.250",.312",.375",.437",.500". CORN... | 1 | |
| AFNDT-2054CS-2 | CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .125", .156", .187" ,.250",.375", .500". ... | 1 | |
| AFNDT-2055 | CUSTOM ROTARY BLOCK REFERENCE STANDARD. 10MM, 13MM, 15MM, 17MM , 19MM, .020X.020X.004 +/-.001, ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2064/AL | SAFRAN MESSIER-BUGATTI-DOWTY ET SURFACE REFERENCE STANDARD 32-09-01 FIGURE 67,GRAPHIC-32-09-01-041-008-A01. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of conformance. | 1 | |
| AFNDT-2064/MAG | SAFRAN MESSIER-BUGATTI-DOWTY REFERENCE STANDARD 32-09-01 MAGNESIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2064/TI | SAFRAN MESSIER-BUGATTI-DOWTY REFERENCE STANDARD 32-09-01 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2070-AL | MD STACKABLE REFERENCE STANDARD, 06-20-01, .040, .050, .060, .063, .068, .071, .090, .100, .190, AL. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2071 | BOEING REFERENCE STANDARD 767 PT 4 51-00-04. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2094/6.2 | EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 6.2. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2094/7.8 | EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 7.8. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2094/8.2 | EMBRAER REFERENCE STANDARD 57-28-00 PT 2, HOLE SIZE 8.2. Includes Test Report and Certificate of Conformance. | 1 | |
| 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.. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2116 | CUSTOM EC REFERENCE STANDARD BRT189-080 REV A, STEEL 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2127 | SAFRAN MESSIER -BUGATTI-DOWTY REFERENCE STANDARD Material aluminum 7075-T6; Thickness 1/2". - Number of holes 5;- hole diameter 9/16 in, 10/16 in, 11/16 in, 12/16 in, 13/16 in; EDM notch in each hole: thru the thickness, depth and width in according with | 1 | |
| 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. Incl | 1 | |
| 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.. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2227Ti-1 | 8 Hole Calibration Standard, Hole Sizes; 1/8" 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", EDM NOTCH: .050" x .050" x .005" +0.000/-.002" BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, 737 PT 6 51-00-00 FIG 3 PROCEDURE 17, PG.8 MATERIAL(6AL-4V) TIT | 1 | |
| 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". Includes Test Report and Certifica | 1 | |
| 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... | 1 | |
| 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. | 1 | |
| AFNDT-3026AL | EDDY CURRENT SURFACE REFERENCE STANDARD Leonardo Helicopters SB No. 109EP-158. MATERIAL: 7475-T7 ALUMINUM. SIZE: 1.0" x 3.0" x .25" EDM SLOT (0.5mm DEEP) x (0.05-0.25mm WIDE) +/-.03mm. Includes Test Report and Certificate of Conformance. | 1 | |
| 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... | 1 | |
| 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... | 1 | |
| 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. | 1 | |
| 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... | 1 | |
| AFNDT-3071 | Custom designed eddy current multi-layer aircraft aluminum skin test specimen, drawing 2, sheets 1-4. reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3073 TYPE 1 | Custom designed eddy current reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3073 TYPE 2 | Custom designed eddy current reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3073 TYPE 3 | Custom designed eddy current reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3104 | The VMA.01-0-07 reference standard is ..3 ½” long x 3.0” wide x 1/4” thick...• The tapered notch on both standards is 0.080” deep at the edge of the standard and tapers to 0.000” deep...• The tapered notch has scribe marks every 0.010” deep from 0.000”... | 1 | |
| 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", ... | 1 | |
| 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... | 1 | |
| 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... | 1 | |
| 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 ... | 1 | |
| 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... | 1 | |
| 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... | 1 | |
| AFNDT-3141AL-1 | Custom McDonnell Douglas 12 bolt hole reference standard 7075-T6 Aluminum with .005" max width through EDM notch in holes #1-#6 and a .060"L x .030"D x .005" max width mid-wall notch in holes #7-12, and .030"x.030"x.005" max width corner notch in each hol | 1 | |
| AFNDT-3141AL-2 | Custom McDonnell Douglas 12 bolt hole reference standard 7075-T6 Aluminum with a .060"L x .030Dx .005" max width mid-wall notch, and .030"x.030"x.005" max width corner notch in each hole. Hole sizes (.2966, .3122", .3278", .3434", .359", ..3746", .3902", | 1 | |
| AFNDT-3151CS | 15 HOLE REFERENCE STANDARD 4130 OR 4340 CARBON STEEL, HOLE SIZES: 1/8, 5/32, 3/16, 7/32 ,1/4, 9/32, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 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 Re | 1 | |
| AFNDT-3166 | CUSTOM 2 HOLE REFERENCE STANDARD. MATERIAL: 718 INCONEL, BLOCK SIZE: .500" x 1.0" x 4.0" . HOLE SIZES: 5/16", 9/32" WITH -3( .030" x .060" x .005" W MID-WALL NOTCH ' | 1 | |
| AFNDT-3171CS | 17 HOLE REFERENCE STANDARD 4130/4340 Carbon Steel, 1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 5/8, 11/16 and 3/4 diameters. Includes 15 Thru EDM Notches .040" +/- 10% x .005" +/- .001" Wide. Includes Test Report ... | 1 | |
| AFNDT-3180 | 6 FLAT BOTTOM HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. Hole Sizes: 5/16", 3/8", 7/16", 1/2", 9/16", 5/8" .060" LONG X. 020" x DEEP x .005" WIDE +/- .001" WIDE. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3197AL | BOEING REFERENCE STANDARD 737 PT 6 51-00-00 FIGURE 3 PG.9 & 777 PT 6 51-00-02 PAGE 7-8. HOLE SIZES: 1.000", 1.250" . Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3204/4130 | 8 HOLE REFERENCE STANDARD IN 4130 CARBON STEEL; HOLE SIZES: (1/8, 5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2), WITH .020"x.020" CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3215AL | BOEING REFERENCE STANDARD. PT 6 51-0-00. 13 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 5/32", 3/16", 1/4", 7/32", 9/32" 5/16" , 11/32", 3/8" ,7/16", 1/2", 9/16", 5/8", 3/4". EACH HOLE CONTAINS A CORNER EDM NOTCH: 0.030" x 0.030" a... | 1 | |
| AFNDT-3217AL | BOEING REFERENCE STANDARD. PT 6 51-0-00. 29 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", ... | 1 | |
| AFNDT-3229AL | BOEING REFERENCE STANDARD. PT 6 51-0-00. 13 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. HOLE SIZES: 3/16", 1/4", 7/32", 9/32" 5/16" , 11/32", 3/8" ,7/16", 1/2", 9/16", 5/8", 3/4". EACH HOLE CONTAINS A CORNER EDM NOTCH: 0.030" x 0.030" and 0.02... | 1 | |
| AFNDT-3231 | Custom McDonnell Douglas Low Frequency Eddy Current reference standard, 06-20-01 Figure 9 sheets 1-4. Material: 2024-T3 or 7075-T6 Aluminum. Fasteners: (NAS1097AD6-5 & BACB30NW6K3). Includes Test Report and Certificate of Confromance. | 1 | |
| AFNDT-3235 | BOEING REFERENCE STANDARD PT 6 32-11-11. 4340M. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3264 | Custom Reference Standard for the Boeing Lead Screw inspection, equivalent to 7903385. Material: 4150 Alloy Steel, 1.5 Outside Diameter and 1.069" Inside Diameter with 3 EDM Flaws per BSS 7048 page 2 Table 1. Includes Test Report and Certificate of Confor | 1 | |
| AFNDT-3286 | 12 HOLE REFERENCE STANDARD 7075-T6 (Hole Sizes 3/8", 7/16", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 15/16", 1.0", 1-1/8",) .020"x.020" and .030"x.030" x .005"W +/-.002" CORNER EDM NOTCH PER BOEING SPECIFICATION 747 PART 6 51-00-00 PAGE 8 FIGURE 3 | 1 | |
| AFNDT-3291AL | BOMBARDIER 15 HOLE METRIC REFERENCE STANDARD. CL-215T PART 6 PAGE 8 FIGURE 5 GENERAL. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES: 4MM, 5MM, 6MM, 7MM, 8MM, 9MM, 10MM, 11MM, 12MM, 13MM, 14MM, 15MM, 16MM, 17MM, 18MM diameters. Includes 15 Thru EDM Notches 0.040 | 1 | |
| AFNDT-3291CS | BOMBARDIER 15 HOLE METRIC REFERENCE STANDARD. CL-215T PART 6 PAGE 8 FIGURE 5 GENERAL. MATERIAL: 4340 CARBON STEEL. HOLE SIZES: 4MM, 5MM, 6MM, 7MM, 8MM, 9MM, 10MM, 11MM, 12MM, 13MM, 14MM, 15MM, 16MM, 17MM, 18MM diameters. Includes 15 Thru EDM Notches 0.040 | 1 | |
| AFNDT-3292AL | CUSTOM 20 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .(1/8", 5/32",3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8",13/32" | 1 | |
| AFNDT-3303AL | SINGLE HOLE REFERENCE STANDARD 2024-T3 ALUMINUM, HOLE SIZE 3/8"( .375) EDM CORNER NOTCHES .030" x .030". BLOCK SIZE: 2.0" x 2.0" x 1/4" Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3306/MAG | EDDY CURRENT METRIC SURFACE REFERENCE STANDARD. EDM NOTCH SIZES: 0.2mm, 0.5mm &1.0mm. WIDTH = .005" +/- .002" MATERIAL: MAGNESIUM ZK60A-T5 PER ASTM-B107. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3320AL | 6 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-02 Part 6 Procedure 1 or 2. Hole Sizes: 15/32", 17/32", 9/16", 11/16", 5/8", 3/4" ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002 | 1 | |
| AFNDT-3321AL | 5 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Hole Sizes: 11.5mm, 14.4mm, 14.6mm, 17.4mm and 17.5mm. Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .0 | 1 | |
| AFNDT-3329ST | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(. | 1 | |
| AFNDT-3329TI | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(. | 1 | |
| AFNDT-3347CS | EDDY CURRENT WELD SURFACE REFERENCE STANDARD. EDM NOTCHES: 0.5mm, 1.0mm, 2.0mm (.1mm (.004") WIDE ± .05mm( .002") MAX WIDTH .152mm (.006"). MATERIAL: 4340 CARBON STEEL. SIZE: 1.0"W x 4.0"L Includeds 4 piece .020" thick shim and Key Ring set. Includes Tes | 1 | |
| AFNDT-3390AL | CUSTOM 10 HOLE FLAT BOTTOM REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .218", .250", 312", .375" .437" .500",.562", .625", | 1 | |
| AFNDT-3391AL | CUSTOM 10 HOLE FLAT BOTTOM HOLE REFERENCE STANDARD ASSEMBLY PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .875", 1.00", 1.125", 1.250" 1.375", 1.500", | 1 | |
| AFNDT-3396CS | SURFACE NOTCH REFERENCE STANDARD 4130 or 4340 CARBON STEEL. EDM NOTCH SIZE: FULL WIDTH OF PART x .51mm(.020") DEEP +/- .05mm(.002"). BLOCK SIZE: 1.0" WIDE x 3.0" LONG. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3405AL | CUSTOM 15 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(. | 1 | |
| AFNDT-3456AL | CUSTOM 19 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00 Procedure16 Figure 3 , 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. Total of 19 Hole Sizes: .128", .159", .189", .2 | 1 | |
| AFNDT-3457 | EDDY CURRENT SURFACE REFERENCE STANDARD. Cadmium plated on one side to AMS-QQ-P-416-f Type 1, Class 2. 3 EDM FLAWS ON BOTH SIDES. ONE SIDE UNPLATED(BARE). NOTCH DEPTHS : .008", .020", .040". NOTCH WIDTH: (.004"W +/- .002). MATERIAL: 4340 STEEL. SIZE: 1. | 1 | |
| AFNDT-3470/17-4 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCH .020"(0.5mm), (.004"W +/- .002), 17-4PH STEEL. SIZE: 1.0"W x 3.0"L x .25".Includes certification Report Traceable to NIST and Certificate of Conformance(COC). | 1 | |
| AFNDT-3476CS | CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION..737 PART 6 51-00-00 FIG.3 PG. 8, 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance..... Hole Sizes: .188", .250", .313", .3... | 1 | |
| AFNDT-3499 | EDDY CURRENT SURFACE REFERENCE STANDARD. Low Hydrogen Embrittlement Cadmium-Titaniium Alloy Plating per BAC5804. 4 EDM FLAWS ON BOTH SIDES. ONE SIDE UNPLATED(BARE). NOTCH DEPTHS : .005", .010", .020", .050". NOTCH WIDTH: (.007" +/- .002"). MATERIAL: 4... | 1 | |
| AFNDT-3504TI | 12 HOLE REFERENCE STANDARD MANUFACTURED TO SPECIFICATION USAF T.O. 33-B-1-1. MATERIAL: 6AL-4V TITANIUM. HOLE SIZES: 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/ 16" 5/8", 3/4" 0.020" x 0.004" +/-.001" Wide thru EDM NOTCHES. 4 tot... | 1 | |
| AFNDT-3507 | Custom 2 hole BOEING REFERENCE STANDARD MANUFACTURED PER 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. ....HOLE SIZES: 0.344" (11/32''),0.562"... | 1 | |
| AFNDT-3513AL | SAFRAN MESSIER -BUGATTI-DOWTY REFERENCE STANDARD Material aluminum 7075-T6; Thickness 1/2"...- Number of holes 11;..- hole diameters: 14.0mm, 14.2mm, 14.4mm, 14.6mm, 15.6mm, 15.8mm, 16.1mm, 16.2mm, 16.3mm, 16.6mm, 16.9mm...EDM notch in each hole: thru ... | 1 | |
| AFNDT-3524CS | 4 HOLE REFERENCE STANDARD. Material: 4130 or 4340 Carbon Steel 10" x 3.5" x .375" , HOLE SIZES: 1.25", 1.50", 1.75", 2.00". EDM NOTCH: .030" x .030" x .005 ± .001" CORNER NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3531/2014-T6 | 13 HOLE REFERENCE STANDARD, 2014-T6 Aluminum. 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", 3/4", MId-Wall EDM Notch = .060"L x .030D x .004" ± .001". Manufactured in accordance to Aircraft Braking System... | 1 | |
| AFNDT-3551CS | 7 HOLE REFERENCE STANDARD in 4340 Steel; Hole Sizes: .875", 1.000", 1.100", 1.200", 1.300", 1.400", 1.500"), With a .030" x .030" x .004" ± .001" Corner EDM Notch in top and bottom of each hole in the top plate. 14 Notches Total. Includes Engraving, ... | 1 | |
| AFNDT-3559AL-3 | 15 HOLE REFERENCE STANDARD, Material: 7075-T6 Aluminum. Hole Sizes: 1/8, 3/16, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 11/16, 3/4, 13/16, 7/8, 15/16, 1.0. A Total 15 Mid-bore notch @ 0.030" deep x 0.004" wide x 0.060" long in each hole. 3 Surface EDM No... | 1 | |
| AFNDT-3560A | Corrosion Reference Standard used for verifying function of low frequency corrosion probes. It is 0.100” thick with simulated 5%, 10% and 20% material loss. Overall size: 7.50” x 3.50” (190 x 89 mm). Material: 2024-T3 Aluminum. Includes Certification. | 1 | |
| AFNDT-3560B | Corrosion Reference Standard used for verifying function of low frequency corrosion probes. It is 0.100” thick with simulated 5%, 10% and 20% material loss. Overall size: 7.50” x 3.50” (190 x 89 mm). Material: 7075-T6 Aluminum. Includes Certification. | 1 | |
| AFNDT-3669-1043 | BOEING COUNTERSINK REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER 100° COUNTERSINK HOLE. MATERIAL: 43404340M STEEL. SIZE: 2.0" X .375" THICK( ROUNDSQUARE. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 1 | |
| AFNDT-VL769-1A | TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(.800"THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES) | 1 | |
| AFNDT-VL769-2A | TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(1.500" THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES) | 1 | |
| AFNDT1016-12S-2024 | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", . | 1 | |
| AFNDT1016-12S-7075 | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .6 | 1 | |
| AFS-0507 | 5MHZ 32° SHEARWAVE IN ALUMINUM. CASE SIZE .50"X.80"L. HEIGHT TAPERS FROM .20"H FRONT TO .32" H BACK. REFERENCE STANDARD IS NDT624 | 1 | |
| AFS-0570-1L | CUSTOM ANGLE BEAM TRANSDUCER (LEFT) FOR ( .328" )DIAMETER FASTENER HOLE'S (0.430" ) STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-1R | CUSTOM ANGLE BEAM TRANSDUCER (RIGHT) FOR ( .328" )DIAMETER FASTENER HOLE'S (0.430" ) STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-2L | CUSTOM ANGLE BEAM TRANSDUCER (LEFT) FOR (0.438" & 0.500") DIAMETER FASTENER HOLE'S (0.430" & 0.590") STEPS OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-2R | CUSTOM ANGLE BEAM TRANSDUCER (RIGHT) FOR (0.438" & 0.500") DIAMETER FASTENER HOLE'S (0.430" & 0.590") STEPS OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-3L | CUSTOM ANGLE BEAM TRANSDUCER (LEFT) FOR (0.642") DIAMETER FASTENER HOLE IN (0.570") STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-3R | CUSTOM ANGLE BEAM TRANSDUCER (RIGHT) FOR (0.642") DIAMETER FASTENER HOLE IN (0.570") STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-4L | CUSTOM ANGLE BEAM TRANSDUCER (LEFT) FOR (0.438") DIAMETER FASTENER HOLE (0.710") STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-4R | CUSTOM ANGLE BEAM TRANSDUCER (RIGHT) FOR (0.438") DIAMETER FASTENER HOLE (0.710") STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-5L | CUSTOM ANGLE BEAM TRANSDUCER (LEFT) FOR (0.625") DIAMETER FASTENER HOLE IN (0.850") STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0570-5R | CUSTOM ANGLE BEAM TRANSDUCER (RIGHT) FOR (0.625") DIAMETER FASTENER HOLE IN (0.850") STEP OF REFERENCE STANDARD NDT815 | 1 | |
| AFS-0572-1L | CUSTOM 45° IN STEEL ANGLE BEAM TRANSDUCER (LEFT) FOR ( .307" )DIAMETER FASTENER HOLE'S (0.340" ) STEP OF REFERENCE STANDARD NDT6091. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-1R | CUSTOM 45° IN STEEL ANGLE BEAM TRANSDUCER (RIGHT) FOR ( .307" )DIAMETER FASTENER HOLE'S (0.340" ) STEP OF REFERENCE STANDARD NDT6091. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-2L | CUSTOM 50° IN STEEL ANGLE BEAM TRANSDUCER (LEFT) FOR ( .307" )DIAMETER FASTENER HOLE'S (0.240" ) STEP OF REFERENCE STANDARD NDT6092. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-2R | CUSTOM 50° IN STEEL ANGLE BEAM TRANSDUCER (RIGHT) FOR ( .307" )DIAMETER FASTENER HOLE'S (0.240" ) STEP OF REFERENCE STANDARD NDT6092. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-3L | CUSTOM 60° IN STEEL ANGLE BEAM TRANSDUCER (LEFT) FOR ( .307" )DIAMETER FASTENER HOLE'S (0.200" ) STEP OF REFERENCE STANDARD NDT6092. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-3R | CUSTOM 60° IN STEEL ANGLE BEAM TRANSDUCER (RIGHT) FOR ( .307" )DIAMETER FASTENER HOLE'S (0.200" ) STEP OF REFERENCE STANDARD NDT6092. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-4L | CUSTOM 60° IN STEEL ANGLE BEAM TRANSDUCER (LEFT) FOR ( .412" )DIAMETER FASTENER HOLE'S (0.200" ) STEP OF REFERENCE STANDARD NDT6092. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-0572-4R | CUSTOM 60° IN STEEL ANGLE BEAM TRANSDUCER (RIGHT) FOR ( .412" )DIAMETER FASTENER HOLE'S (0.200" ) STEP OF REFERENCE STANDARD NDT6092. Includes Test Report and Certificate of Conformance. | 1 | |
| AFS-1175 | 70°. ANGLE BEAM TRANSDUCER in ALUMINUM, SIDE MOUNT MICRODOT CONNECTOR, .187" x .187" ELEMENT. CASE SIZE: .67'L x .26"W x .33"H. Includes Test Report and Certificate of Conformance. Reference: B767 Part 4 53-50-05. Standard Part number NDT679 | 1 | |
| AFS-1175T | 70°. ANGLE BEAM TRANSDUCER in ALUMINUM, .187" x .187" ELEMENT, TOP MOUNTED MICRODOT CONNECTOR. CASE SIZE: .67'L x .26"W x .33"H. Includes Test Report and Certificate of Conformance. Reference: B767 Part 4 53-50-05. Standard Part number NDT679 | 1 | |
| AFS-1346 | CUSTOM 2 ELEMENT RING TRANSDUCER FOR BORE HOLE INSPECTION WITH BOEING REFERENCE STANDARD 55-10-13 PAGE 9 FIGURE 2. TWO MICRODOT CONNECTORS "A" and "B" | 1 | |
| AFS-1394 | CARGOLUX CUSTOM 5MHz .187", 40° IN ALUMINUM SHEAR WAVE TRANSDUCER WITH A 1.00" RADIUS FOR THE BOEING REFERENCE STANDARD LUG 1B7- FITTING-SEQUENCE CARRIAGE ATTACHMENT INBOARD TRAILING EDGE FLAP. CASE SIZE: .500"L x .270"W x .350". Includes Test Report... | 1 | |
| AFW-45/1.83R | 45° IN ALUMINUM LUCITE (PLEXIGLASS) WEDGE, 3/8-32 THREAD WITH A 1.83" RADIUS USED WITH A .25"Ø DIAMETER TRANSDUCER AFC-0520(ABT-0504). Includes Certificate of Conformance...Used with Fairchild Reference Standard part number 27-95031-001. | 1 | |
| AGE-02321-401 | Embraer 170 Reference Standard. Material: 2024-T351 Clad. Top skin = 0.040, Lower skin = 0.080. Rivet - MS2047AD-5. Includes Test Report and Certificate of Conformance. | 1 | |
| AGE-04383-001 | REFERENCE STANDARD, NDI (GSE NUMBER: 538) | 1 | |
| AGE-05546-401 | REFERENCE STANDARD FOR BAGGAGE DOOR CUTOUT, NDI | 2 | |
| AGE-05697-401 | HORIZONTAL STABILIZER REFERENCE STANDARD | 3 | |
| AGE-05698 | REFERENCE STANDARD HORIZONTAL STABILIZER | 1 | |
| AGE-05698-401 | REFERENCE STANDARD HORIZONTAL STABILIZER | 1 | |
| AGE-05698-403 | REFERENCE STANDARD HORIZONTAL STABILIZER | 1 | |
| AGE-05698-405 | REFERENCE STANDARD HORIZONTAL STABILIZER | 1 | |
| AGE-05700 | BAG REFERENCE STANDARD - FABRIC | 1 | |
| AGE-05700-401 | REFERENCE STANDARD BAG-FABRIC | 1 | |
| 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... | 1 | |
| AHS29-C2-A1 | CUSTOM 29 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM WITH 0.015" THRU EDM NOTCH AND 0.030X0.030 CORNER NOTCH. Includes Test Report Traceable to NIST and Certificate of Conformance. | 1 | |
| AL29-32 | BOMBARDIER CALIBRATION REFERENCE STANDARD | 6 | |
| AL35-45 | BOMBARDIER SURFACE REFERENCE STANDARD - 7075-T7ALUMINUM. FULL WIDTH EDM NOTCHES .008", .020", .040" (.005"W +/- .002, MAX.006) BLOCK SIZE: 3.75"L x 1.50"W x 0.25"H | 8 | |
| AMS2630C Custom | Custom Reference Standard Per SAE AMS2630C. material: Titanium Alloy, Ti6Al4V per AMS-4928R Annealed. Includes 2 EDM Flaws per customer supplied Drawing. Includes Test Report Traceable to NIST and Certificate of Conformance. | 1 | |
| AN670-55-31-102 | CALIBRATION REFERENCE STANDARD (CRS), MADE OF ALUMINUM WITH MULTIPLE LAYERS CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| AN670-55-31-110 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| ANDT-3016-B | BOEING REFERENCE STANDARD | 4 | |
| ANDT1015 | BOEING REFERENCE STANDARD 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT1049 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN5-2, BACR15CE5D-2, BACR15ET7D-2). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT1049/.036 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5, .036 SKIN. Includes Test Report and Certificate of Conformance. | 1 | |
| ANDT1050 | REFERENCE STANDARD B737 | 3 | |
| ANDT1051 | REFERENCE STANDARD B737 | 4 | |
| ANDT1052 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-2, BACR15CE8D-2, BACR15BB8D-2). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT1053 | REFERENCE STANDARD B737 | 5 | |
| ANDT1054 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-3, BACR158D-3, BACR15BB8D-3). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT1055 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT1056 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | 4 | |
| ANDT1057 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN8-4, BACR15CE8D-4, BACR15BB8D-4). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT1077 | BOEING REFERENCE STANDARD, 53-30-00 PT 6 FIG 5 and 737 51- 00-26. FASTENER (BACB30FN5-2, BACR15CE5D-2, BACR15ET7D-2). Includes Test Report and Certificate of Conformance. | 4 | |
| 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) | 4 | |
| 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) | 2 | |
| ANDT1081 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENER (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | 2 | |
| ANDT1082 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENERS: (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT3004 | BOEING REFERENCE STANDARD 737 Part 6 53-30-12 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT3006 | BOEING REFERENCE STANDARD 737 Part 6 53-30-14 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT3016-B | Boeing Reference Standard, PT6 53-10-54 | 4 | |
| ANDT3016B | BOEING REFERENCE STANDARD 737 PT6 53-10-54 PG 7 FG 2 | 4 | |
| ANDT3019 | BOEING REFERENCE STANDARD 737 Part 6 53-30-16 Page 5 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| ANDT378 | REFERENCE STANDARD B737 | 1 | |
| ANDT388 | BOEING 737 REFERENCE STANDARD PART 6 53-10-48, ..PAGE 11 FIGURE 4. Includes Test Report and Certificate of Conformance. | 1 | |
| ANDT390A | BOEING REFERENCE STANDARD 737 Part 6 53-10-47 Page 10 Figure 4. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| ANDT390B | BOEING REFERENCE STANDARD 737 Part 6 53-10-47 Page 11 Figure 5. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| ANDT4126 | Boeing Reference Standard, 747 PT6 53-30-00:PG5 FIG6 DETAIL I | 2 | |
| ANDT4223 | BOEING REFERENCE STANDARD PT 6 53-10-33 FIG 2, PAGE8. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT001 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-02 Page 6 Frigure 2. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes | 1 | |
| APB-NDT003 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-02 Page 9-10 Figure 5. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Include | 1 | |
| APB-NDT004 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-01 Page 5-6 Figure 2. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Include | 1 | |
| APB-NDT005 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-02 Page 13-14. Figure 7. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Inclu | 1 | |
| APB-NDT006 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-53 Page 5-6 Figure 2. Material: 7075-T7 (40-44% IACS), 2324-T3 (29.5-33.5% IACS), and 2224-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Inclu | 2 | |
| APB-NDT011A | REFERENCE STANDARD B767 | 1 | |
| APB-NDT011B | REFERENCE STANDARD B767 | 1 | |
| APB-NDT011C | REFERENCE STANDARD B767 | 1 | |
| APB-NDT011D | REFERENCE STANDARD B767 | 1 | |
| APB-NDT012 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 4 57-20-03 Page 8 Figure 3. Material: 2224-T3 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT013 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 4 57-20-03 Page 10 Figure 4. Material: 2224-T3 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT014 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 4 57-20-03 Page 12 Figure 5. Material: 2224-T3 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT015 | BOEING AVIATION PARTNERS REFERENCE STANDARD 767 Part 6 57-20-09 Page 21-22 Figure 10. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Ce | 1 | |
| APB-NDT016 | BOEING AVIATION PARTNERS REFERENCE STANDARD 767 Part 6 57-50-09 Page 24-25. Figure 12 Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Ce | 1 | |
| APB-NDT3301 | AVIATION PARTNERS BOEING REFERENCE STANDARD 737 Part 6 57-20-34 Page 7-8 Figure 2. Material: 2024-T3 (28.5-32% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT3302 | AVIATION PARTNERS BOEING REFERENCE STANDARD 737 Part 6 57-20-35 Page 6 Figure 2. Material: 2024-T3, 7050-T7 (40-44% IACS), and 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT3801NG | BOEING REFERENCE STANDARD PT6 737 57-10-205 PAGE 7-8, FIGURE 2, SHEETS 1&2 | 2 | |
| APB-NDT3802NG | BOEING REFERENCE STANDARD PT 6 737 57-10-205 PAGE 11-12, FIGURE 4, SHEETS 1 & 2. | 2 | |
| APB-NDT5203 | AVIATION PARTNERS REFERENCE STANDARD 737 Part 6 57-20-02 Page 7-8 Figure 2. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate | 2 | |
| APB-NDT5204 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-02 Page 11-12 Figure 4. Material: 2224-T3 and 2324-T3 or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 2 | |
| APB-NDT5205 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-02 Page 15-16 Figure 6. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Cer | 2 | |
| APB-NDT5206 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-03 Page 8-9 Figure 2. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certi | 2 | |
| APB-NDT5207 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-03 Page 12-13 Figure 4. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Cer | 2 | |
| APB-NDT5208 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-03 Page 16-17 Figure 6. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Cer | 2 | |
| APB-NDT5209 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 4 57-20-03 Page 9 Figure 2. Material: Airplane Quality Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT5301 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-01 Page 15-16 Figure 6. Material: 7050-T7 (40-44% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT5302 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-01 Page 11-12 Figure 4. Material: 7050-T7 (40-44% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT5303 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-01 Page 7-8 Figure 2. Material: 7050-T7 (40-44% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| ARP-.385/.720 | LOW FREQUENCY REFLECTION RING PROBE, 500Hz-5KHz.385"Ø ID .720"Ø OD, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. FOR REFERENCE STANDARD APB-3302. Includes Test Report and Certificate of Conformance. | 1 | |
| ARP-.75-1.25/300Hz | REFLECTION RING PROBE, 1.25"OD .75" ID(19.6mm) TRIAX FISHER CONNECTOR 300HZ-1KHZ. REFERENCE STANDARD NDT3176-X 737 PT 6 57-10-59, 737 PART 6 57-10-53 NDT3168. Includes Test Report and Certificate of Conformance. | 1 | |
| ARP-.85/1.40-200Hz | LOW FREQUENCY REFLECTION RING PROBE .85" I.D. 1.40" O.D. TRIAX CONNECTOR 100Hz-500Hz. REFERENCE STANDARD NDT3176-X 737 PT 6 57-10-59. Includes test report and Certificate of Conformance. | 1 | |
| ARP-1.2/100H-7 | LOW FREQUENCY REFLECTION RING PROBE 1.2" OD, .605" ID, 50Hz-3KHz TRIAX FISHER CONNECTOR. 737 PART 6 57-10-58, pg.2. and 737 PART 6 57-10-54, pg.2 USED WITH NDT3153-X AND 3167-X SERIES REFERENCE STANDARDS. Includes Test Report and Certificate of ... | 1 | |
| ARP-1.25-.75-300H | REFLECTION RING PROBE TRIAX FISHER CONNECTOR, 1.25"OD .75" ID(19.6mm) 300HZ-1KHZ. 737 PART 6 57-10-53, pg.2, USED WITH REFERENCE STANDARD NDT3168 AND NDT3176-X. Includes test report and Certificate of Conformance... | 1 | |
| ARP-1.40/.85-200Hz | LOW FREQUENCY REFLECTION RING PROBE .85" I.D. 1.40" O.D. TRIAX FISCHER CONNECTOR 100Hz-500Hz. REFERENCE STANDARD NDT3176-X 737 PT 6 57-10-59. Includes test report and Certificate of Conformance. | 1 | |
| ARS-1012HCS | 12 HOLE REFERENCE STANDARD 4130 OR 4340 CARBON STEEL WITH 0.020" x 0.020" and 0.030" x 0.030" CORNER EDM NOTCH. HOLE SIZES: 1/8, 5/32, 3/16, 13/64, 7/32, 5/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64. Includes Test Report and Certificate of Conformance. | 1 | |
| ARS-1S | Surface reference standard, 4340 or 4130 steel, with EDM notch depth of 0.010" x .005" wide Reference standard overall dImensions 1.0" X 3.0" X 0.25" inches .007" W MAX. Includes Certification traceable to NIST. | 1 | |
| BASE PLATES 717RS2 1/4 | BOEING UT REFERENCES STANDARD | 1 | |
| BASE PLATES 717RS2 1/8 | BOEING UT REFERENCES STANDARD | 1 | |
| BH7475-T7351 | CALIBRATION REFERENCE STANDARD, ALUMINUM ALLOY, CONDUCTIVITY VALUE OF 35% TO 45% IACS THAT CONTAINS VARIOUS HOLE SIZES WITH 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ OR EQUIVALENT) | 4 | |
| BHS6061-T6/C2 | Bombardier Bolt hole and surface crack reference standard 6061-T6, 15 Holes, .030 Midwall notches top plate, (2) .030 corner notches each hole on the bottom plate. .008, .020, .030 surface notches | 1 | |
| C12-DEL-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance... | 3 | |
| C12-DIS-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DISBOND and CORE LAMINATE INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance. | 3 | |
| C12-PCS-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED HOLE and SPLICE CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance... | 3 | |
| C12-POT-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED CORE and CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance... | 3 | |
| CA12-1508A | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T7 ALUMINUM, 54-10-11 PAGE 634A FIG.603 SHEET 21B | 1 | |
| CA235-235502 | AIRBUS MILITARY REFERENCE STANDARD 53-30-10 FIG 505, PAGE 508. | 1 | |
| CE1617528 | CALIBRATION STANDARD, BOMBARDIER TEST REFERENCE ULTRA SONIC NDI. MATERIAL: 7475-T7351 and 7040-T7451 ALUMINUM. MS90254U0805D FASTENERS. Includes Test Report and Certificate of Conformance. | 1 | |
| CE1617529 | CALIBRATION STANDARD, BOMBARDIER TEST REFERENCE ULTRA SONIC NDI. MATERIAL: 7475-T7351 and 7040-T7451 ALUMINUM. MS90254U0805D FASTENERS. Includes Test Report and Certificate of Conformance. | 1 | |
| CE9900085-101 | COMPOSITE LAMINATE CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900086-101 | COMPOSITE LAMINATE CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-001 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-003 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-005 | CALIBRATION REFERENCE STANDARD (CRS) | 1 | |
| CE9900088-007 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-009 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900430-001 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CHRS-2-12 | Carbon Reference Standard, SAE ARP5606, 12 PLY R&D | 1 | |
| CHRS-2-3 | Carbon Reference Standard, SAE ARP5606, 3 PLY R&D | 1 | |
| CHRS-2-3-.5D | Carbon Reference Standard, SAE ARP5606, 3 PLY- .5D R&D | 1 | |
| CHRS-2-6 | Carbon Reference Standard, SAE ARP5606, 6 PLY R&D | 1 | |
| CHRS-2-6-.5D | Carbon Reference Standard, SAE ARP5606, 6 PLY- .5D R&D | 1 | |
| CHRS-2-9 | Carbon Reference Standard, SAE ARP5606, 9 PLY R&D | 1 | |
| CHRS-2-9-.5D | Carbon Reference Standard, SAE ARP5606, 9 PLY- .5D R&D | 1 | |
| DAC GSET MG.01 | Aluminum-Broze (10%-20% IACS) Reference Standard | 1 | |
| DAC GSET-MG | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 ALUMINUM BRONZE | 1 | |
| DC-10 FIG603/15C | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628B FIG.603 SHEET 15C | 1 | |
| DC-10 FIG603/15E/4340 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628D FIG.603 SHEET 15E | 1 | |
| DC-10 FIG603/15G | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628F FIG.603 SHEET 15G | 1 | |
| 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 | 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 | 1 | |
| 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 | 1 | |
| DC-10 FIG603/39-4 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #4 | 1 | |
| DC-10 FIG603/5 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 617 FIG.603 SHEET 5 | 1 | |
| 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. | 1 | |
| DRT74469 | Messier-Dowty Reference Standard, Aluminum, Appendix A Service Bulletin No. 146-32-174 Pg 4 Fg A2 | 2 | |
| 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. | 1 | |
| E53-002A | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler = .040"..Filler = .031"..Stringer = .063" | 1 | |
| E53-002A. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler 1 = .040"..Doubler 2 = .063"..Filler = .... | 1 | |
| E53-002B | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .047"..Doubler = .050"..Filler = .047"..Stringer = .063" | 1 | |
| E53-002B. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .047"..Doubler 1 = .050"..Doubler 2 = .063"..Filler = .... | 1 | |
| E53-002C | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .055"..Doubler = .063"..Filler = .055"..Stringer = .063" | 1 | |
| E53-002C. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .055"..Doubler 1 = .063"..Doubler 2 = .063"..Filler = .... | 1 | |
| E53-002D | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .071"..Doubler = .080"..Filler = .071"..Stringer = .063" | 1 | |
| E53-002D. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .071"..Doubler 1 = .080"..Doubler 2 = .063"..Filler = .... | 1 | |
| E53-002E | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .080"..Doubler = .098"..Filler = .080"..Stringer = .063" | 1 | |
| E53-002E. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .080"..Doubler 1 = .098"..Doubler 2 = .063"..Filler = .... | 1 | |
| E53-002F | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .098"..Doubler = .110"..Filler = .098"..Stringer = .063" | 1 | |
| E53-002F. | EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .098"..Doubler 1 = .110"..Doubler 2 = .063"..Filler = .... | 1 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| E53-004 | EMBRAER 190/195 REFERENCE STANDARD PT 6 53-23-00 pages 1-13. Material: 2024-T3 Alclad Aluminum. Repair Doubler Configuration. Includes Test Report and Certificate of Conformance. Repair Doubler = .125" Fus Skin Thickness = .098" Filler = .098" In | 1 | |
| EM145NDI540043A | EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 606 | 1 | |
| EM145NDI540047A | EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 615 | 1 | |
| EMB170-175-NDT4195 | REFERENCE STANDARD, EMB | 1 | |
| ET.28 | Bombardier Bolt hole and surface crack reference standard 6061-T6, 15 Holes, .030 Midwall notches top plate, (2) .030 corner notches each hole on the bottom plate. .008, .020, .030 surface notches | 1 | |
| ET6018 | CUSTOM SIKORSKY S61-N FLAT BOTTOM HOLE AFT REAR FUSELAGE REFERENCE STANDARD 51-10-05 FIGURE 7 (SHEETS 1-5). MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certiicate of Conformance. | 1 | |
| EX601R47015-001 | CALIBRATION REFERENCE STANDARD | 1 | |
| EX601R47015−001 | Calibration reference standard − piano hinge passenger door (Bombardier Inc.) | 1 | |
| EX601R51086-001 | CALIBRATION REFERENCE STANDARD | 1 | |
| EX601R51093 | Calibration reference standard (CRS) multiple layers fastened assembly containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EX604-60024 | CALIBRATION REFERENCE STANDARD MULTI-LAYERED ALUMINUM ALLOY FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 2 | |
| EX604-60024-001 | CALIBRATION REFERENCE STANDARD | 1 | |
| EX604−60024 | Calibration reference standard multi−layered aluminum alloy fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 2 | |
| EX605−60037−001 | CALIBRATION REFERENCE STANDARD MADE FROM | 1 | |
| EXBC100-59009-001 | CALIBRATION REFERENCE STANDARD | 1 | |
| EXBC670-59040-005 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 3.000 IN. (76.20 MM)OUTSIDE DIAMETER 1.563 IN. (39.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−001 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 4.224 IN. (107.29 MM)OUTSIDE DIAMETER 2.311 IN. (58.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−003 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 3.374 IN. (85.70 MM)OUTSIDE DIAMETER 2.311 IN. (58.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−007 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.000 IN. (50.80 MM)OUTSIDE DIAMETER 1.032 IN. (26.21 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−009 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.000 IN. (50.80 MM)OUTSIDE DIAMETER 1.332 IN. (33.83 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−011 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.500 IN. (63.50 MM)OUTSIDE DIAMETER 1.563 IN. (39.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−013 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.500 IN. (63.50 MM)OUTSIDE DIAMETER 1.332 IN. (33.83 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59045 | CALIBRATION REFERENCE STANDARD ASSEMBLY ALUMINUM ALLOY CONTAINS 0.250 IN. (6.35 MM) LONG ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59046 | CALIBRATION REFERENCE STANDARD ASSEMBLY ALUMINUM ALLOY CONTAINS 0.250 IN. (6.35 MM) LONG ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59066-001 | CALIBRATION REFERENCE STANDARD CONTAINS 0.250 IN | 1 | |
| EXBC670-59066−001 | CALIBRATION REFERENCE STANDARD CONTAINS 0.250 IN (6.35 MM) LONG0.005 IN. (0.127 MM) WIDE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59089-001 | CALIBRATION REFERENCE STANDARD SIMILAR IN MATERIAL AS THE INSPECTION AREA CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ) | 1 | |
| EXBC670-59089−001 | CALIBRATION REFERENCE STANDARD SIMILAR IN MATERIAL AS THE INSPECTION AREA CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59133 | CALIBRATION REFERENCE STANDARD MADE FROM ALUMINUM ALLOY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59141 | CALIBRATION REFERENCE STANDARD MULTI LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59142 | CALIBRATION REFERENCE STANDARD MADE FROM ALUMINUM ALLOY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59143-001 | CALIBRATION REFERENCE STANDARD, ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES. (MHIRJ) | 1 | |
| EXBC670-59145 | CALIBRATION REFERENCE STANDARD ALUMINUM ALLOY MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59148 | CALIBRATION REFERENCE STANDARD (CRS) MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES. (BOMBARDIER INC.) | 1 | |
| EXBC670-59156 | CALIBRATION REFERENCE STANDARD MADE FROM MULTIPLE ALUMINUM ALLOY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59157-003 | CALIBRATION REFERENCE STANDARD, MULTIPLE LAYERED FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (MHIRJ) | 1 | |
| EXBC670-59159 | CALIBRATION REFERENCE STANDARD(CRS), MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM)NOTCHES (MHIRJ). | 1 | |
| EXBC670-59160 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERED FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| EXBC670-59161 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59162 | CALIBRATION REFERENCE STANDARD, ALUMINUM ALLOY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCH. (MHIRJ OR EQUIVALENT) | 1 | |
| EXBC670-59163 | CALIBRATION REFERENCE STANDARD TITANIUM ALLOY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCH. (BOMBARDIER INC.EQUIVALENT) | 1 | |
| EXBC670-59164 | CALIBRATION REFERENCE STANDARD MULTIPLE LAYERS ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59174 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59174-001 | CALIBRATION REFERENCE STANDARD | 1 | |
| EXBC670-59176 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59177 | CALIBRATION REFERENCE STANDARD ALUMINUM MULTIPLE LAYER FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59178 | CALIBRATION REFERENCE STANDARD, MULTIPLE LAYER FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (MHIRJ) | 1 | |
| EXBC670-59179 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ). | 1 | |
| EXBC670-59180 | CALIBRATION REFERENCE STANDARD ALUMINUM ALLOY MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59181 | CALIBRATION REFERENCE STANDARD ALUMINUM MULTIPLE LAYER FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES. (BOMBARDIER INC.) | 1 | |
| EXBC670-59182 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ). | 1 | |
| EXBC670-59182-001FS | CALIBRATION REFERENCE STANDARD | 1 | |
| EXBC670-59183-001 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) TRANSDUCER - ANGLE BEAM, 5.0 MHZ, 0.375 IN. (9.53 MM) H X | 1 | |
| EXBC670-59185 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| EXBC670−59040−001 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 4.224 in. (107.29 mm)outside diameter 2.311 in. (58.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−003 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 3.374 in. (85.70 mm)outside diameter 2.311 in. (58.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−005 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 3.000 in. (76.20 mm)outside diameter 1.563 in. (39.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−007 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.000 in. (50.80 mm)outside diameter 1.032 in. (26.21 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−009 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.000 in. (50.80 mm)outside diameter 1.332 in. (33.83 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−011 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.500 in. (63.50 mm)outside diameter 1.563 in. (39.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−013 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.500 in. (63.50 mm)outside diameter 1.332 in. (33.83 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59044 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined (EDM) notches. (Bombardier Inc.) | 1 | |
| EXBC670−59045 | Calibration reference standard assembly aluminum alloy contains 0.250 in. (6.35 mm) long electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59046 | Calibration reference standard assembly aluminum alloy contains 0.250 in. (6.35 mm) long electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59065 | Calibration reference standard assembly aluminum and steel alloy contains 0.250 in. (6.35 mm) long electrical discharge machined notches (Bombardier inc.) | 1 | |
| EXBC670−59066−001 | Calibration reference standard contains 0.250 in (6.35 mm) long0.005 in. (0.127 mm) wide electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59068 | Calibration reference standard multiple layered assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59089−001 | Calibration reference standard similar in material as the inspection area containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59094 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59098 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59099 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59101 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59125 | Calibration reference standard assembly contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59133 | Calibration reference standard made from aluminum alloy containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59134 | Calibration reference standard aluminum alloy that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59139−001 | Calibration reference standard made from aluminum alloy that contains electrical discharge machined notches (Bombardier inc.) | 1 | |
| EXBC670−59141 | Calibration reference standard multi layers fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59142 | Calibration Reference Standard made from aluminum alloy containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59143 | Calibration Reference Standard assembly that contains electrical discharge machined notches. (Bombardier Inc.) | 1 | |
| EXBC670−59145 | Calibration reference standard aluminum alloy multiple layers fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59148 | Calibration Reference Standard (CRS) multiple layers fastened assembly that contains electrical discharge machined (EDM) notches. (Bombardier Inc.) | 1 | |
| EXBC670−59153 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59154 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59156 | Calibration Reference Standard made from multiple aluminum alloy containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59157 | Calibration reference standard multiple layered fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59158 | Calibration Reference Standard (CRS) multiple layers fastened assembly containing electrical discharge machined (EDM) notches (Bombardier Inc.). | 1 | |
| EXBC670−59159 | Calibration Reference Standard (CRS) multiple layers fastened assembly containing electrical discharge machined (EDM) notches (Bombardier Inc.). | 1 | |
| EXBC670−59161 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59162 | Calibration Reference Standard aluminum alloy that contains electrical discharge machined notch. (Bombardier Inc. or equivalent) | 1 | |
| EXBC670−59163 | Calibration Reference Standard titanium alloy that contains electrical discharge machined notch. (Bombardier Inc. or equivalent) | 1 | |
| EXBC670−59164 | Calibration Reference Standard multiple layers assembly that contains electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59174 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59176 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59177 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59178 | Calibration reference standard multiple layer fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59180 | Calibration reference standard aluminum alloy multiple layers fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59181 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined (EDM) notches. (Bombardier Inc.) | 1 | |
| EXSH670-31001-1 | CALIBRATION REFERENCE STANDARD, STGR15R BUTT JOINT, CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ) | 1 | |
| EXSH670-31001−1 | CALIBRATION REFERENCE STANDARD STGR15R BUTT JOINT CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-31002-1 | CALIBRATION REFERENCE STANDARD STGR1L AND STGR20L BUTT JOINTS CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-31011−1 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-35910-1 | CALIBRATION REFERENCE STANDARD, ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES | 1 | |
| EXSH670-35910−1 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES | 1 | |
| EXSH670−31001−1 | Calibration reference standard STGR15R butt joint contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31002−1 | Calibration reference standard STGR1L and STGR20L butt joints contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31011−1 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31014−1 | Calibration reference standard pressure bulkhead machined frames FS693.00 and FS847.00 contains subsurface electrical discharge machined notches. (Bombardier Inc.) | 1 | |
| EXSH670−35910−1 | Calibration Reference Standard assembly that contains electrical discharge machined notches | 1 | |
| EXSH690-31003−11 | CALIBRATION REFERENCE STANDARD EMERGENCY EXIT DOOR SURROUND STRUCTURE CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH690-31022 | CALIBRATION REFERENCE STANDARD POTABLE WATER. | 1 | |
| EXSH690-31023-1 | CALIBRATION REFERENCE STANDARD, CIRCUMFERENTIAL SKIN JOINT STGR7 TEST PIECE, CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (MHIRJ) | 1 | |
| EXSH690-31023−1 | CALIBRATION REFERENCE STANDARD CIRCUMFERENTIAL SKIN JOINT STGR7 TEST PIECE CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH690−31003−11 | Calibration reference standard emergency exit door surround structure contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH690−31022 | Calibration reference standard potable water. | 1 | |
| EXSH690−31023−1 | Calibration reference standard circumferential skin joint STGR7 test piece contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH698-31024-1 | CALIBRATION REFERENCE STANDARD | 1 | |
| F12-DEL-3C1N | REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance. | 1 | |
| F12-DIS-3C1N | REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DISBOND and CORE FIBERGLASS INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance. | 1 | |
| F15-AL-UT-0.175-2 | F15 REFERENCE STANDARD. MATERIAL: 2024-T3, OUTBOARD TORQUE BOX REAR SPAR, 68A115101, LOWER FLANGE FASTENER HOLES. Includes Test Report and Certificate of Conformance. | 1 | |
| 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 | 1 | |
| G11-STD-1 | G11 PHENOLIC (GAROLITE) Reference Standard, SAE ARP5605, .007 THRU .050 FBH (REMAINING THICKNESS) | 1 | |
| G11-STD-2 | G11 PHENOLIC (GAROLITE) Reference Standard, SAE ARP5605, .060 THRU .180 FBH (REMAINING THICKNESS) | 1 | |
| G11-STD-3 | G11 PHENOLIC (GAROLITE) Reference Standard, SAE ARP5605, .220 THRU .450 FBH (REMAINING THICKNESS) | 1 | |
| G11-STD-4 | G11 PHENOLIC (GAROLITE) Reference Standard, SAE ARP5605, .500 THRU 1.00 FBH (REMAINING THICKNESS) | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| GSE 503/171T17969-401 | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance. | 1 | |
| II W V1 (STEEL) | RUDDER BOLT REFERENCE STANDARD | 1 | |
| IIW TYPE 2 | CALIBRATION REFERENCE STANDARD BLOCK, ALUMINUM. (GE OR EQUIVALENT) | 1 | |
| KC10-7025-3 ASSEMBLY | CUSTOM MANUFACTURED BOEING REFERENCE STANDARD FOR ULTRASONIC INSPECTION 101/201 | 1 | |
| KC10-7027 | BOEING REFERENCE STANDARD KC10 FUEL COMPENSATOR CUTOUT-INSPECTION.( 301 GUIDE AND 302 GUIDE ARE PART OF INSPECTION AND SOLD SEPARATELY) | 1 | |
| MD11-05b | MD11 SUBSURFACE ALUMINUM ETLF REFERENCE STANDARD FIG 1.10 (Sheets 1-5) Section 2-1 Pages 1-5. Includes Test Report and Certificate of Conformance. | 1 | |
| MD11-05c | MD11 SUBSURFACE ALUMINUM ETLF REFERENCE STANDARD FIG 1.11 (Sheets 1-5) Section 2-1 Pages 1-5. Includes Test Report and Certificate of Conformance. | 1 | |
| MD90-01 | MD-90 REFERENCE STANDARD, SECTION 2-1 FIG 1.1 FASTENER (HL19PB-6-4 +NAS1252-10L + NAS679A3) Includes Test Report and Certificate of Conformance. | 1 | |
| MHS-12-1A-2 | ALUMINUM (7075-T6) MULTI-HOLE REFERENCE STANDARD WITH CERTIFICATE TRACEABLE TO NIST | 1 | |
| NDT 1016 | BOEING REFERENCE STANDARD | 3 | |
| NDT 1017 | 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. | 2 | |
| NDT 1018 | BOEING REFERENCE STANDARD | 3 | |
| NDT 1019 | BOEING REFERENCE STANDARD | 3 | |
| NDT 1020 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1021 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1039-0.040/0.020 | REFERENCE STANDARD BOND TEST INS | 2 | |
| NDT 1039-0.040/0.040 | REFERENCE STANDARD BOND TEST INS | 2 | |
| NDT 1039-0.050/0.040 | REFERENCE STANDARD BOND TEST INS | 2 | |
| NDT 1039-0.063/0.056 | REFERENCE STANDARD BOND TEST INS | 2 | |
| NDT 1040 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1041 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1042 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1043 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1044 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1045 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1048 | BOEING REFERENCE STANDARD | 4 | |
| NDT 1061 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1062 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1072 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1073 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1074 | BOEING REFERENCE STANDARD | 2 | |
| NDT 1084 | BOEING REFERENCE STANDARD | 1 | |
| NDT 1086-040 | BOEING REFERENCE STANDARD NDT1086-040 767 PT 4 53-00-01 AND 747 PT 4 53-30-05 | 3 | |
| NDT 1086-070 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 AND 737 53-30-05. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 1086-100 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 AND 737 53-30-05. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 1086-110 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 AND 737 53-30-05. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 1086-120 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 AND 737 53-30-05. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 1087- 3 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 | 3 | |
| NDT 1087-3 | BOEING REFERENCE STANDARD | 3 | |
| NDT 1087-4 | BOEING REFERENCE STANDARD | 3 | |
| NDT 1088-072/050 | Boeing Reference Standard | 4 | |
| NDT 1088-144/050 | Boeing Reference Standard | 3 | |
| NDT 185 | BOEING REFERENCE STANDARD | 1 | |
| NDT 188A | BOEING REFERENCE STANDARD | 1 | |
| NDT 189 | BOEING REFERENCE STANDARD | 2 | |
| NDT 192 | BOEING REFERENCE STANDARD | 1 | |
| NDT 194B | Boeing Reference standard w/Certs | 2 | |
| 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. | 1 | |
| NDT 3019 | Boeing Reference Standard | 2 | |
| NDT 3030 | Boeing Reference Standard, 737 PT4 57-10-01: Page 5, Figure 2 | 2 | |
| NDT 3116 | BOEING REFERENCE STANDARD 737 PT 4 53-10-06 FIG 2. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT 3141 | BOEING REFERENCE STANDARD 737 PART 4 55-10-13 PAGE | 2 | |
| NDT 3152- A | BOEING REFERENCE STANDARD 737 PART 6 57-10-55 PAGE 8 FIGURE 2. MATERIAL: 2024-T3. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 3152- F | BOEING REFERENCE STANDARD 737 PART 6 57-10-55 PAGE 8 FIGURE 2. MATERIAL: 2024-T3. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 3152- K | BOEING REFERENCE STANDARD 737 PART 6 57-10-55 PAGE 8 FIGURE 2. MATERIAL: 2024-T3. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 3156 | BOEING REFERENCE STANDARD 737 PART 6 57-10-60 PAGE 11 FIGURE 2. MATERIAL: 2024-T3. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 4 | |
| NDT 3164 | BOEING REFERENCE STANDARD 737 PART 6 57-10-60 PAGE 11 FIGURE 2. MATERIAL: 7150-T7. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT 3166- 007 | BOEING REFERENCE STANDARD 737 PART 4 57-10-08 PAGE 6 FIGURE 2. MATERIAL: AIRCRAFT QUALITY ALUMINUM. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 4 | |
| NDT 3170 | BOEING REFERENCE STANDARD 737 PART 4 57-10-06 PAGE 16 FIGURE 2. MATERIAL: AIRCRAFT QUALITY ALUMINUM. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 5 | |
| NDT 3171 | BOEING REFERENCE STANDARD 737 PART 4 57-10-06 PAGE 17 FIGURE 3. MATERIAL: AIRCRAFT QUALITY ALUMINUM. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 5 | |
| NDT 3285 | BOEING REFERENCE STANDARD 737 PART 6 53-30-63 PAGE 11 FIGURE 2. MATERIAL: 7075-T6. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT 3289 | BOEING REFERENCE STANDARD 737 PART 6 53-30-65 PAGE 8 FIGURE 2. MATERIAL: 2024-T3 AND 7075-T6. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT 3293 | BOEING REFERENCE STANDARD 737 PART 6 53-30-65 PAGE 8 FIGURE 2. MATERIAL: 2024-T3 AND 7075-T6. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT 3299 | BOEING REFERENCE STANDARD 737 PART 6 53-30-65 PAGE 8 FIGURE 2. MATERIAL: 2024-T3 AND 7075-T6. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT 396 | BOEING REFERENCE STANDARD | 6 | |
| NDT 398 | BOEING REFERENCE STANDARD 737 PT 4 53-10-01. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT 4245 | Boeing Reference Standard, 747 PT4 54-40-25, PG6 FIG2 | 1 | |
| NDT 6001 | Boeing Steel Reference Standard w/certs | 2 | |
| NDT 6017 | Boeing titanium reference standard. | 2 | |
| NDT 6018 | Boeing Titanium Reference Standard w/certs | 2 | |
| NDT 7015 C | CALIBRATION REFERENCE STANDARD | 1 | |
| NDT 7015B | ULTRASONIC CALIBRATION REFERENCE STANDARD | 1 | |
| NDT 7078 | ULTRASONIC CALIBRATION REFERENCE STANDARD | 1 | |
| NDT 745 | CALIBRATION REFERENCE STANDARD | 2 | |
| NDT 786-A | CALIBRATION REFERENCE STANDARD | 2 | |
| NDT-1024 | BOEING REFERENCE STANDARD | 2 | |
| NDT-1039-1.0/0.5 | Bond Reference Standard | 1 | |
| NDT-1039-1.0/1.0 | Bond Reference Standard | 1 | |
| NDT-1039-1.3/1.1 | Bond Reference Standard | 1 | |
| NDT-1039-1.6/1.4 | Bond Reference Standard | 1 | |
| NDT-1069B | Reference Standard NDT-1069B | 1 | |
| NDT-1094-110-A | BOEING REFERENCE STANDARD 737 PART 4 53-30-07, 757 PART 4 53-00-02 FIG 2, 777 PART 4 53-00-02 PAGE 34 FIGURE 2. MATERIAL: ALUMINUM. PROCUDURES VARY WITH PLANE MODEL. ALL MODELS FOR THIS REFERENCE STANDARD. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMAN | 2 | |
| NDT-1094-130-A | BOEING REFERENCE STANDARD 737 PART 4 53-30-07, 757 PART 4 53-00-02 FIG 2, 777 PART 4 53-00-02 PAGE 34 FIGURE 2. MATERIAL: ALUMINUM. PROCUDURES VARY WITH PLANE MODEL. ALL MODELS FOR THIS REFERENCE STANDARD. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMAN | 2 | |
| NDT-1094-40 | REFERENCE STANDARD BOEING 737 | 2 | |
| NDT-1094-40-A | REFERENCE STANDARD BOEING 737 | 2 | |
| NDT-3021 | REFERENCE STANDARD B737 PT.6 7-50-01 | 6 | |
| NDT006 | NDT REFERENCE STANDARD BOEING 767 | 1 | |
| 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. | 3 | |
| NDT1016 3.2-5.5MM | Special Boeing Type Reference Standard, PT6 51-00-00 PG 10, Fig 16 Detail III | 1 | |
| 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. | 2 | |
| 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. | 3 | |
| 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. | 3 | |
| 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. | 2 | |
| 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. | 2 | |
| NDT1022 | BOEING REFERENCE STANDARD PT 6 51-00-00 | 3 | |
| NDT1022-27/6 | BOEING REFERENCE STANDARD 767 51-00-14 PT 6 FIG 3, 757 Part 6 51-00-14 Page 8 Figure 3. SINGLE STANDARD WITH ALL SIX HOLES. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1023 | BOEING REFERENCE STANDARD PT 6 51-00-00 | 2 | |
| NDT1024 | BOEING REFERENCE STANDARD PT 6 51-00-00 | 2 | |
| NDT1025 | BOEING REFERENCE STANDARD PT 6 51-00-00 | 2 | |
| NDT1026 | BOEING REFERENCE STANDARD PT 6 51-00-00 | 2 | |
| NDT1027 | BOEING REFERENCE STANDARD PT 6 51-00-00 | 2 | |
| NDT1031 | BOEING 707 REFERENCE STANDARD 707 PART 6, 57-10-07 DETAIL 2 FIGURE 93 SHEET 7 PG.1525. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1033-10 | ALUMINUM TO ALUMINUM SKIN REFERENCE STANDARD WITH A TOTAL OF 10 BONDED SHIMS .016"-.125" THICK. 100 THICKNESS COMBINATIONS WITH SIMULATED DISBOND DEFECTS. PART 4 51-00-01 | 4 | |
| NDT1037-0.032 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.036 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.040 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.050 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.063 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.072 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.080 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.090 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.100 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.110 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1037-0.125 | BOEING REFERENCE STANDARD 767 Part 6 51-00-20 Page 7-10 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1038 | BOEING REFERENCE STANDARD (ALUMINUM SKIN/CORE DEFECTS) 737/757 PART 4 51-00-05 PAGE 5-7 FIGURE 1. MATERIAL: ANY 2000, 6000,7000 SERIES ALUMINUM, INCLUDES C-SCAN AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT1039-.016/.016 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.016/.020 | Boeing Reference Standard 737 PT4 53-30-01 PG5 FIG2 | 1 | |
| NDT1039-.025/.025 | Boeing Reference Standard 737 PT4 53-30-01 PG5 FIG2 | 1 | |
| NDT1039-.032/.032-I625 | Boeing Reference Standard, 757 PT4 51-00-05:PG8 FIG2, Inconel 625 | 1 | |
| NDT1039-.036/.036 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.040/.016 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.040/.020 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.040/.040 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.040/.063 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.050/.032 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.050/.040 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.050/.063 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.050/.080 | Boeing Reference Standard 737 PT4 53-30-01 PG5 FIG2 | 1 | |
| NDT1039-.063/.056 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.063/.063 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.063/.080 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2.. | 1 | |
| NDT1039-.080/.025 | Boeing Reference Standard 737 PT4 53-30-01 PG5 FIG2 | 1 | |
| NDT1039-.080/.063 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-.080/.100 | Boeing Reference Standard 737 PT4 53-30-01 PG5 FIG2 | 1 | |
| NDT1039-0.016/0.016 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.016". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.016/0.020 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.020". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.016/0.025 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.025". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.016/0.100 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.100". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.020/0.020 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.016"/0.016". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.020/0.025 | BOEING REFERENCE STANDARD 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.020"/0.025". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.020/0.032 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.020"/0.032". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.025/0.025 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.030/0.030 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.030"/0.030". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.032/0.032 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.032"/0.032". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.032/0.036 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.032/0.050 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.032"/0.050". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.036/0.036 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.040/0.020 | BOEING REFERENCE STANDARD | 2 | |
| NDT1039-0.040/0.032 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.040/0.036 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.040/0.040 | BOEING REFERENCE STANDARD | 2 | |
| NDT1039-0.040/0.050 | BOEING REFERENCE STANDARD BOEING REFERNCE STANDARD 737 PT4 53-30-01, 767 PT 4 51-00-05 FIGURE 2, PAGE 7. 2000 SERIES ALUMINUM 0.040"/0.050". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.040/0.056 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.045/0.040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.050/0.040 | BOEING REFERENCE STANDARD | 2 | |
| NDT1039-0.050/0.056 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.050/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.050/0.080 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.063/0.040 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.063/0.056 | BOEING REFERENCE STANDARD | 2 | |
| NDT1039-0.063/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.063/0.080 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 PAGE 5 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.071/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.080/0.025 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.080/0.063 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1039-0.080/0.100 | BOEING REFERENCE STANDARD 737 PT 4 53-30-01 FIGURE 2 and 767 PT 4 51-00-05 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1039-0.52/0.52 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2, T1= .52mm T2=.52mm | 1 | |
| NDT1039-1.0/0.5 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-1.0/1.0 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-1.3/1.1 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-1.3/1.6 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-1.6/0.5 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-1.6/1.4 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-1.6/1.6 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2 | 1 | |
| NDT1039-2.0/1.6 | Boeing Reference Standard, 737 PT4 53-30-01:PG5 FIG2, (.080/.063) size in mm | 1 | |
| 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. | 2 | |
| NDT1040 | BOEING REFERENCE STANDARD 737 PT 6 51-00-00. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1041 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.250” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1042 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.313” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1043 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1043CS | BOEING COUNTERSINK REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER 100° COUNTERSINK HOLE. MATERIAL: 43404340M STEEL. SIZE: 2.0" X .375" THICK( ROUNDSQUARE. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 1 | |
| NDT1044 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.438” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1045 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.500” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1046-8/NDT1046-3 | FIBERGLASS SKIN REFERENCE STANDARD, 8 PLIES AND 3 PLIES | 1 | |
| 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. | 3 | |
| NDT1048 | BOEING REFERENCE STANDARD 51-00-01 PT 6 FIG 5. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT1061 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13. Includes Test Report and Certificte of Conformance. | 2 | |
| NDT1062 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 24. Includes Test Report and Certificte of Conformance. | 2 | |
| NDT1069A | BOEING REFERENCE STANDARD 737 pt 6 53-30-19 FIGURE 3 SHEET 1 PAGE 9. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1069B | BOEING REFERENCE STANDARD 737 PT 6 53-30-19 FIGURE 3 SHEET 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1071 | BOEING REFERENCE STANDARD 767 Part 4 51-00-22 Page 4 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 2 | |
| NDT1073 | BOEING REFERENCE STANDARD Part 6 51-00-00 Page 12 Figure 13. Material:4130 or 4340. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1074 | BOEING REFERENCE STANDARD Part 6 51-00-00 Page 11 Figure 24. Material: 304 1/2 Hard. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1075 | BOEING REFERENCE STANDARD Part 6 51-00-00 Page 14 Figure 13. Material: 301 1/2 Hard. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1083 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1083-.157 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-.5625 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-.630 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.5620 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.563 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.625 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.630 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.688 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.695 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.750 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 2 | |
| NDT1083-0.787 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.812 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.813 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.875 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.938 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-1.000 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-1.286 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-1.347 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-3.2/8.7 | REFERENCE STANDARD BOEING 12 HOLE | 1 | |
| NDT1083.157 | Boeing Reference Standard 0.157" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1083.219 | Boeing Reference Standard 0.219" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1083.282 | Boeing Reference Standard 0.282" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1083.344 | Boeing Reference Standard 0.344" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1083.407 | Boeing Reference Standard 0.407" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1083.469 | Boeing Reference Standard 0.469" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1083.516 | Boeing Reference Standard 0.516" Hole, 51-00-00, PT6: Fig.19, Page 10, Detail III | 1 | |
| NDT1084 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-.0625 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII, .0625 (1/16") Diameter Hole | 2 | |
| NDT1084-.096 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-.125 | BOEING REFERENCE STANDARD PT6 51-00-00 FIG 3 PG6 | 2 | |
| NDT1084-.531 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084-.5625 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-.750 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII .750" hole diameter | 1 | |
| NDT1084-.813 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084-.875 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII .875" hole diameter | 1 | |
| NDT1084-.938 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084-0.09375 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.122 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.125 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.127 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.129 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.156 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 2 | |
| NDT1084-0.157 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.161 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.200 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.218 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.219 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 2 | |
| NDT1084-0.234 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.265 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.281 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.297 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.328 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.359 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.391 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.422 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.453 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.469 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.484 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.531 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.562 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.563 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.578 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.594 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.600 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.625 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 2 | |
| NDT1084-0.630 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.640 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.656 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.675 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.688 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.689 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.695 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.700 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.719 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.750 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 2 | |
| NDT1084-0.787 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.813 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.875 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.906 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.938 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0.XXX | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-0125 | BOEING REFERENCE STANDARD 737 PART 6 51-00-00 PAGE 9 FIGURE 3, 777 PART 6 51-00-02 PAGE 7 FIGURE 3,777-200/300 PART 6 51-00-02 PAGE 9 FIGURE 3. MATERIAL: 2024-T3. PROCUDURES VARY WITH PLANE MODEL. ALL MODELS FOR THIS REFERENCE STANDARD. PROVIDE CUSTOM | 1 | |
| NDT1084-1.00 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.0" hole diameter | 2 | |
| NDT1084-1.000 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.062 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.100 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.124 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.125 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.125" hole diameter | 2 | |
| NDT1084-1.187 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.200 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.200" hole diameter | 1 | |
| NDT1084-1.250 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.250" hole diameter | 1 | |
| NDT1084-1.300 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.312 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.3605 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.375 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.375" hole diameter | 2 | |
| NDT1084-1.390 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.390" hole diameter | 1 | |
| NDT1084-1.400 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.420 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.420" hole diameter | 1 | |
| NDT1084-1.437 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.500 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.500" hole diameter | 1 | |
| NDT1084-1.590 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.590" hole diameter | 1 | |
| NDT1084-1.625 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.625" hole diameter | 2 | |
| NDT1084-1.750 | Boeing Reference Standard,737 PT6 51-00-00: FIG16 PG10 DETAILIII, 1.75" hole diameter | 1 | |
| NDT1084-1.750-7075T6 | Boeing Reference Standard,737 PT6 51-00-00: FIG16 PG10 DETAILIII, 7075T6 Aluminum | 1 | |
| NDT1084-1.795 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.795" hole diameter | 1 | |
| NDT1084-1.875 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.875" hole diameter | 1 | |
| NDT1084-1.940 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-1.985 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 1.985" hole diameter | 1 | |
| NDT1084-1.9855 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-11.5MM | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-14.4MM | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-14.6MM | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-17.4MM | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-17.5MM | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-2.00 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 2.0" hole diameter | 1 | |
| NDT1084-2.000 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-2.250 | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-2.650 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII 2.650" hole diameter | 1 | |
| NDT1084-27.6MM | BOEING REFERENCE STANDARD 737 Part 6 51-00-00 Page 9 Figure 3, 777 Part 6 51-00-02 Page 7 Figure 3, or 777-200/300 Part 6 51-00-02 Page 9 Figure 3. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom | 1 | |
| NDT1084-3.2/8.7 | REFERENCE STANDARD BOEING 12 HOLE | 1 | |
| NDT1084.125 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 2 | |
| NDT1084.156 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.157 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 2 | |
| NDT1084.158 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.188 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.195 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.218 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.219 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.245 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.250 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.275 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.281 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.282 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.297 | Boeing Reference Standard, 19/64" Hole, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.313 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.343 | Boeing Reference Standard, 11/32" Hole, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.344 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.407 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIIII | 1 | |
| NDT1084.469 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.500 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.531 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.547 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.562 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.625 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.688 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.750 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1084.875 | Boeing Reference Standard, PT6 51-00-00: FIG16 PG10 DETAILIII | 1 | |
| NDT1085-032 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1085-036 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1085-050 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-063 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-071 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-080 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-090 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-100 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-112 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1085-125 | BOEING REFERENCE STANDARD 767 PT 6 53-00-10, 737 PART 6 53-30-23. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1086-032 | Boeing Reference Standard | 3 | |
| NDT1086-040 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-050 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-060 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-070 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-080 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-090 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-100 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-110 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1086-120 | BOEING REFERENCE STANDARD 767 PT 4 53-00-01 and 737 53-30-05. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1087-1 | REFERENCE STANDARD PT6 B737 | 4 | |
| NDT1087-10 | BOEING REFERENCE STANDARD, 767 PT6 53-30-11, PG.7-9, .132"/.056". Includes Certification Report. | 2 | |
| NDT1087-11 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.140 / Lower 2 - 0.080. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-12 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.120 / Lower 2 - 0.063. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-13 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.140 / Lower 2 - 0.063. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-14 | BOEING REFERENCE STANDARD, 757 Part 6 53-00-11. Plate Thickness: Upper 1 - 0.160 / Lower 2 - 0.100. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1087-2 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT 6 53-30-09. .071/.040. INCLUDES NDT1087-P1 POSITIONERS. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1087-3 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT 6 53-30-09, .080/.040. INCLUDES NDT1087-P1 POSITIONERS. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1087-4 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .090/.040. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1087-5 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .100/.050. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-6 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .071/.063. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-7 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .090/.080. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-8 | BOEING REFERENCE STANDARD 737 PT 6 53-30-00 & 777 PT6 53-30-09 .100/.090). Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1087-9 | BOEING REFERENCE STANDARD,. Includes Certification Report. | 2 | |
| 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 | 3 | |
| NDT1088-036X2/050-B | Boeing Reference Standard, Bare, Drawing Provided | 1 | |
| NDT1088-036X2/050-C | Boeing Reference Standard, Drawing Provided | 1 | |
| NDT1088-050/063 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 1 | |
| NDT1088-062/071 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 1 | |
| NDT1088-072/050 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 4 | |
| NDT1088-095/071 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 1 | |
| NDT1088-112/100 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 2 | |
| NDT1088-133/071 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 1 | |
| NDT1088-144/050 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 3 | |
| NDT1088-156/100 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 1 | |
| NDT1088-180/180 | BOEING REFERENCE STANDARD 737 Part 6 53-30-24 Page 6 Figure 2, 747 Part 6 53-30-17 Page 7 Figure 1, 757 Part 6 53-00-13 Page 6 Figure 2. Material: 2024-T3. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and | 1 | |
| NDT1089-.500 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-.626 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-.750 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-0.125 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16,BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø0.125" | 2 | |
| NDT1089-0.157 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø0.157" | 1 | |
| NDT1089-0.563 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance.Hole Ø 0.563" | 1 | |
| NDT1089-0.600 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. HOLE SIZE: 0.600". Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-0.625 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.625" | 1 | |
| NDT1089-0.626 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.626" | 1 | |
| NDT1089-0.656 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-0.660 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-0.688 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.688" | 1 | |
| NDT1089-0.750 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.750" | 1 | |
| NDT1089-0.813 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.813" | 1 | |
| NDT1089-0.875 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.875" | 1 | |
| NDT1089-0.938 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 0.938" | 1 | |
| NDT1089-1.000 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. Hole Ø 1.000" | 1 | |
| NDT1089-1.375 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-1.438 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-1.500 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16, MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1089-1.9855 | BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, PT 6 51-00-00 FIG 16. MATERIAL(6AL-4V) TITANIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1092-.040/.016 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2 .040/.016. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1092-.040/.032 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2 .040/.32. Includes Test Report and Certificate of Conformance | 1 | |
| NDT1092-.050/.040 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2, .050/.040. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1092-.071/.056 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2 .071/.056. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1092-.080/.040 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2 .080/.040. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1092-1.02/.8mm | Reference Standard 737 PT9 51-00-03 PG 9 FG 2, 1.02mm Top, .8mm Bottom | 1 | |
| NDT1093-.050/.040 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2. Material: 2024-T3 Aluminum .050"/.040" thicknesses. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1093-.071/.056 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2. Material: 2024-T3 Aluminum .071"/.056" thicknesses. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1093-.080/.040 | BOEING REFERENCE STANDARD 737 Part 9 51-00-03 Page 8 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1093-1.27/1.02mm | Reference Standard 737 PT9 51-00-03 PG 10 FG 3, 1.27mm Top, 1.02mm Bottom | 1 | |
| NDT1093-1.8/1.42mm | Reference Standard 737 PT9 51-00-03 PG 10 FG 3, 1.8mm Top, 1.42mm Bottom | 1 | |
| NDT1094-040 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-040-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-050 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-050-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-050/010-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-070 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-070-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-090 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-090-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-110 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-110-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-130 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-130-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-155 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-155-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-185 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-185-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-215 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-215-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-245 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-245-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-275 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-275-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 2 | |
| NDT1094-300 | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1094-300-A | BOEING REFERENCE STANDARD 737 Part 4 53-30-07, 757 Part 4 53-00-02 FIG 2, 777 Part 4 53-00-02 Page 34 Figure 2. Material: Aluminum. Procudures vary with Plane Model. All Models for this Reference Standard. Includes Test Report and Certificate of Conforman | 1 | |
| NDT1096-040 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-040-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-050 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-050-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-070 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-070-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-090 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-090-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-110 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-110-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-130 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-130-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-155 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-155-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-185 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-185-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-215 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-215-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-245 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-245-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-275 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-275-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-300 | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1096-300-A | BOEING REFERENCE STANDARD 757,767, 777 PART 4 53-00-03 and PART 4 53-30-08 707,727,737,747. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1097-A | BOEING REFERENCE STANDARD PT 6 53-30-25 FIG 2. Includes Certification Report and Certificate of Conformance. | 2 | |
| NDT1097-B | BOEING REFERENCE STANDARD PT 6 53-30-25 FIG 2. Includes Certification Report and Certificate of Conformance. | 2 | |
| NDT1097-C | BOEING REFERENCE STANDARD PT 6 53-30-25 FIG 2. Includes Certification Report and Certificate of Conformance. | 2 | |
| NDT1097B | NDT1097B Reference standard | 2 | |
| NDT1099 | BOEING REFERENCE STANDARD 757 PT 6 53-30-14 Page 5 Figure 1. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT1099G-P1 | BEOING REFERENCE STANDARD 757 Part 4 53-30-04 Page 15-17 Figure 3. Material: Delrin. *** SEE FINALIZED DRAWING*** | 1 | |
| NDT1102-100 | BOEING REFERENCE STANDARD 787 Part 6 51-00-11 Page 5 Figure 1. Material:Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1102-200 | BOEING REFERENCE STANDARD 787 Part 6 51-00-11 Page 5 Figure 1. Material:Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1102-300 | BOEING REFERENCE STANDARD 787 Part 6 51-00-11 Page 5 Figure 1. Material:Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1102-400 | BOEING REFERENCE STANDARD 787 Part 6 51-00-11 Page 5 Figure 1. Material:Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1102-500 | BOEING REFERENCE STANDARD 787 Part 6 51-00-11 Page 5 Figure 1. Material:Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1102-600 | BOEING REFERENCE STANDARD 787 Part 6 51-00-11 Page 5 Figure 1. Material:Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT1106 | Boeing Reference Standard composite..737 PT4 51-00-05 PG 5-6 FG 1 | 2 | |
| NDT1106-1 | Boeing Reference Standard composite..737 PT4 51-00-05 PG 5-6 FG 1 With top plate thickness of .060", .080" .100".. | 1 | |
| NDT126 | BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4. INC | 1 | |
| NDT17031A | BOEING REFERENCE STANDARD 777-200/300 PART 4 57-20-14 PAGE 6 FIGURE 2. MATERIAL: 7055-T7751,AIRPLANE QUALITY ALUMINUM. INCLUDES TEST REPORT AND CE | 1 | |
| NDT17031B | BOEING REFERENCE STANDARD 777-200/300 PART 4 57-20-15 PAGE 11-12 FIGURE 2, SHEET 1&2 AND PART 4 57-20-13 PAGE 6 FIGURE 2. MATERIAL: 7055-T7751,AIR | 1 | |
| NDT17031C | BOEING REFERENCE STANDARD 777-200/300 PART 4 57-20-15 PAGE 13 FIGURE 2, SHEET 3. MATERIAL: 7055-T7751,AIRPLANE QUALITY ALUMINUM. INCLUDES TEST RE | 1 | |
| NDT185 | BOEING REFERENCE STANDARD | 1 | |
| NDT188A | REFERENCE STANDARD BLOCO PADR?O | 1 | |
| NDT194B | Reference Standard NDT194B | 2 | |
| NDT194C | BOEING REFERENCE STANDARD 737 Part 6 53-30-00 Page 10 Figure 6. MATERIAL: 2024-T3 OR T4 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT2009 | BOEING REFERENCE STANDARD 727 Part 4 57-10-27 Page 10 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2015 | BOEING REFERENCE STANDARD 727 PT 4 54-30-27. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2016 | BOEING REFERENCE STANDARD 727 Part 6 54-40-27 Page 5 Figure 1. Material: 6AL-4V and 4130, 4330, or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT2019 | BOEING REFERENCE STANDARD 727 PT 6 57-40-27 DETAIL II. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2024 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 Page 4 Figure 1. Material: 2024-T3 or T4 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2025 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 Page 4 Figure 1. Material: 2024-T3 or T4 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2026 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 Page 4 Figure 1. Material: 2024-T3 or T4 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2027 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 Page 4 Figure 1. Material: 2024-T3 or T4 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2028 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 Page 4 Figure 1. Material: 2024-T3 or T4 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2029 | BOEING REFERENCE STANDARD 727 Part 6 53-30-27 Page 4 Figure 1. Material: 2024-T3 or T4 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2031 | BOEING REFERENCE STANDARD 727 PART 6 55-30-27 FIGURE 3 PAGE 22. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT2032-A | BOEING REFERENCE STANDARD 727 Part 6 57-10-28 Page 7 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT297 | BOEING REFERENCE STANDARD 727 PART 4 32-30-27 PROCEDURE 5 PAGE 10 FIGURE 1. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT298 | BOEING REFERENCE STANDARD 727 PART 4 32-30-27 PROCEDURE 5 PAGE 11 FIGURE 1. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3001 | BOEING REFERENCE STANDARD 737 Part 4 53-10-02 Page 8 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3004 | BOEING REFERENCE STANDARD PART 6 53-30-10 FIGURE 2 (SHEET1&2) PAGE 9&10. | 3 | |
| NDT3005 | BOEING REFERENCE STANDARD 737 Part 6 53-30-13 Page 5 Figure 1. Material: 2024-T3 or T4. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3008 | BOEING REFERENCE STANDARD 737 Part 6 54-40-01 Page 9 Figure 2. Material: 4330 or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3009 | BOEING REFERENCE STANDARD 737 Part 6 54-40-01 Page 9 Figure 2. Material: 4330 or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3010 | BOEING REFERENCE STANDARD 737 Part 6 54-40-01 Page 9 Figure 2. Material: 4330 or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3011 | BOEING REFERENCE STANDARD 737 Part 6 53-30-10 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3012 | BOEING REFERENCE STANDARD 737 Part 4 53-10-03 Page 8 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3014-A | BOEING REFERENCE STANDARD 737 Part 4 27-00-01 Page 13 Figure 5. Material: 7075-T6 or T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3014-B | BOEING REFERENCE STANDARD 737 Part 4 27-00-01 Page 13 Figure 5. Material: 7075-T6 or T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3015 | BOEING REFERENCE STANDARD 737 Part 6 53-30-15 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3016B | BOEING REFERENCE STANDARD 737 PT6 53-10-54 PG 7 FG 2 | 1 | |
| NDT3019 | BOEING REFERENCE STANDARD 737 PT 6 53-30-16 FIG 1 & 727 PT 6 53-30-27 FIG.17 SHEET 5 PAGE 115. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3021 | BOEING REFERENCE STANDARD | 6 | |
| NDT3023 | BOEING REFERENCE STANDARD 737 PT 4 32-10-02 FIG 5. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT3023P1 | BOEING REFERENCE STANDARD TRANSDUCER POSITIONER TRANSDUCER POSITIONER TRANSDUCER POSITIONER CONTACT TRANSDUCER | 4 | |
| NDT3023P2 | BOEING REFERENCE STANDARD TRANSDUCER POSITIONER TRANSDUCER POSITIONER TRANSDUCER POSITIONER CONTACT TRANSDUCER | 4 | |
| NDT3023P3 | BOEING REFERENCE STANDARD TRANSDUCER POSITIONER TRANSDUCER POSITIONER TRANSDUCER POSITIONER CONTACT TRANSDUCER | 4 | |
| NDT3024A | BOEING REFERENCE STANDARD 737 PT 4 53-10-04. Includes test report and Certificate of Conformance. | 2 | |
| NDT3030 | BOEING REFERENCE STANDARD 737 PT 4 57-10-01 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3038 | BOEING REFERENCE STANDARD 737 57-50-02 PT 4 FIG 4. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT3039 | BOEING REFERENCE STANDARD 737 53-30-04 PT 4 FIG 2 SHEETS 1&2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3041 | BOEING REFERENCE STANDARD PT 6 57-50-15 PAGE 7 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3046 | BOEING REFERENCE STANDARD 767 PT 4 53-20-01. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3048D | BOEING REFERENCE STANDARD 737 PART 6 53-10-56 FIGURE 4. | 1 | |
| NDT3049 | BOEING REFERENCE STANDARD 737 PT 6 53-10-67. Includes test report and Certificate of Conformance. | 2 | |
| NDT3050 | BOEING REFERENCE STANDARD PT 6 53-30-20 FIG 2. Includes Test Report and Certificate of Conformance. (SCREW AND NUT) | 4 | |
| NDT3052 | BOEING REFERENCE STANDARD 737 Part 6 57-10-26 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3053 | BOEING REFERENCE STANDARD 737 Part 6 53-30-21 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3054 | BOEING REFERENCE STANDARD 737 Part 4 57-10-04 Page 12 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3062 | BOEING REFERENCE STANDARD 737 Part 4 57-10-02 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3065 | BOEING REFERENCE STANDARD 767 PT 6 53-00-12 FIG 2.707, 727, 737, 747 Aircrafts; Part 6, 53-30-22. On 737 Aircraft; Part 4, 53-30-06. On 757, 767 Aircrafts; Part 6, 53-00-09. On 777 Aircraft; Part 6,53-00-07. Includes Test Report and certificate of Conform | 3 | |
| NDT3065-STL | BOEING REFERENCE STANDARD 777 Part 6 53-00-07 Page 8 Figure 3. Material: Aluminum and 301 1/2 Hard. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3068 | BOEING REFERENCE STANDARD 52-10-02 PT 4 FIG 2. Includes Test Report and Certificate of Conformance. | 5 | |
| NDT3070 | BOEING REFERENCE STANDARD 737 Part 6 57-10-30 Page 4 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3071A and NDT3071B | BOEING REFERENCE STANDARD 737 Part 6 53-10-65 Page 11 Figure 2. Material: 2024-T3 Bare or Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3073 | BOEING REFERENCE STANDARD 737 Part 6 57-10-31 Page 8 Figure 2. Material: 2024-T3 or T4. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3075 | BOEING REFERENCE STANDARD 727 Part 6 53-30-26 Page 7 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3077 | BOEING REFERENCE STANDARD 737 Part 6 53-10-69 Page 13 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3078 | BOEING REFERENCE STANDARD 737 Part 6 53-10-38 Page 9 Figure 4. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3080 | BOEING REFERENCE STANDARD 737 Part 4 55-30-02 Page 10 Figure 3. Material: 2024-T3, 7050 or 7075. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3080-A | Boeing Reference Standard, .700 x .350 Thumbnail | 1 | |
| NDT3080-B | Boeing Reference Standard, .400 corner notch | 1 | |
| NDT3081 | BOEING REFERENCE STANDARD 737 PT 4 55-10-01 FIG 4. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3082A | Boeing reference standard | 2 | |
| NDT3082B | Boeing reference standard | 2 | |
| NDT3082C | Boeing reference standard | 2 | |
| NDT3083 | BOEING REFERENCE STANDARD 737 Part 4 55-10-03 Page 14 Figure 3. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3085A | BOEING REFERENCE STANDARD 737 Part 6 57-10-32 Page 8 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3085B | BOEING REFERENCE STANDARD 737 Part 6 57-10-32 Page 8 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3085C | BOEING REFERENCE STANDARD 737 Part 6 57-10-32 Page 8 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3086A | BOEING REFERENCE STANDARD 737 Part 6 57-10-32 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3086B | BOEING REFERENCE STANDARD 737 Part 6 57-10-32 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3086C | BOEING REFERENCE STANDARD 737 Part 6 57-10-32 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3090A | Boeing Reference Standard, 737 PT6 53-10-52:FIG2 PG5 | 1 | |
| NDT3090B | Boeing Reference Standard, 737 PT6 53-10-52:FIG3 PG6 | 1 | |
| NDT3090C | Boeing Reference Standard, 737 PT6 53-10-52:FIG3 PG6 | 1 | |
| 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. | 2 | |
| NDT3092 | BOEING REFERENCE STANDARD 53-10-05 PT 4 FIG 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3094 | BOEING REFERENCE STANDARD 737 Part 4 55-10-24 Page 14 Figure 4. Material: 2000 or 7000 Series Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3098 | BOEING REFERENCE STANDARD 737 Part 4 55-10-07 Page 6 Figure 2. Material: Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3099 | BOEING REFERENCE STANDARD 737 Part 4 55-10-06 Page 8 Figure 2. Material: Ti-6AL-4V. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3100 | BOEING REFERENCE STANDARD 737 PT 4 55-10-08. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3101 | BOEING REFERENCE STANDARD 737 PT 4 55-10-12 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3102 | BOEING REFERENCE STANDARD 737 PT 4 55-10-10 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3104 | BOEING REFERENCE STANDARD 737 PT 4 55-10-04 FIG 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3105 | BOEING REFERENCE STANDARD 737 PT 4 55-10-15 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3106 | BOEING REFERENCE STANDARD 737 PT 6 55-10-30 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3107 | BOEING REFERENCE STANDARD 737 PT 4 55-10-09 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3109 | BOEING REFERENCE STANDARD 737 PT 4 53-80-01 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3111 | BOEING REFERENCE STANDARD 737 PT 4 55-10-05 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3112 | BOEING REFERENCE STANDARD 737 Part 4 57-50-05 Page 7 Figure 2. Material: 15-5 Steel. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3113 | Boeing Reference Standard | 1 | |
| NDT3114 | BOEING REFERENCE STANDARD 737 PART 6 53-30-31 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3115 | BOEING REFERENCE STANDARD 737 PART 6 53-30-31 FIGURE 1 PAGE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3116 | BOEING REFERENCE STANDARD 737 PT 4 53-10-06 FIG 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3117 | BOEING REFERENCE STANDARD 737 Part 5 54-40-03 Page 7 Figure 2. Material: 4330M or 4340M and 6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3118 | Boeing Reference Standard, 737 PT6 52-30-01:FIG3 PG6, BACB30FN6-2 or -3 fasteners | 3 | |
| NDT3118/MF | Boeing Reference Standard, 737 PT6 52-30-01:FIG3 PG6, BACB30FN6-2 or -3 fastners | 1 | |
| NDT3119 R&D | Boeing Reference Standard | 1 | |
| NDT3120 | BOEING REFERENCE STANDARD, 737 PT6 55-10-28: FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3121 | BOEING REFERENCE STANDARD, 737 PT6 55-10-28: FIGURE 3 PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3122 | BOEING REFERENCE STANDARD 737 PART 4 55-10-20 PAGE 14 FIGURE 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3123 | BOEING REFERENCE STANDARD 737 PART 4 55-10-20 PAGE 15 FIGURE 3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3124 | BOEING REFERENCE STANDARD 737 PART 4 55-10-20 PAGE 16 FIGURE 4. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3125 | BOEING REFERENCE STANDARD PART 4 55-10-25 FIGURE 2 PAGE 18. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3126 | BOEING REFERENCE STANDARD PART 4 55-10-25 FIGURE 3 PAGE 19. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3127 | BOEING REFERENCE STANDARD PART 4 55-10-25 FIGURE 4 PAGE 20. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3129 | BOEING REFERENCE STANDARD Part 6 53-30-38 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3130 | BOEING REFERENCE STANDARD 737, PART 6 53-30-37 PAGE 8 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3131 | BOEING REFERENCE STANDARD 737 Part 6 53-11-10 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3132 | BOEING REFERENCE STANDARD 737 Part 6 53-11-18 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3132B | BOEING REFERENCE STANDARD 737 Part 6 53-11-18 page 8 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3133 | BOEING REFERENCE STANDARD 737 Part 6 53-11-16 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3134 | Boeing Reference Standard | 1 | |
| NDT3136 | BOEING REFERENCE STANDARD 737 Part 4 55-10-14 Page 6 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3137 | BOEING REFERENCE STANDARD 737 Part 6 57-50-03 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3139 | BOEING REFERENCE STANDARD 737 9T 4 53-10-07. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3141 | REFERENCE STANDARD BOEING | 2 | |
| NDT3142 | BOEING REFERENCE STANDARD 737 Part 6 53-11-08 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3144 | BOEING REFERENCE STANDARD 737 Part 4 55-10-16 Page 6 Figure 2. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3145 | BOEING REFERENCE STANDARD 737 Part 4 55-10-16 Page 7 Figure 3. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3146 | BOEING REFERENCE STANDARD 737 Part 4 55-10-16 Page 8 Figure 4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3147 | BOEING REFERENCE STANDARD 737 PART 4 53-30-10 PAGE 7 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3149 | BOEING REFERENCE STANDARD 737 Part 6 53-30-41 Page 6 Figure 2. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3151 | BOEING REFERENCE STANDARD 737 PT 6 53-30-46 PAGE 7 FIGURE2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3152- H | BOEING REFERENCE STANDARD 737 PART 6 57-10-55 PAGE 8 FIGURE 2. MATERIAL: 2024-T3. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 3 | |
| NDT3152-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-D | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-E | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-F | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-G | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-H | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-I | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-J | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3152-K | BOEING REFERENCE STANDARD 737 Part 6 57-10-55 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-D | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-E | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-F | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-G | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-H | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3153-J | BOEING REFERENCE STANDARD 737 Part 6 57-10-54 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3156 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 2024-T3. Includes test report and Certificate of Conformance. | 4 | |
| NDT3157 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 7150-T7. Includes test report and Certificate of Conformance. | 4 | |
| NDT3159 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 2024-T3. Includes test report and Certificate of Conformance. | 4 | |
| NDT3161 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 2024-T3. Includes test report and Certificate of Conformance. | 3 | |
| NDT3162 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 7150-T7. Includes test report and Certificate of Conformance. | 4 | |
| NDT3163 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 7150-T7. Includes test report and Certificate of Conformance. | 2 | |
| NDT3164 | BOEING REFERENCE STANDARD 737 Part 6 57-10-60 Page 11 Figure 2. Material: 7150-T7. Includes test report and Certificate of Conformance. | 3 | |
| NDT3166-001 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3166-002 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3166-003 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3166-004 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3166-005 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3166-006 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT3166-007 | BOEING REFERENCE STANDARD 737 Part 4 57-10-08 Page 6 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT3167-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-D | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-E | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-F | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-G | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-H | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3167-J | BOEING REFERENCE STANDARD 737 Part 6 57-10-58 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3168 | BOEING REFERENCE STANDARD 737 Part 6 57-10-53 Page 6 Figure 2. Material: 7075-T7. Includes test report and Certificate of Conformance. | 3 | |
| NDT3169 | BOEING REFERENCE STANDARD 737 Part 6 57-10-48 Page 5 Figure 2. Material: 2024-T3. Includes test report and Certificate of Conformance. | 1 | |
| NDT3170 | BOEING REFERENCE STANDARD 737 Part 4 57-10-06 Page 16 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 5 | |
| NDT3171 | BOEING REFERENCE STANDARD 737 Part 4 57-10-06 Page 17 Figure 3. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 5 | |
| NDT3172 | BOEING REFERENCE STANDARD 737 Part 4 57-10-05 Page 14 Figure 2. Material: Aircraft Quality Aluminum. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3176-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-59 Page 12 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3176-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-59 Page 12 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3176-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-59 Page 12 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3176-D | BOEING REFERENCE STANDARD 737 Part 6 57-10-59 Page 12 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3176A-D | BOEING REFERENCE STANDARD | 1 | |
| NDT3178-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 2 | |
| NDT3178-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 2 | |
| NDT3178-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 3 | |
| NDT3178-D | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 3 | |
| NDT3178-E | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 2 | |
| NDT3178-F | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 2 | |
| NDT3178-G | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 2 | |
| NDT3178-X | BOEING REFERENCE STANDARD 737 Part 6 57-10-62 Page 8 Figure 2. Material: 2024-T3. Test Report and Certificate of Conformance. | 1 | |
| NDT3179-A | BOEING REFERENCE STANDARD 737 Part 6 53-30-39 Page 4 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3179-B | BOEING REFERENCE STANDARD 737 Part 6 53-30-39 Page 4 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3179-C | BOEING REFERENCE STANDARD 737 Part 6 53-30-39 Page 4 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-D | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-E | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-F | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-G | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-H | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3180-J | BOEING REFERENCE STANDARD 737 Part 6 57-10-61 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3181-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 page 9 Figure 2. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3181-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 page 9 Figure 2. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3182-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 Page 10 Figure 3. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3182-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 Page 10 Figure 3. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3183 | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 Page 11 Figure 4. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3184 | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 Page 12 Figure 5 | 1 | |
| NDT3185-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 Page 13 Figure 6. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3185-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-63 Page 13 Figure 6. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3186 | BOEING REFERENCE STANDARD 737 PT 4 57-10-17. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3187 | BOEING REFERENCE STANDARD 737 PT 4 57-10-17. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3189 | BOEING REFERENCE STANDARD 737 Part 4 55-10-18 Page 6 Figure 2. Material: 7075-T6, 2024 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3190-A | BOEING REFERENCE STANDARD 737 Part 6 55-10-45 Page 6 Figure 2. Material: 2024-T6, 7150-T7 or 7150-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3190-B | BOEING REFERENCE STANDARD 737 Part 6 55-10-45 Page 6 Figure 2. Material: 2024-T6, 7150-T7 or 7150-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3190-C | BOEING REFERENCE STANDARD 737 Part 6 55-10-45 Page 6 Figure 2. Material: 2024-T6, 7150-T7 or 7150-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3190-D | BOEING REFERENCE STANDARD 737 Part 6 55-10-45 Page 6 Figure 2. Material: 2024-T6, 7150-T7 or 7150-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3191 | BOEING REFERENCE STANDARD 737 Part 6 55-10-28 Page 6 Figure 2. Material: 2024-T3 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3192 | BOEING REFERENCE STANDARD 737 Part 6 55-10-28 Page 7 Figure 3. Material: 2024-T3 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3193 | BOEING REFERENCE STANDARD 737 PT 6 51-30-28 FIG 1. Includes Certification Report and Certificate of Conformance. | 1 | |
| NDT3194 | Boeing Metal reference Standard | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| NDT3195 | BOEING REFERENCE STANDARD 737 PT 4 55-10-17 PAGE 18 FIGURE 4. MATERIAL: 7075-T6 or EQUIVALENT AIRCRAFT QUALITY ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3196 | BOEING REFERENCE STANDARD 737 PT 4 55-10-17 PAGE 19 FIGURE 5. MATERIAL: 7075-T6 or EQUIVALENT AIRCRAFT QUALITY ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3197 | BOEING REFERENCE STANDARD 737 PT 4 55-10-17 PAGE 20 FIGURE 6. MATERIAL: 7075-T6 or EQUIVALENT AIRCRAFT QUALITY ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3202-A | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3202-B | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3202-C | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3202-D | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3202-E | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3202-F | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3202-G | BOEING REFERENCE STANDARD 737 Part 6 55-10-53 Page 9 Figure 2. Material: 2024-T3 or Equivalent with a Conductivity of 28-32 IACS. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3204 | BOEING REFERENCE STANDARD 737 Part 4 53-10-08 Page 9 Figure 2. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3207 | BOEING REFERENCE STANDARD 737 Part 6 55-10-50 Page 5 Figure 2. Material: 7075-T6 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3207A | BOEING REFERENCE STANDARD 737 Part 6 55-10-82 Paqe 5 Figure 2. Material: 7075-T6 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3208-C | BOEING REFERENCE STANDARD 737 Part 6 55-10-55 Page 6 Figure 3. Material: Carbon Fiber and 2024-T3 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3209-A | BOEING REFERENCE STANDARD PART 6 55-10-62 PAGE 17 FIGURE 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3209A | BOEING REFERENCE STANDARD 737 Part 6 55-10-74 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3210 | BOEING REFERENCE STANDARD 737, PART 6: 57-10-81, PAGE 8 FIGURE 2. Includes test report and Certificate of Conformance. | 1 | |
| NDT3211 | BOEING REFERENCE STANDARD B737 NDTM P6, 57-10-81, PAGE 9 FIGURE 3. Includes test report and Certificate of Conformance. | 1 | |
| NDT3212 | BOEING REFERENCE STANDARD B737 NDTM P6, 57-10-81 PAGE 10 FIGURE 4. Includes test report and Certificate of Conformance. | 1 | |
| NDT3214 | BOEING REFERENCE STANDARD PT 4 53-10-09 FIGURE 2 PAGE 6. Includes test report and Certificate of Conformance. | 1 | |
| NDT3217-A | BOEING REFERENCE STANDARD 737, PART 6: 57-10-79. Includes test report and Certificate of Conformance. | 1 | |
| NDT3217-B | BOEING REFERENCE STANDARD 737, PART 6: 57-10-79. Includes test report and Certificate of Conformance. | 1 | |
| NDT3218 | BOEING REFERENCE STANDARD 737, PART 6 55-10-53 FIGURE 3 PAGE 10. Includes test report and Certificate of Conformance. | 2 | |
| NDT3219 | BOEING REFERENCE STANDARD 737 PART 4 57-10-19 PAGE 11 FIGURE 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3220 | BOEING REFERENCE STANDARD 737 PART 4 57-50-04 | 1 | |
| NDT3221 | BOEING REFERENCE STANDARD 737 Part 4 55-10-19 Page 6 Figure 2. Material: 2024-T3 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3223 | BOEING REFERENCE STANDARD 737 Part 6 55-11-34 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3224 | BOEING REFERENCE STANDARD 737 Part 4 54-40-01 Page 7 Figure 3. Material: 15-5PH or 4330. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3225 | BOEING REFERENCE STANDARD 737 Part 6 54-40-20 Page 6 Figure 2. Material: 6AL-4V and 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3226 | BOEING REFERENCE STANDARD 53-11-39 PART 6. MATERIAL: 2024-T3 ALUMINUM. 2. Includes Test Report and Certificate of Conformance.BACR15FT6D RIVETS BUCKED BETWEEN .250"Ø and .280"Ø. | 2 | |
| NDT3226A | BOEING REFERENCE STANDARD 737 Part 6 53-11-39 Page 5 Figure 2. Material: 2024-T4 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3227 | BOEING REFERENCE STANDARD 737 Part 4 54-40-09 Page 6 Figure 2. Material: 15-5 PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3228-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-87 Page 7 Figure 2. Material: 7150-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3228-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-87 Page 7 Figure 2. Material: 7150-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3228-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-87 Page 7 Figure 2. Material: 7150-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3229 | BOEING REFERENCE STANDARD 737 PT6 53-30-50 FIGURE 2 PAGE 21. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT322A | BOEING REFERENCE STANDARD 737 Part 6 53-10-25 Page 4 Figure 1. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3230 | BOEING REFERENCE STANDARD 737 pt 4 53-30-11 page 8 figure 2. Includes test report and Certificate of Conformance. | 2 | |
| NDT3231 | BOEING REFERENCE STANDARD 737 Part 4 53-10-10 Page 10 Figure. Material: 2024 or 7075 series Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3232-A | BOEING REFERENCE STANDARD 737 Part 6 57-10-86 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3232-B | BOEING REFERENCE STANDARD 737 Part 6 57-10-86 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3232-C | BOEING REFERENCE STANDARD 737 Part 6 57-10-86 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3233 | BOEING REFERENCE STANDARD 737 Part 4 53-30-11 Page 8 Figure 2. Includes test report and Certificate of Conformance. | 2 | |
| NDT3234 | BOEING REFERENCE STANDARD 737 Part 6 57-10-89 Page 7 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3235 | BOEING REFERENCE STANDARD 737 Part 4 -54-40-05 Page 5 Figure 2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3236 | BOEING REFERENCE STANDARD 737 Part 6 57-10-85 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3237-0.040/0.010 | BOEING REFERENCE STANDARD 737 PT 4 53-30-12 FASTENER (BACR15GF5*). Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3237-0.050-0.015 | REFERENCE STANDARD BLOCO PADR?O | 1 | |
| NDT3237-0.050/0.015 | BOEING REFERENCE STANDARD 737 PT 4 53-30-12 FASTENER (BACR15GF5*). Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3237-0.130/0.020 | BOEING REFERENCE STANDARD 737 PT 4 53-30-12 FASTENER (BACR15GF5*). Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3238 | BOEING REFERENCE STANDARD 737 Part 4 55-10-23 Page 6 Figure 2. Material: 7050-T7 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3239 | BOEING REFERENCE STANDARD 737 Part 4 55-30-03 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3240 | BOEING REFERENCE STANDARD 737 Part 6 57-10-90 Page 6 Figure 3. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3242 | BOEING REFERENCE STANDARD 737 PT 4 54-40-03. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3243 | BOEING REFERENCE STANDARD 737 PT 4 54-40-04. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3244 | BOEING REFERENCE STANDARD 737 Part 6 53-11-42 Page 8 Figure 2. Material: 2024-T4 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3248 | BOEING REFERENCE STANDARD 737 Part 6 55-10-66 Page 5 Figure 2. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3249 | BOEING Reference Standard 551064 | 1 | |
| NDT3250 | BOEING Reference Standard 551064 | 1 | |
| NDT3251 | BOEING REFERENCE STANDARD 737 Part 6 52-30-02 page 5 Figure 2. Material: 7050-T7 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3252 | BOEING REFERENCE STANDARD 737 Part 4 52-10-03 Page 7 Figure 2. Material: 7050-T7 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3253 | BOEING REFERENCE STANDARD 737 Part 4 54-40-06 Page 7 Figure 2. Material: 15-5PH or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3254 | BOEING REFERENCE STANDARD 737 Part 4 54-40-06 Page 8 Figure 3. Material: 15-5PH or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3257 | BOEING REFERENCE STANDARD 737 Part 657-10-96 Page 7 Figure 2. Material: 7050-T7 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3258-B | BOEING REFERENCE STANDARD 737 Part 4 54-40-08 Page 6 Figure 2. Material: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3259 | BOEING REFERENCE STANDARD 737 Part 6 54-40-17 Page 8 Figure 2. Material: 6AL-4V, 15-5PH and 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3260 | BOEING REFERENCE STANDARD 737 Part 6 54-40-17 Page 9 Figure 3. Material: 6AL-4V, 15-5PH and 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3261 | BOEING REFERENCE STANDARD 737 Part 6 57-50-31 Page 9 Figure 2. Material: 2024-T3 and 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3262 | BOEING REFERENCE STANDARD 737 Part 4 54-40-17 Page 6 Figure 2. Material: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3263 | BOEING REFERENCE STANDARD 737 Part 6 57-50-31 Page 10 Figure 3. Material: 2024-T3 and 7075-T7. Inlcudes | 1 | |
| NDT3264 | BOEING REFERENCE STANDARD 737 Part 4 55-10-22 page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3265 | BOEING REFERENCE STANDARD 737 Part 655-10-70 Page 8 Figure 2. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3266 | BOEING REFERENCE STANDARD 737 Part 6 -57-10-96 Page 8 Figure 3. Material: 7050-T7 or Eqivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3267-.040/.040 | Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .040/.040. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT3267-.050/.040 | Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .050/.040. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT3267-.063/.056 | Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .063/.056. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT3267-.063/.063 | Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .063/.063. IncludesTest Report and Certificate of Conformance. | 1 | |
| NDT3267-.080/.063 | Boeing Bonded Reference Standard | 2 | |
| NDT3267-.080/.100 | Boeing Bonded Reference Standard 737 PT4 53-30-01 PG 6 FG 3, .080/.100. IncludesTest Report and Certificate of Conformance. | 1 | |
| NDT3267-T1/T2 | BOEING REFERENCE STANDARD NDT3267-T1/T2 X 1SET OF 4 PIECES | 1 | |
| NDT3268 | BOEING REFERENCE STANDARD 737 Part 4 53-10-11 Page 4 Figure 2. Material: 7075-T6 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3269 | BOEING REFERENCE STANDARD, PT6, 54-40-19 PAGE 12 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3271 | BOEING REFERENCE STANDARD 737 PART 4 55-10-27 FIGURE 2 SHEET 1&2 PAGE 12. MATERIAL: 6AL-4v Includes Test Report and Certificate of Conformance. MATERIAL: 6AL-4v TITANIUM. | 1 | |
| NDT3272 | BOEING REFERENCE STANDARD 737 PART 4 55-10-27 FIGURE 3 PAGE 14. MATERIAL: 6AL-4v. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3273A | BOEING REFERENCE STANDARD PART 6 55-10-84 PAGE 6 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3276 | BOEING REFERENCE STANDARD | 2 | |
| NDT3276A | REFERENCE STANDARD BOEING | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| 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. | 2 | |
| NDT3282 | BOEING REFERENCE STANDARD 737 PART 4 57-10-20 PAGE 7 FIGURE 2 . MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3285 | BOEING REFERENCE STANDARD 737 Part 6 53-30-63 Page 11 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3286 | BOEING REFERENCE STANDARD 787 Part 4 53-20-02 Page 7 Figure 2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3287 | BOEING REFERENCE STANDARD 787 Part 4 53-20-01 Page 7 Figure 2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3288 | BOEING REFERENCE STANDARD 787 Part 4 53-20-01 Page 7 Figure 2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3289 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3291 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3292 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3293 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3294 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3295 | BOEING REFERENCE STANDARD 737 Part 6 53-30-66 Page 6 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3296 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3297 | BOEING REFERENCE STANDARD 737 Part 6 53-30-64 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3298 | BOEING REFERENCE STANDARD 737 Part 6 53-30-66 Page 6 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3299 | BOEING REFERENCE STANDARD 737 Part 6 53-30-65 Page 8 Figure 2. Material: 2024-T3 and 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3300 | BOEING REFERENCE STANDARD 737 Part 6 5330-60 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3301A | REFERENCE STANDARD B737 NDTM P4 53-10-13 | 1 | |
| NDT3303 | BOEING REFERENCE STANDARD 737 PT 4 FIGURE 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3304 | BOEING 737 R&D REFERENCE STANDARD, 53-30-XX PART 6. MATERIAL: 2024-T3 CLAD, 1100 FOIL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3305A | BOEING REFERENCE STANDARD PART 4 53-10-64 PG.18, FIG. 5. MATERIAL: 2024-T42 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3305B | BOEING REFERENCE STANDARD PART 4 53-10-64 PG.18, FIG. 5. MATERIAL: 2024-T42 CLAD ALUMINUM. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT3307 | BOEING REFERENCE STANDARD 737 PART 6 57-11-05 PAGE 5 FIGURE 2 SHEET 1. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3308 | BOEING REFERENCE STANDARD 737 PART 6 57-11-05 PAGE 6 FIGURE 2 SHEET 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT3312 | BOEING REFERENCE STANDARD 737 PART 4 53-10-13 FIGURE 2 SHEET 1&2 | 2 | |
| NDT3316 | REFERENCE STANDARD FOR INSPECTION USE ON B737 AS PER B737 NDTM PART 4 53-10-16 | 2 | |
| NDT335 | REFERENCE STANDARD BLOCO PADR?O | 2 | |
| NDT363 | Boeing Reference Standard 737 53-30-03 PT6 PG3 | 1 | |
| NDT391 | BOEING REFERENCE STANDARD Part 6 53-10-51 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT392 | BOEING REFERENCE STANDARD 737 Part 4 53-30-03 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT394 | BOEING REFERENCE STANDARD 737 PT 6 54-30-01. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT396 | Boeing Reference Standard, 737 PT6 53-30-09:PG7 FIG 2 / 53-30-18:PG10 FIG2 | 6 | |
| NDT396-32/40 | BOEING REFERENCE STANDARD 737 PT 6 53-30-44 FIGURE 2 PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT396-36/36 | Boeing Reference Standard, 737 PT6 53-30-44, PG7 FIG 2, .036" Upper skin, .036 Lower skin | 1 | |
| NDT396-40/40 | Boeing Reference Standard, 737 PT6 53-30-44, PG7 FIG 2, .040" Upper skin, .040 Lower skin | 1 | |
| NDT396-45/40 | Boeing Reference Standard, 737 PT6 53-30-44, PG7 FIG 2, .045" Upper skin, .040 Lower skin | 1 | |
| NDT396-50/40 | Boeing Reference Standard, 737 PT6 53-30-44, PG7 FIG 2, .050" Upper skin, .040 Lower skin | 1 | |
| NDT396-56/40 | Boeing Reference Standard, 737 PT6 53-30-44, PG7 FIG 2, .056" Upper skin, .040 Lower skin | 1 | |
| NDT396B | Boeing Reference Standard | 1 | |
| NDT396C | Boeing Reference Standard | 1 | |
| NDT398 | BOEING REFERENCE STANDARD 737 PT 4 53-10-01. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4064 | BOEING REFERENCE STANDARD 747 Part 6 53-30-06 Page 4 Figure 1. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4116 | BOEING REFERENCE STANDARD 747 Part 4 54-40-02 Page 20 Figure 7. Material: 4330M or 4340M. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4150 | BOEING 747 COMPOSITE REFERENCE STANDARD PART 4 57-22-01 FIGURE 2. Includes C-Scan Report and Certificate of Conformance. | 1 | |
| NDT4151 | BOEING 747 REFERENCE STANDARD PART 4 57-10-17 FIGURE 3 PAGE 10. 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT4153 | BOEING 747 REFERENCE STANDARD PART 4 57-30-08 PAGE 6 FIGURE 2. PROCEDURE FOR INSPECTING CRACKED RIVET PART NUMBER BACR15FH10DD17 | 1 | |
| NDT4154 | BOEING REFERENCE STANDARD 747 PT 4 54-40-14 FIGURE 5 PAGE 19. Includes Test Report and Certificate of Conformance | 1 | |
| NDT4155 | BOEING REFERENCE STANDARD 747 PT 4 54-40-14 FIGURE 6 PAGE 20. Includes Test Report and Certificate of Conformance | 1 | |
| NDT4156 | BOEING REFERENCE STANDARD 747 PT 4 54-40-14 FIGURE 7 PAGE 21. Includes Test Report and Certificate of Conformance | 1 | |
| NDT4157 | BOEING REFERENCE STANDARD 747 PT 4 54-40-14 PAGE 22 FIGURE 8. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4170 | BOEING REFERENCE STANDARD 747 Part 4 53-30-02 Page 5 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4175 | BOEING REFERENCE STANDARD 747 PT 6 53-10-41 Page 12 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4176 | BOEING REFERENCE STANDARD 747 PT 6 53-10-41 Page 13 Figure 3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4178 | BOEING REFERENCE STANDARD 747 Part 4 53-40-05 Page 4 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4180 | Boeing Reference Standard, 747 57-10-37 part 6, page 8 | 1 | |
| NDT4183 | Boeing Bonded Reference Standard, PT4, 53-30-03, PG11, FIG2 | 1 | |
| NDT4187 | BOEING 747 REFERENCE STANDARD PART 4 57-10-18 FIGURE 2 PAGE 8. 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4190 | BOEING REFERENCE STANDARD 747 PT 6 53-10-34 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4190A | BOEING REFERENCE STANDARD 747 PT 6 53-10-34 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4205 | BOEING REFERENCE STANDARD 747 PT 4 57-40-07 PAGE 5 FIGURE 2. MATERIAL: 4340 STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4208 | BOEING REFERENCE STANDARD 747 PART 4 54-40-23 FIGURE 2 PAGE 8. Includes Certification Report and Certificate of Conformance. | 2 | |
| NDT4209 | BOEING REFERENCE STANDARD 747 PT 4 53-10-08 PAGE 12. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4211 | BOEING REFERENCE STANDARD 747 PT 4 53-10-08 PAGE 12. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4212 | BOEING REFERENCE STANDARD 747 PT 4 53-10-09 Page 5 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4217 | Boeing Reference Standard, 747 PT6 53-30-14:PG6 FIG1 | 1 | |
| NDT4218A | BOEING METAL REFERENCE STANDARD | 1 | |
| NDT4219 | BOEING REFERENCE STANDARD 747 Part 4 53-10-11 Page 9 Figure 2. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4220 | BOEING REFERENCE STANDARD 747 Part 6 53-30-13 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4221 | BOEING 747 REFERENCE STANDARD PART 6 53-30-12 PAGE 5 FIGURE 2. MATERIAL: 2024-T3 Bare or Clad Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4225 | BOEING 747 REFERENCE STANDARD PART 6 53-10-47 PAGE 7 FIGURE 2. MATERIAL: 7075-T6 or 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4226 | BOEING REFERENCE STANDARD 747 Part 4 57-10-22 Page 6 Figure 2, Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT4229 | BOEING REFERENCE STANDARD PT 6 54-40-16 FIG 3, PAGE 12. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4230 | BOEING REFERENCE STANDARD 747 PT 4 53-10-10 Page 6 Figure 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4231 | BOEING 747 REFERENCE STANDARD PART 4 57-10-18 FIGURE 2 PAGE 8. 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 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). | 1 | |
| 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). | 1 | |
| 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). | 1 | |
| 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). | 1 | |
| NDT4236 | Boeing Reference Standard 747 53-30-16 PART 6 Figure 1, Page 5&6. Material: 2024-T3 Clad Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). | 1 | |
| NDT4237 | Boeing Reference Standard 747 53-30-16 PART 6 Figure 1, Page 5&6. Material: 2024-T3 Clad Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). | 1 | |
| NDT4238 | Boeing Reference Standard 747 53-30-16 PART 6 Figure 1, Page 5&6. Material: 2024-T3 Clad Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). | 1 | |
| NDT4239 | Boeing Reference Standard 747 53-30-16 PART 6 Figure 1, Page 5&6. Material: 2024-T3 Clad Aluminum. Includes test report traceable to NIST Standards and Certificate of Conformance(COC). | 1 | |
| NDT4240 | BOEING REFERENCE STANDARD 747 Part 4 27-20-01 Page 8 Figure 3, Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4240P | BOEING 747 REFERENCE STANDARD PART 4, 27-20-01 PAGE 6 FIGURE 2 Includes Certificate of Conformance. | 1 | |
| NDT4243 | BOEING REFERENCE STANDARD 747 Part 6 57-10-31 Page 4 Figure 1. Material: 2024-T3 or An Airplane Quality with an Electrical Conductivity of 28-43% IACS. Fasteners: Non-Magetic Fastener. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4244 | BOEING REFERENCE STANDARD 747 Part 4 53-10-12 Page 5 Figure 2. Material: 7075-T6, 7075-T7, or 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT4246 | BOEING REFERENCE STANDARD 747 PT 6 53-10-34 Page 6 Figure 3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4247 | BOEING REFERENCE STANDARD 747 PART 4 27-60-01, PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT4249 | BOEING REFERENCE STANDARD 747 Part 6 53-30-19 Page 3 Figure 1. Material: 2024-T3 Clad. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4250 | BOEING REFERENCE STANDARD 747 PT 4 57-30-10 Page 6 Figure 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4251 | BOEING REFERENCE STANDARD 747 Part 4 57-30-11 Page 11 Figure 2. Material: Aircraft Qualtiy Alimunim Plate, Any 2024 and 7075. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4252 | BOEING REFERENCE STANDARD 747 Part 4 57-10-23 Page 6 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4254 | BOEING REFERENCE STANDARD 747 PT 4 57-10-24. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4263 | BOEING REFERENCE STANDARD 747 PT 4 57-10-25 PAGE 20 FIGURE 3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4264 | BOEING REFERENCE STANDARD 747 PT 4 57-10-25 PAGE 21 FIGURE 4. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4266 | BOEING REFERENCE STANDARD 747 PT 4 57-30-12 PAGE 8 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4267 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 10 FIGURE 2. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4268 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 11 FIGURE 3. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4269 | BOEING REFERENCE STANDARD 747 part 4 57-40-08 page 12 Figure 4. Material: 7075-T7. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4270 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 13 FIGURE 5. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4271 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 14 FIGURE 6. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4272 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 15 FIGURE 7. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4273 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 16 FIGURE 8. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4274 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 17 FIGURE 9. MATERIAL: 7075-T7 or 2024-T3 ALUMINUM,. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4275 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 18 FIGURE 10. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4276 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 18 FIGURE 10. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4277 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 18 FIGURE 10. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4278 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 18 FIGURE 10. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4279 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 18 FIGURE 10. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT4280 | BOEING REFERENCE STANDARD 747 PT 4 57-40-08 PAGE 18 FIGURE 10. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT4281 | BOEING REFERENCE STANDARD 747 PT 4 57-10-26 PAGE 5 FIGURE 2. MATERIAL: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT504A | Boeing 757 Reference Standard, Part 6, 54-40-01; Figure 3, Page 14 | 1 | |
| NDT504B | Boeing 757 Reference Standard, Part 6, 54-40-01; Figure 3, Page 14 | 1 | |
| NDT504C | Boeing 757 Reference Standard, Part 6, 54-40-01; Figure 3, Page 14 | 1 | |
| NDT504D | Boeing 757 Reference Standard, Part 6, 54-40-01; Figure 3, Page 14 | 1 | |
| NDT504E | Boeing 757 Reference Standard, Part 6, 54-40-01; Figure 3, Page 14 | 1 | |
| NDT5097-A | BOEING REFERENCE STANDARD 757 PT 4 57-20-03 FIG 2 PG 6. Material 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT5097-B | BOEING REFERENCE STANDARD 757 PT 4 57-20-03 FIG 2 PG 6. Material 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT5097-C | BOEING REFERENCE STANDARD 757 PT 4 57-20-03 FIG 2 PG 6. Material 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT5097-D | BOEING REFERENCE STANDARD 757 PT 4 57-20-03 FIG 2 PG 6. Material 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT511 | BOEING REFERENCE STANDARD 757 Part 6 57-10-02 Page 7 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT512 | BOEING REFERENCE STANDARD 757, PT 4 5710-01. Includes Test Report and Certificate of Conformance. | 1 | |
| 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) | 1 | |
| NDT515 | BOEING REFERENCE STANDARD 757 PT 4 57-21-01 FIG 3 PG 6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT516 | BOEING REFERENCE STANDARD 757 Part 6 57-23-01 Page 3 Figure 1. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT518 | BOEING REFERENCE STANDARD 757 PT 4 57-21-02 FIG 2 PG 6. Includes Test Report and Certificate of Conformance... | 1 | |
| NDT519 | BOEING REFERENCE STANDARD 757 Part 6 52-30-01 Page 8 Figure 4. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT522 | BOEING REFERENCE STANDARD 757 PT 4 53-80-01 FIGURE 4 PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT524 | BOEING REFERENCE STANDARD 757 PART 6 53-10-06 PAGE 5 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT525 | Boeing Reference Standard 757 Part 4 54-50-01 Page 7 Figure 3. Material: 4330, 4330M, 4340, or 4340M. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT527 | BOEING REFERENCE STANDARD 757 Part 6 53-30-06 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT528 | BOEING REFERENCE STANDARD 757 Part 4 55-10-04 Page 10 Figure 2. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT531 | BOEING REFERENCE STANDARD 757 Part 6 53-60-01 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT533 | BOEING REFERENCE STANDARD 757 PT 4 55-10-03 FI2 3 PG 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT537 | BOEING REFERENCE STANDARD 757 PT 4 57-10-02 FIG 3 PG 8. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT542 | BOEING REFERENCE STANDARD 757 Part 4 55-10-07 Page 11 Figure 3. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT546 | BOEING REFERENCE STANDARD 757 PT 4 57-20-02 FIGURE 2 PG. 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT549 | BOEING REFERENCE STANDARD 757 Part 6 57-20-02 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT552 | BOEING REFERENCE STANDARD 757 PT 4 57-20-01. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT555 | BOEING REFERENCE STANDARD 757 PT 4 53-10-19 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT558 | BOEING REFERENCE STANDARD 757 Part 6 53-30-12 Page 8 Figure 1. Material: 2024-T3. Includes Certification Report and Certificate of Conformance. | 1 | |
| NDT560 | BOEING REFERENCE STANDARD 757 PT 4 57-50-02 FIG 6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT561 | BOEING REFERENCE STANDARD 757 PT 4 57-50-02 FIG 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT562 | Boeing Reference Standard, 757 PT4 57-25-01:PG11 FIG2 | 1 | |
| NDT563 | BOEING REFERENCE STANDARD 757 PT 6 57-51-04 FIGURE 2, SHEETS 1 & 2 PAGE 10. Includes Test Report and Certificate of conformance. | 2 | |
| NDT564A | BOEING REFERENCE STANDARD 757 Part 4 57-50-01 Page 4 Figure 2. Material: Aircraft Grade Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT564B | BOEING REFERENCE STANDARD 757 Part 4 57-50-01 Page 4 Figure 2. Material: Aircraft Grade Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT566 | BOEING REFERENCE STANDARD 757 PT 4 54-50-03 FIGURE 2 PAGE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT567 | BOEING REFERENCE STANDARD 757 PT4 54-50-02 FIGURE 3 PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT568 | BOEING REFERENCE STANDARD 757 Part 6 57-51-05 Page 8 Figure 2. Material: 7050-T7. includes Test Report and Certificate of Conformance. | 2 | |
| NDT569 | BOEING REFERENCE STANDARD 757 PT 6 53-40-07 FASTENER (BACR15FV6KE). Includes Test Report and Certificate of Conformance. | 1 | |
| NDT575 | BOEING REFERENCE STANDARD 757 Part 6 53-60-12 Page 8 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT576 | Boeing Reference Standard, 757 | 1 | |
| NDT578 | BOEING REFERENCE STANDARD 757 Part 6 55-10-04 Page 10 Figure 2. Material: 2024-T6 or 7150-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT579 | BOEING REFERENCE STANDARD 757 Part 6 54-40-05 page 6 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT581 | BOEING REFERENCE STANDARD 757 PT 6 57-50-09 FIGURE 2 PAGE 7. Includes Test Report and Certificate of conformance. | 1 | |
| NDT582 | BOEING REFERENCE STANDARD 757 PT 6 57-50-08 Page 7 Figure 2. Material: 2024-T351 Aluminum Includes Test Report and Certificate of Conformance. | 2 | |
| NDT583 | Boeing Reference Standard | 1 | |
| NDT595 | BOEING REFERENCE STANDARD 757 Part 4 53-80-02 Page 7 Figure 2. Material: 2024-T3 or Equivalent. includes Test Report and Certificate of Conformance. | 1 | |
| NDT596 | BOEING REFERENCE STANDARD 757 PT 4 52-30-01. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6000-EC | BOEING REFERENCE STANDARD 57-50-02 PT 4 FIG 3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6000A | BOEING REFERENCE STANDARD 767 Part 4 57-50-02 Page 9 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6000B | BOEING REFERENCE STANDARD 767 Part 4 57-50-02 Page 9 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6000C | BOEING REFERENCE STANDARD 767 Part 4 57-50-02 Page 9 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6000D | BOEING REFERENCE STANDARD 767 Part 4 57-50-02 Page 9 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6000E | BOEING REFERENCE STANDARD 767 Part 4 57-50-02 Page 9 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6001 | BOEING REFERENCE STANDARD 767 Part 4 57-50-23 Page 7 Figure 2. Material: 4330M, 4340M or 4340. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6002 | BOEING REFERENCE STANDARD 767 Part 4 57-50-24 Page 7 Figure 2. Material: 6AL-4V. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6004 | BOEING REFERENCE STANDARD 767 PART 4 57-50-09 PAGE 11 FIGURE 2. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6005 | BOEING REFERENCE STANDARD 767 PART 4 57-50-09 PAGE 12 FIGURE 3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6006 | BOEING REFERENCE STANDARD 767 PART 4 57-50-09 PAGE 13 FIGURE 4. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6007 | Boeing Titanium Reference Standard w/certs 767 PT4 57-50-11 PG 7 FG 2 | 2 | |
| NDT6008 | Boeing Titanium Reference Standard w/certs 767 PT4 57-50-11 PG 8 FG 3 | 2 | |
| NDT6009 | Boeing Reference Standard, 767 PT4 52-30-03:PG5 FIG2 | 2 | |
| NDT6010 | Boeing Reference Standard, 767 PT4 52-30-02:PG5 FIG2 | 1 | |
| NDT6011 | BOEING REFERENCE STANDARD 767 Part 4 57-50-20 Page 6 Figure 2. Material: Titanium. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6012 | BOEING REFERENCE STANDARD 767 PT 4 57-50-26 FIGURE 2, PAGE 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6013 | BOEING REFERENCE STANDARD 767 PT 4 57-50-26 FIGURE 3, PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6014 | BOEING REFERENCE STANDARD 767 Part 4 57-50-16 page 6 Figure 2. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6015 | BOEING REFERENCE STANDARD 767 Part 4 57-50-16 Page 6 Figure 3. Material: 7075-T or 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6016 | Boeing Reference Standard, 767 PT4 53-10-03:PG4 FIG2 | 2 | |
| NDT6017 | Boeing Titanium Reference Standard w/certs 767 PT4 57-50-22 PG 6-7 FG 2 | 2 | |
| NDT6018 | Boeing Titanium Reference Standard w/certs 767 PT4 57-50-22 PG 8-9 FG 3 | 2 | |
| NDT6019 | Boeing Reference Standard 767 52-32-06 Fig. 2 | 2 | |
| NDT602 | Calibration Reference Standard | 1 | |
| NDT6020 | BOEING REFERENCE STANDARD 767 PART 4 57-50-14 PAGE 11 FIGURE 4. Includes Certificate of Conformance. | 2 | |
| NDT6021 | BOEING REFERENCE STANDARD 767 PART 4 57-50-14 PAGE 112 FIGURE 5. Includes Certificate of Conformance. | 2 | |
| NDT6022 | BOEING REFERENCE STANDARD 767 Part 4 57-50-15 Page 5 Figure 2. Material: 7075-T6 or 2024, 7050, 7075. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6023 | BOEING REFERENCE STANDARD 767 Part 4 -57-50-21 Page 5 Figure 2. Material: 7075-T7 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6024 | BOEING REFERENCE STANDARD 767 Part 6 57-50-10 Page 5 Figure 2. Material: 4330M. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 2 | |
| 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. | 2 | |
| NDT6027 | BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 9 FIGURE 2. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6028 | BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 10 FIGURE 3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6029 | BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 11 FIGURE 4. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6030 | BOEING REFERENCE STANDARD 767 PART 4 57-50-10 PAGE 12 FIGURE 5. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6031-1 | BOEING REFERENCE STANDARD 767 Part 4 57-50-18 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6031-2 | BOEING REFERENCE STANDARD 767 Part 4 57-50-18 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6031-3 | BOEING REFERENCE STANDARD 767 Part 4 57-50-18 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6031-4 | BOEING REFERENCE STANDARD 767 Part 4 57-50-18 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6032-1 | BOEING REFERENCE STANDARD 767 Part 4 57-50-19 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6032-2 | BOEING REFERENCE STANDARD 767 Part 4 57-50-19 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6032-3 | BOEING REFERENCE STANDARD 767 Part 4 57-50-19 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6032-4 | BOEING REFERENCE STANDARD 767 Part 4 57-50-19 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6033-1 | BOEING REFERENCE STANDARD 767 Part 4 57-50-12 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6033-2 | BOEING REFERENCE STANDARD 767 Part 4 57-50-12 Page 5 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6034 | Boeing Reference Standard 767 PT4 57-50-13 PG7 FG 2 | 1 | |
| NDT6035-1 | BOEING REFERENCE STANDARD 767 Part 4 57-50-13 Page 8 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6035-2 | BOEING REFERENCE STANDARD 767 Part 4 57-50-13 Page 8 Figure 3. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6036 | REFERENCE STANDARD BOEING | 2 | |
| NDT6038 | BOEING REFERENCE STANDARD 767 Part 4 57-50-25 Page 6 Figure 2. Material: 7050-T7 or Equivalent. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6041 | REFERENCE STANDARD B767 4 57-20-03 | 3 | |
| NDT6045 | BOEING REFERENCE STANDARD 767 PART 4 54-50-08. MATERIAL: 7075-T6 or 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6045-SC1 | Boeing Transducer Guide. Material: Delrin ( Black Acetal). Used with NDT6045 Reference Standard. 767 PART 4 54-50-08 PAGE 15 FIGURE 3 | 1 | |
| NDT6045-SC2 | Boeing Transducer Guide. Material: Delrin ( Black Acetal). Used with NDT6045 Reference Standard. 767 PART 4 54-50-08 PAGE 15 FIGURE 3 | 1 | |
| NDT6046 | BOEING REFERENCE STANDARD 767 Part 4 53-30-02 Page 8 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6047 | BOEING REFERENCE STANDARD 767 PT 4 53-30-02 PAGE 9 FIG 1. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6048 | BOEING REFERENCE STANDARD 767 Part 4 27-40-02 horizontal stab inspection. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6049 | BOEING REFERENCE STANDARD 767 PART 6 57-20-09 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6050 | BOEING REFERENCE STANDARD 767 PART 6 57-20-09 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6051 | BOEING REFERENCE STANDARD 767 PART 6 57-20-09 FIGURE 2 PAGE 5. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6052 | BOEING REFERENCE STANDARD 767 P4, 57-50-27. UT INSPECTION OF MAIN LANDING GEAR FORWARD TRUNNION SUPPORT SIDE LOAD FITTING | 1 | |
| NDT6052G | BOEING 767 6052 REFERENCE STANDARD GUIDE. DELRIN | 1 | |
| NDT6057 | BOEING REFERENCE STANDARD 767 PART 4 54-50-11 PAGE 7 FIGURE 2. MATERIAL: 15-5 CRES. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6058 | REFERENCE STANDARD B767 | 3 | |
| 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. | 3 | |
| NDT6060 | BOEING REFERENCE STANDARD 767 | 3 | |
| NDT6061 | BOEING REFERENCE STANDARD 767 | 3 | |
| 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. | 1 | |
| NDT6063 | BOEING REFERENCE STANDARD 767 | 3 | |
| 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. | 1 | |
| NDT6065 | BOEING REFERENCE STANDARD 767 PART 4 54-50-09 PAGE 12 FIGURE 2. MATERIAL: 2024-T3 OR 7075 SERIES ALUMINUM.. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6066 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 11. LUG B 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6067 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 9. LUG A 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6068 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 15. LUG D 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6069 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 13. LUG C..4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT607 | BOEING REFERENCE STANDARD 767 Part 6 53-80-02 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6070 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 17. LUG E 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6071 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 19. LUG F 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6072 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 21. LUG H 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6073 | BOEING REFERENCE STANDARD PART 4 54-50-11 FIGURE 4 PAGE 23. LUG G 4340M STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT6075 | BOEING REFERENCE STANDARD 767 PART 6 53-10-22 FIGURE 2 PAGE 5. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| NDT607A | BOEING REFERENCE STANDARD 767 Part 6 53-80-02 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT6081 | BOEING REFERENCE STANDARD 767 PART 4 54-50-16 PAGE 5 FIGURE 2 MATERIAL: 15-5PH STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6082 | BOEING REFERENCE STANDARD 767 Part 4 54-50-13 Page 13 Figure 2. Material: 7075-T6 or 7075-T7, 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6083 | BOEING REFERENCE STANDARD 767 Part 4 54-50-13 Page 14 Figure 3. Material: 7075-T7 or 7075-T6, 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6084 | BOEING REFERENCE STANDARD 767 Part 4 54-50-13 Page 15 Figure 4. Material: 7075-T6 or 7075-T7, 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6085 | BOEING REFERENCE STANDARD 767 Part 4 54-50-13 Page 16 Figure 5. Material: 7075-T6 or 7075-T7, 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6086 | BOEING REFERENCE STANDARD 767 Part 4 54-50-13 Page 17 Figure 6. Material: 7075-T6 or 7075-T7, 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6088 | BOEING REFERENCE STANDARD 767 PART 4 54-50-12 PAGE 9 FIGURE 2. MATERIAL: 15-5 CRES. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6089 | BOEING REFERENCE STANDARD 767 PART 4 54-50-15 PAGE 35-37 FIGURE 10 SHEETS 1-3. MATERIAL: 15-5PH STEEL.. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6090 | BOEING REFERENCE STANDARD 767 PART 4 54-50-15 PAGE 38-40 FIGURE 10 SHEETS 1-3. MATERIAL: 15-5PH STEEL.. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6091 | BOEING REFERENCE STANDARD 767 PART 4 54-50-14 PAGE 26 FIGURE 2. MATERIAL: 15-5 CRES. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6092 | BOEING REFERENCE STANDARD 767 PART 4 54-50-14 PAGE 27 FIGURE 3. MATERIAL: 15-5 CRES. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6094 | BOEING REFERENCE STANDARD 767 PART 4 54-50-14 PAGE 29 FIGURE 5. MATERIAL: 15-5 CRES. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| NDT6099 | BOEING REFERENCE STANDARD PER MARKUP 767 PT 4 57-20-01 PAGE 4 FIGURE 2 | 2 | |
| NDT6100 | BOEING REFERENCE STANDARD 767 PART 4 57-10-03 PAGE 6 FIGURE 2 MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6102 | BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM. Includes Test Report Traceable to NIST. | 1 | |
| NDT6103 | BOEING REFERENCE STANDARD 767 PART 4 54-50-17 PAGE 5 FIGURE 2. MATERIAL: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6104 | BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM. Includes Test Report Traceable to NIST. | 1 | |
| NDT6105 | BOEING REFERENCE STANDARD 767 PT 6 53-50-16 PAGE 5 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Certification Report | 1 | |
| NDT6108 | BOEING REFERENCE STANDARD 767 PT 4 57-20-03, Figure 4 Page 9. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6109 | BOEING REFERENCE STANDARD BOEING REFERENCE STANDARD 767 PART 6 57-20-01. Includes Test Report and Certificate of Conformance. MATERIAL: 7075-T6, 2024-T3 CLAD OR BARE ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT611 | BOEING REFERENCE STANDARD 767 PT 6 54-51-01 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6110A | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 FIGURE 4 SHEETS 1&2 PAGES 9&10. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6110B | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 FIGURE 4 SHEETS 1&2 PAGES 9&10. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6110C | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 FIGURE 4 SHEETS 1&2 PAGES 9&10. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6110D | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 FIGURE 4 SHEETS 1&2 PAGES 9&10. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6110E | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 FIGURE 4 SHEETS 1&2 PAGES 9&10. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6111A | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 Figure 5, Sheets 1-2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6111B | BOEING 767 REFERENCE STANDARD PART 6 57-20-08 Figure 5, Sheets 1-2. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT612 | BOEING REFERENCE STANDARD 767 PT 6 54-51-01 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT613 | BOEING REFERENCE STANDARD 767 PT 6 54-51-01 FIGURE 2 PAGE 8. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT614 | REFERENCE STANDARD B767 4 57-20-01 | 3 | |
| NDT615 | BOEING REFERENCE STANDARD 767 PT 4 53-80-01 FIG 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT616 | BOEING REFERENCE STANDARD 767 Part 4 27-40-01 Page 4 Figure 2. Matierial: 7075-T7 (Preferred) or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT617 | BOEING REFERENCE STANDARD 767 Part 6 53-80-03 Page 6 Figure 2. Material: 4330M or 4340M. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT618 | BOEING REFERENCE STANDARD 767 Part 6 53-80-03 Page 7 Figure 3. Material: 4330M or 4340M. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT618A | BOEING REFERENCE STANDARD 767 Part 6 53-80-03 Page 8 Figure 3. Material: 4330M or 4340M. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT619 | BOEING REFERENCE STANDARD 767 Part 4 55-10-04 Page 5 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT620 | BOEING REFERENCE STANDARD 767 Part 4 53-60-01 Page 5 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT621 | BOEING REFERENCE STANDARD 767 PT 4 57-10-01 page 4 fig.1. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT622 | REFERENCE STANDARD B767 657-20-01 | 4 | |
| NDT623 | REFERENCE STANDARD B767 4 57-10-03 | 3 | |
| NDT624 | BOEING REFERENCE STANDARD 767 Part 4 53-80-02 Page 6 Figure 2. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT625 | BOEING REFERENCE STANDARD 767 Part 4 55-10-03 Page 4 Figure 2. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT627 | BOEING REFERENCE STANDARD 767 Part 4 57-10-02 Page 5 Figure 3. Material: 7075-T6 or Equivalent. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT628 | BOEING REFERENCE STANDARD 767 PT 4 53-50-01. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT629 | BOEING COMPOSITE REFERENCE STANDARD 767 PT 4 57-40-01. AULUMINUM to ALUMINUM HONEYCOMB CORE. Includes C-Scan Report and Certificate of Conformance. 2 year Unconditional Warranty. | 2 | |
| NDT630 | BOEING REFERENCE STANDARD 767 Part 4 55-10-02 Page 5 Figure 2. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT631 | BOEING REFERENCE STANDARD 767 Part 4 71-20-01 Page 6 Figure 2. Material: 15-5 PH or 4130, 4140, 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT632 | BOEING REFERENCE STANDARD 767 Part 4 71-20-01 Page 7 Figure 3. Material: 15-5 PH or 4130, 4140, 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT633 | BOEING REFERENCE STANDARD 767 Part 6 54-51-02 Page 9 Figure 2. Material: 4330, 4330M, 4340, 4340M. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT634 | BOEING REFERENCE STANDARD 767 Part 4 54-50-02 Page 5 Figure 2. Material: 15-5PH or 4330M, 4340M. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT636 | BOEING REFERENCE STANDARD 767 Part 4 32-10-03 Page 4 Figure 2. Material: 4140, 4330, 4340, 4330M, or 4340M. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT637 | BOEING REFERENCE STANDARD 767 Part 4 32-10-04 Page 7 Figure 2. Material: 4330 or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT638 | BOEING REFERENCE STANDARD 767 Part 4 57-40-02 Page 5 Figure 2. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT639 | BOEING REFERENCE STANDARD 767 Part 4 54-50-02 Page 6 Figure 3. Material: 15-5 PH or 4330M , 4340M. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT640 | BOEING REFERENCE STANDARD 767 Part 4 54-50-01 Page 5 Figure 2. Material: 15-5 PH or 4330M, 4340M. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT641 | BOEING REFERENCE STANDARD 767 Part 4 54-50-01 Page 6 Figure 3. Material: 15-5 PH or 4330M, 4340M. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT642 | BOEING REFERENCE STANDARD 767 Part 4 53-50-02 Page 6 Figure 2. Material: 7075-T6 or Equivalent. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT643 | BOEING REFERENCE STANDARD 767 PT 6 57-20-03. Includes Test Report and Certificate of Conformance. | 5 | |
| NDT644 | BOEING REFERENCE STANDARD 767 PT 4 57-20-02. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT648 | BOEING REFERENCE STANDARD 767 PT 6 53-30-06 FIGURE 3 PAGE 32. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT650 | BOEING REFERENCE STANDARD 767 Part 6 Page 4 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT651 | BOEING REFERENCE STANDARD 767, 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT652 | REFERENCE STANDARD B767 4 57-20-07 | 4 | |
| NDT655 | BOEING REFERENCE STANDARD 767 Part 4 54-50-03 Page 7 Figure 4. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT656 | BOEING REFERENCE STANDARD 767 Part 4 54-50-03 Page 8 Figure 3. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT657 | BOEING REFERENCE STANDARD 767 Part 6 53-10-09 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT658 | BOEING REFERENCE STANDARD 767 Part 4 53-10-01 Page 5 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT660 | Boeing Reference Standard, 767 PT6 53-80-04:PG11 FIG3 | 4 | |
| NDT661 | BOEING REFERENCE STANDARD 767 Part 4 53-30-01 Page 5 Figure 2. Material: 7075-T6 or 7075-T7. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT662 | BOEING REFERENCE STANDARD 767 PT 4 57-20-03, Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT663A | BOEING REFERENCE STANDARD 767 Part 6 53-10-13 Page 7 Figure 3. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT663A/B | Boeing Reference Standard, 767 PT6 53-10-13:PG7 FIG3 | 1 | |
| NDT663B | BOEING REFERENCE STANDARD 767 Part 6 53-10-13 Page 7 Figure 3. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT664 | BOEING REFERENCE STANDARD 767 Part 6 57-20-06 Page 8 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT664-A | BOEING REFERENCE STANDARD 767 PART 6 57-20-06. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT665 | BOEING REFERENCE STANDARD 767 PT 6 53-10-06 PAGE 4 FIGURE 2. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT666A | BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 8 Figure 3. Material 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT666B | BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 9 Figure 4. Material 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT666C | BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 10 Figure 5. Material 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT667 | BOEING REFERENCE STANDARD 767 Part 4 54-50-05 Page 7 Figure 2. Material: 15-5 PH or 4130. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT668 | BOEING REFERENCE STANDARD 767 Part 6 57-50-01 Page 5 Figure 2. Material: 15-5 PH. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT669 | BOEING REFERENCE STANDARD 767 Part 4 3210-05 Page 5 Figure 2. Material: 4330 or 4340. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT670 | BOEING REFERENCE STANDARD 767 Part 4 53-10-02 Page 5 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT671 | BOEING REFERENCE STANDARD 767 Part 6 53-30-12 Page 4 Figure 2. Material: 7075-T6 or 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT672 | BOEING REFERENCE STANDARD 767 Part 6 54-50-01 Page 4 Figure 2. Material: 15-5 PH or 4130. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT674 | BOEING REFERENCE STANDARD 767 PT 4 54-50-06 PAGE 14 FIGURE 3. Includes Certification Report. | 3 | |
| NDT675 | BOEING REFERENCE STANDARD 767 Part 4 54-50-06 Page 15 Figure 4. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT676 | BOEING REFERENCE STANDARD FOR PW4000 and JT9D-7R4D/E STRUTS FIGURE 2 Part 4 54-50-07 page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT679 | BOEING REFERENCE STANDARD 767 53-50-05 PT 4 FIG 3. Includes.Test Report and Certificate of Conformance. | 2 | |
| NDT680 | BOEING REFERENCE STANDARD 767 Part 4 32-10-06 Page 5 Figure 2. Material: 4340M. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT682 | BOEING REFERENCE STANDARD 767 Part 6 53-80-02 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 4 | |
| NDT684 | BOEING REFERENCE STANDARD 767 Part 6 52-32-02 Page 5 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT685 | BOEING REFERENCE STANDARD 767 Part 6 53-10-018 Page 5 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT686 | BOEING REFERENCE STANDARD 767 Part 6 53-50-09 Page 5 Figure 3. Material: 7075-T6 or Equivalent. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT687 | BOEING REFERENCE STANDARD 767 PT 4 57-50-08 PAGE 6 FIGURE 3. . Includes Test Report and Certificate of Conformance. | 2 | |
| NDT688 | BOEING REFERENCE STANDARD 767 Part 4 57-50-03 Page 8 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance | 3 | |
| NDT689 | BOEING REFERENCE STANDARD 767 Part 4 57-50-06 Page 6 Figure 2. Material: 4340. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT690 | BOEING REFERENCE STANDARD 767 PT 4 57-50-04 PAGE 8 FIGURE 3. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT691 | BOEING REFERENCE STANDARD 767 Part 6 57-50-08 Page 6 Figure 2. Material: 4340M. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT693 | BOEING REFERENCE STANDARD 767 Part 4 53-50-04 Page 6 Figure 4. Material: 2024-T3 or 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT694 | BOEING REFERENCE STANDARD 767 Part 4 57-50-05 Page 8 Figure 3. Material: 15-5 PH. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT695 | BOEING REFERENCE STANDARD 767 Part 4 57-50-05 Page 8 Figure 3. Material: 15-5 PH. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT697 | BOEING REFERENCE STANDARD 767 Part 4 -57-50-07 Page 5 Figure 2. Material: 15-5 PH. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT698 | BOEING REFERENCE STANDARD 767 Part 4 57-50-03 Page 9 Figure 3. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT7001P | BOEING LUCITE WEDGE WITH A .315"Ø FLAT BOTTOM HOLE, 2.010" RADIUS FOR A .25"Ø STRAIGHT BEAM TRANSDUCER. USED WITH REFERENCE STANDARD NDT7001. | 1 | |
| NDT7005 | REFERENCE STANDARD NDT7005 BOEING777 | 2 | |
| NDT7010A | BOEING REFERENCE STANDARD | 1 | |
| NDT7010B | BOEING REFERENCE STANDARD | 1 | |
| NDT7011 | BOEING REFERENCE STANDARD | 1 | |
| NDT7013 | BOEING REFERENCE STANDARD | 1 | |
| NDT7015 C | CALIBRATION REFERENCE STANDARD | 1 | |
| NDT7015-A | BOEING REFERENCE STANDARD | 1 | |
| NDT7015-B | BOEING REFERENCE STANDARD | 1 | |
| NDT7023 | BOEING REFERENCE STANDARD | 1 | |
| NDT7024 | BOEING REFERENCE STANDARD | 1 | |
| NDT703 | Boeing 777 Reference Standard, Part 6, 57-60-01 | 1 | |
| NDT7031A | BOEING REFERENCE STANDARD 777-200/300 PART 4 57-20-14 PAGE 6 FIGURE 2. MATERIAL: 7055-T7751, OR AIRPLANE QUALITY ALUMINUM. INCLUDES TEST REPORT AND CE | 2 | |
| NDT7031B | BOEING REFERENCE STANDARD 777-200/300 PART 4 57-20-15 PAGE 11-12 FIGURE 2, SHEET 1&2 AND PART 4 57-20-13 PAGE 6 FIGURE 2. MATERIAL: 7055-T7751, OR AIR | 2 | |
| NDT7031C | BOEING REFERENCE STANDARD 777-200/300 PART 4 57-20-15 PAGE 13 FIGURE 2, SHEET 3. MATERIAL: 7055-T7751, OR AIRPLANE QUALITY ALUMINUM. INCLUDES TEST RE | 1 | |
| NDT705 | Boeing 777 Reference Standard, Part 6, 57-40-01 | 1 | |
| NDT708 | Boeing 777 Reference Standard, Part 6, 53-50-01 | 1 | |
| NDT709 | Boeing 777 Reference Standard, UT, Part 4, 57-60-01 | 1 | |
| NDT710 | Boeing 777 Reference Standard, Part 6, 54-51-01 | 2 | |
| NDT711 | Boeing 777 Reference Standard, Part 6, 54-51-01 | 2 | |
| NDT712 | Boeing 777 Reference Standard, Part 6, 54-51-01 | 2 | |
| NDT731 | BOEING REFERENCE STANDARD 777 Part 4 53-40-01 Page 5 Figure 2. Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT732A | Boeing Reference Standard 777 PT4 55-17-03 PG6 FG2 | 2 | |
| NDT733 | Boeing Reference Standard 777 PT4 53-40-03 PG7 FG2 | 2 | |
| NDT734 | Boeing Reference Standard Part 4 57-54-02 Page 8 Figure 4. Includes Certificate of Conformance. | 2 | |
| NDT735 | BOEING REFERENCE STANDARD 777 Part 4 53-40-02 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 1 | |
| NDT737 | BOEING REFERENCE STANDARD 777 Part 6 53-50-03 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT738 | Boeing Reference Standard 777 PT4 53-10-02 PG6 FG2 | 2 | |
| NDT739 | Boeing Reference Standard 777 PT4 53-10-02 PG7 FG3 | 2 | |
| NDT740 | BOEING REFERENCE STANDARD 777 Part 4 53-10-01 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT741 | BOEING REFERENCE STANDARD 777 PT 4 57-12-01 PAGE 7 FIGURE 2. Includes Test Report and Certificate of Conformance | 2 | |
| NDT742B | Boeing Reference Standard, RIB 34 | 1 | |
| NDT742C | Boeing Reference Standard, RIB 36 | 1 | |
| NDT742D | Boeing Reference Standard, RIB 37 | 1 | |
| NDT744 | BOEING REFERENCE STANDARD 777 Part 6 53-10-09 Page 4 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT745 | BOEING REFERENCE STANDARD 777 PT 6 57-20-01 FASTENER (BACB30WQ7K15L + BACN10TN7K). Includes Test Report and Certificate of Conformance. | 2 | |
| NDT746 | BOEING REFERENCE STANDARD 777 Part 6 53-60-07 Page 7 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT747-1 | BOEING REFERENCE STANDARD 777 PT 6 53-00-11 FASTENER (BACR15FVKE). Includes Test Report and Certificate of Conformance. | 2 | |
| NDT747-2 | BOEING REFERENCE STANDARD 777 PT 6 53-00-11 FASTENER (BACR15FV8KE). Includes Test Report and Certificate of Conformance. | 2 | |
| NDT748 | BOEING REFERENCE STANDARD 777 Part 4 54-51-01 Page 14 Figure 2. Material: 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT749 | Boeing Reference Standard 777 PT6 57-20-03 PG 7 FG 2 | 2 | |
| NDT753 | BOEING REFERENCE STANDARD 777 Part 4 57-20-04 Page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT754 | BOEING 777 REFERENCE STANDARD PART 6 53-80-03 FIGURE 3 PAGE 5. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT755 | BOEING REFERENCE STANDARD 777 Part 6 53-60-07 Page 8 Figure 3. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT756 | BOEING REFERENCE STANDARD Part 6 53-60-07 Page 9 Figure 4. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT757 | Boeing Reference Standard 777 PT4 57-20-03 PG 7 FG 2 | 1 | |
| NDT760 | BOEING REFERENCE STANDARD 777 Part 6 53-60-06 Page 6 Figure 2. Material: 7075-T7. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT761 | BOEING 777 REFERENCE STANDARD PART 4 53-80-01 FIGURE 2 PAGE 9. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 2 | |
| NDT763 | BOEING REFERENCE STANDARD 777 PT 4 54-51-04. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT766 | BOEING REFERENCE STANDARD 777 PT 4 57-10-02 PAGE 9 FIGURE 2. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT767 | BOEING REFERENCE STANDARD 777 PT 4 57-10-02 PAGE 11 FIGURE 3. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT768 | Boeing Reference Standard 777 PT4 57-10-01 PG 6 FG 2 | 2 | |
| NDT769 | Boeing Reference Standard 777 PT4 57-10-01 PG 7 FG 3 | 2 | |
| NDT770 | Boeing Reference Standard | 2 | |
| NDT771 | Boeing Reference Standard | 2 | |
| NDT772 | Boeing Reference Standard 777 PT4 57-10-04 PG 18 FG 4 | 2 | |
| NDT773 | Boeing Reference Standard 777 PT4 57-10-04 PG 19 FG 5 | 2 | |
| NDT774 | Boeing Reference Standard | 2 | |
| NDT775 | Boeing Reference Standard 777 PT6 54-51-15 PG 5 FG 2 | 1 | |
| NDT776 | Boeing Reference Standard 777 PT4 54-51-03 PG 7 FG 2 *make part out of 2024-T3, heat treat to 2024-T8 | 2 | |
| NDT777 | BOEING REFERENCE STANDARD | 1 | |
| NDT778 | Boeing Reference Standard, 777 PT4 78-30-05 PG 8-9 FG 2 | 1 | |
| NDT779 | Boeing Reference Standard 777 PT4 55-51-01 PG 15 FG 3 | 1 | |
| NDT780-A | BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT780-B | BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT780-C | BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT780-D | BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT780-E | BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT780-F | BOEING REFERENCE STANDARD 777 PT 4 -57-50-01 Figure 2 Page 7. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT781 | BOEING REFERENCE STANDARD 777 PT 6 57-40-02 PAGE 6 FIGURE 2. Includes Test Report and Certificate of Conformance... | 2 | |
| NDT784 | BOEING REFERENCE STANDARD | 1 | |
| NDT786-A | BOEING REFERENCE STANDARD 777 Part 6 57-10-04 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT786-B | BOEING REFERENCE STANDARD 777 Part 6 57-10-04 Page 6 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT787 | BOEING REFERENCE STANDARD 777-200/300 Part 6 53-80-06 Page 8 Figure 2. Material: 2024-T3. IncludesTest Report and Certificate of Conformance. | 2 | |
| NDT789 | BOEING REFERENCE STANDARD 777 PT 6 57-20-03 PG.17 FIGURE 3. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT790 | BOEING REFERENCE STANDARD 777 PT 6 57-20-03 PG. 18 FIGURE 4. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT791 | BOEING REFERENCE STANDARD 777 PT 6 57-20-03 PG.19 FIGURE 5. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT792 | BOEING REFERENCE STANDARD 777 PT 6 57-20-03 PAGE 20 FIGURE 6. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 3 | |
| NDT799 | BOEING REFERENCE STANDARD 757 Part 4 51-00-05 Page 7 Figure 2. 777-200/300 Part 4 51-00-05 Page 8 Figure 1. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT801 | BOEING REFERENCE STANDARD 787-8 51-13-02-00A-280A-A. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT803A | BOEING REFERENCE STANDARD ABS PLASTIC THICKNESS MEASUREMENT. PART 4 51-00-07 page 11 figure 2 | 2 | |
| NDT803B | BOEING REFERENCE STANDARD ABS PLASTIC THICKNESS MEASUREMENT. PART 4 51-00-07 page 11 figure 2 | 2 | |
| NDT815 | BOEING REFERENCE STANDARD 787 Part 4 57-10-01 Page 10 Figure 2. Material: 2024 or 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT816 | BOEING REFERENCE STANDARD 787 part 4 57-10-02 Figure 2. MATERIAL: 6AL-4V TITANIUM. Includes Certification Report and Certificate of Conformance. | 2 | |
| NDT817 | BOEING REFERENCE STANDARD 787 Part 4 51-00-23 Page 5 Figure 2. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NEC-6252 | boeing ec reference standard w/cert | 1 | |
| NEC-6429 | BOLT HOLE REFERENCE STANDARD | 1 | |
| PWA84314 | REFERENCE STANDARD FOR EDDY CURRENT TEST ON PW2000 SERIES ENGINE FAN BLADES | 1 | |
| R&D-SHEAR WAVE-EDGE-TI | BOEING REFERENCE STANDARD R&D SHEAR WAVE EDGE | 1 | |
| RH12-T40-7075T6 | CALIBRATION REFERENCE STANDARD (CRS), ALUMINUM ALLOY, CONDUCTIVITY VALUE OF 35% TO 45% IACS THAT CONTAINS VARIOUS HOLE SIZES WITH 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (TECHNA NDT OR EQUIVALENT) | 1 | |
| RM17-C23-2024T3 | Special Boeing Type Reference Standard, per PT6 51-00-00 Fig 16, | 1 | |
| RM200-T40-T6AL4V | CALIBRATION REFERENCE STANDARD, TITANIUM ALLOY, CONDUCTIVITY 1.1 % IACS, CONTAINS 0.010 IN. (0.25 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP SURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES, AND VARIOUS SIZE HOLES WITH 0.040-IN (1.02 MM) EDM NOTC | 1 | |
| RS367SAL | NDT REFERENCE STANDARD 367 BOEING | 1 | |
| RS9000-1 | DC9 REFERENCE STANDARD PER BOEING SB DC9-54A031 PAGE 16 FIGURE 1. Includes Test Report and Certificate of Conformance. | 1 | |
| RSAF-304 | PH TOOL REFERENCE STANDARD STAINLESS SPEC USAF TO 33-B-1-1 | 1 | |
| RSAF-T6AL4V | PH TOOL REFERENCE STANDARD TITANIUM SPEC USAF TO 33-B-1-1 | 1 | |
| RSDC6-5 | BOEING REFERENCE STANDARD DC6 | 1 | |
| RSN-2024T3-1 | Navy Reference Standard, 2024T3 Aluminum *.040" +004/-000 countersink notches, similar to Boeing 194 standard* | 1 | |
| S-17-1 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 1, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-2 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 2, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-3 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 3, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-4 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 4, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-5 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 5, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-6 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 6, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-7 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 7, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S-17-8 | BOEING CUSTOM NDI TEST REFERENCE STANDARD ASSEMBLY DASH NO. 8, MATERIAL 2024-T3, STRINGER=7075-T6 | 1 | |
| S41-E1A | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1A NDI REF STD PER DRAWING SK667-00011. | 1 | |
| S41-E1C | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1C NDI REF STD PER DRAWING SK667-00012. | 1 | |
| S41-F1B | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-F1B NDI REF STD PER DRAWING SK667-00010. | 1 | |
| S46-C2 | BOEING REFERENCE STANDARD S42-C6 FIGURE 2. MATERIAL: 2024-T3 CLAD. RIVET: BACR15CE6. Includes Test Report and Certificate of Conformance | 1 | |
| S46-G1A/G2A | BOEING REFERENCE STANDARD FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. FASTENERS: BACR15CE6D 2 PLACES. Includes Certification Report. | 1 | |
| S53-10-103.3/1 | BAE 146-RJ SERIES REFERENCE STANDARD 53-10-25 PT 4 FIGURE 3&4 PAGES 7&8. Includes Test Report and Certificate of Conformance. | 1 | |
| S57-10-105.2/1 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-58 PT 6 FIGURE 7-9 PAGES 13-15. Material: 2024-T3 Includes Test Report and Certificate of Conformance. | 1 | |
| S57-10-105.2/2 | BAE 146-RJ SERIES REFERENCE STANDARD 57-10-58 PT 6 FIGURE 7-9 PAGES 13-15. Material: 2024-T3 Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| SB 146/53-167/2 | BAE 146-RJ SERIES REFERENCE STANDARD ISB.53-167 APPENDIX 2 DRAWING 15, PAGE 23&24. Material: Substitute 2024-T3 Clad for 2014A-T4 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| SB09270209-5 | Eddy Current Inspection Reference standard SB DC9-27-209 R07 | 1 | |
| SB09270288-5 | NDT REFERENCE STANDARD - SB09270288-5 | 1 | |
| SB09530016-5 | Eddy Current Inspection Reference standard SB MD-A27-320 R01 | 2 | |
| SB09530186-9 | Eddy Current Inspection Reference standard SB DC9-53-186 R06 | 1 | |
| 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. | 2 | |
| 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. | 1 | |
| SB10550016-147 | DC-10 SERVICE BULLETIN REFERENCE STANDARD FIGURE 1 PAGE 14, SHEET 1. MATERIAL: 7075-T6 ALUMNIUM. Includes Test Report and Certificate of Conformance. | 1 | |
| SK601R-10022 | CALIBRATION REFERENCE STANDARD | 1 | |
| SK601R-20003 | CALIBRATION REFERENCE STANDARD | 2 | |
| SK601R-30008A | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERED FASTENED ASSEMBLY, EQUIVALENT IN MATERIAL AND THICKNESS AS THE INSPECTION AREA CONTAINING SUBSURFACE ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ). | 6 | |
| SK601R-30009 | CALIBRATION, REFERENCE STANDARD | 2 | |
| SK601R-30009-1 | CALIBRATION, REFERENCE STANDARD | 5 | |
| SK601R-30014 | CALIBRATION STANDARD REFERENCE | 2 | |
| SK601R-30039 | NDT CALIBRATION REFERENCE STANDARD | 2 | |
| SK601R−10043 | Calibration reference standard block (Bombardier Inc.) | 1 | |
| SLS-123456-SS304 | BOEING REFERENCE STANDARD PER DRAWING STD-1. MATERIAL: 304 STAINLESS STEEL. CHEMICAL CONVERSION COATING PER MIL-DTL-5541, CLASS 1A. Includes Certification Traceable to NIST and Material Certs. | 1 | |
| SLS-IN718-201-010793B2 | BOEING REFERENCE STANDARD, 0.030 x 0.030 x .005" +/- 002" CORNER EDM NOTCH. MATERIAL: 718 INCONEL | 1 | |
| SN10280002 | DOUGLAS REFERENCE STANDARD FIGURE 2 SHEETS 2-8. INCLUDES GANG CHANNEL PART NUMBER RMG9421-3-7-2. Test Report and Certificate of Conformance included. | 1 | |
| SN10550000 | BOEING REFERENCE STANDARD SHEETS 1-4. DETAIL -3,-5,-7. MATERIAL: 7075-T7 & 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| SN90570006 | BOEING REFERENCE STANDARD | 1 | |
| SORFIT 146/151/1 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-96 PG 14&15 FIGURE 5&6. Includes Test Report and Certificate of Conformance. | 1 | |
| SORFIT 146/151/2 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 4 53-20-96 PG 14&15 FIGURE 5&6. Includes Test Report and Certificate of Conformance. | 1 | |
| SORFIT 146/154/1 | BAE REFERENCE STANDARD 146 SERIES / AVRO-RJ SERIES PART 6 53-20-95 PG 11 FIG 5. Includes Test Report and Certificate of Conformance. | 1 | |
| 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. | 1 | |
| SORFIT 146/166/1 | BAE REFERENCE STANDARD 146-RJ 53-238 53-30-15 PT 6 FIGURE 5&6 PAGES 9&10. Includes Test Report and Certificate of Conformance. | 1 | |
| SORFIT 146/166/2 | BAE REFERENCE STANDARD 146-RJ 53-238 53-30-16 PT 6 FIGURE 4-6 PAGES 8-10. Includes Test Report and Certificate of Conformance. | 1 | |
| SPCP12L | REFERENCE STANDARD. PROCEDURE B CONFIG 2 | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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. | 1 | |
| 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)... | 1 | |
| ST4340 | STANDARD, CALIBRATION REFERENCE | 5 | |
| ST8870-1 | BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 20 FIGURE 7. GR/EP SKIN/NOMEX CORE DISBOND DEFECT | 4 | |
| ST8870-4 | BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 19 FIGURE 6. GR/EP SKIN/NOMEX CORE DISBOND DEFECT | 4 | |
| ST8870-7 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 1-10 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK | 4 | |
| ST8870-8 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 11-20 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK | 5 | |
| ST8870-9 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 21-30 PLY), PT 1 51-04-00, PAGE 19 FIGURE 8. SUPPLIED WITH HOLDING BLOCK | 4 | |
| ST8870B-7 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 1-10 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance. | 3 | |
| ST8870B-8 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 11-20 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance. | 3 | |
| ST8870B-9 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 21-30 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance. | 3 | |
| ST8870C-7 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 1-10 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance. | 2 | |
| ST8870C-8 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 11-20 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance. | 2 | |
| ST8870C-9 | BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 21-30 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance. | 2 | |
| ST8870D | BOEING PERFORATED BONDED REFERENCE STANDARD ALUMINUM HONEYCOMB ALL PT4 78-30-01; PG.18 FIG.3 | 1 | |
| ST8871D | BOEING COMPOSITE REFERENCE STANDARD 5-10-15 PLY 737 PT 4; 78-30-02 PG.10 FIGURE 4 & 777 PT 4 78-30-03 | 4 | |
| STANDARD-B | 2/64" FLAT BOTTOM HOLE EQUIVALENT SURFACE NOTCH STANDARD (*ABOVE DESCRIPTION MUST BE ENGRAVED ON THE REFERENCE STANDARD) ..DRAWING "B" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR) MATERIAL=7075-T6 | 1 | |
| STD-00107021 | Avcon Industries LFEC Calibration Reference Standard. BNC Document: 00107021, Rev. B Figure 7 Page 22. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| STR/146/RIT/5089 | BAE 146-RJ SERIES REFERENCE STANDARD 53-20-26 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance. | 1 | |
| STR/146/RP/5139 | BAE 146-RJ SERIES REFERENCE STANDARD 57-55-09 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance. | 1 | |
| TC4-255S | BOEING REFERENCE STANDARD TRANSDUCER POSITIONER TRANSDUCER POSITIONER TRANSDUCER POSITIONER CONTACT TRANSDUCER | 2 | |
| TEK-186-2024T3-12 | 12 Hole Reference Standard Similar to Boeing 186, 3/16" to 3/4", with .030" corner and .020" corner notches on the bottom plate, .040 Long x .020 Deep Midwall Notches on the top plate. 2024-T3 | 1 | |
| TEK-5154 | CUSTOM 2 ELEMENT RING TRANSDUCER FOR BORE HOLE INSPECTION WITH BOEING REFERENCE STANDARD 55-10-13 PAGE 9 FIGURE 2. TWO MICRODOT CONNECTORS "A" AND "B" | 1 | |
| TEK-6007 | Reference Standard, Sliding Probe Type, SPO-3932 | 1 | |
| TEK-767-3 | CALIBRATION REFERENCE STANDARD | 1 | |
| TEKIT-396 | Boeing Reference Standards, 737 PT6 53-30-44, PG7 FIG 2, Kit includes NDT396-36/36, NDT396-40/40, NDT396-45/40, NDT396-50/40, NDT396-56/40, Pelican case 1150 | 1 | |
| TI-6AI-6V-2SN | CALIBRATION REFERENCE STANDARD | 1 | |
| TI-6AL-6V-2SN | CALIBRATION REFERENCE STANDARD, NO.TI-6AL-6V-2SN, MADE FROM TITANIUM ALLOY (1.1% IACS), CONTAINS 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED NOTCHES, (BOMBARDIER INC. OR EQUIVALENT) | 3 | |
| TP-126 | Boeing reference standard; 51-00-00 | 1 | |
| 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. | 2 | |
| TP54-02-1 | AIRBUS REFERENCE STANDARD, NTM 53-41-86, A300-600 PT 6 51-10-01, A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| 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. | 2 | |
| U8860407 | ALUMINUM (7075-T6) MULTI-HOLE REFERENCE STANDARD WITH CERTIFICATE TRACEABLE TO NIST | 1 | |
| U8860842 | Boeing reference standard, NDT-398 | 1 | |
| UT-010-057 | BHTI REFERENCE STANDARD | 1 | |
| VC 010 | Boeing Reference Standard For MR-TCDL Modification (L3H). Material: 7050-T7451 or 7075-T7351 & 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| VC 011 | Boeing Reference Standard For MR-TCDL Modification (L3H). Material: 7050-T7451 or 7075-T7351 & 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| VC009 | BOEING R & D LFEC REFERENCE STANDARD Material: 7076-T6 Clad Aluminum. Fasteners HL18PB6-3, NAS620-10L, MS21042. Includes Test Report and Certificate of Conformance. | 1 | |
| VM650CIT-3A | CALIBRATION REFERENCE STANDARD – ROTARY PRPBE KIT | 1 | |
| W-19-1 | Boeing W-19 Reference Standard.-1 Assembly | 1 | |
| W-87 REF STD IBD | BOEING REFERENCE STANDARD. W-87 INBOARD 360 REFERENCE STANDARD. Materials: 2024-T351 and 7075-T651 Aluminum. Includes Test Report Traceable to NIST. | 1 | |
| W-87 REF STD OBD | BOEING REFERENCE STANDARD. W-87 OUTBOARD 360 REFERENCE STANDARD. Materials: 2024-T351 and 7075-T651 Aluminum. Includes Test Report Traceable to NIST. | 1 | |
| WNG-CB-Repair-0.622 | NDI CB Repair Reference Standard .622 diameter hole, 2" Wide x 11" Long, T=.272" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-0.685 | NDI CB Repair Reference Standard .685 diameter hole, 2" Wide x 11" Long, T=.320" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-0.747 | NDI CB Repair Reference Standard .747 diameter hole, 2" Wide x 11" Long, T=.389" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-0.810 | NDI CB Repair Reference Standard .810 diameter hole, 2" Wide x 11" Long, T=.500" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-0.870 | NDI CB Repair Reference Standard .870 diameter hole, 2" Wide x 11" Long, T=.272" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-0.932 | NDI CB Repair Reference Standard .932 diameter hole, 2" Wide x 11" Long, T=.563" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-0.997 | NDI CB Repair Reference Standard .997 diameter hole, 2" Wide x 11" Long, T=.583" Thick, T2=.500" Thick | 1 | |
| WNG-CB-Repair-1.057 | NDI CB Repair Reference Standard 1.057 diameter hole, 2" Wide x 11" Long, T=.583" Thick, T2=.500" Thick | 1 | |
| WNG-Steel-Doubler-0.625 | NDI Steel Doubler Reference Standard .625" diameter hole, 2" Wide x 11" Long, T=.500" Thick, T2=.500" Thick, 17-4PH | 1 | |
| WNG-Steel-Doubler-1.125 | NDI Steel Doubler Reference Standard 1.125" diameter hole, 2" Wide x 11" Long, T=.500" Thick, T2=.500" Thick, 17-4PH | 1 |
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