| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 126 | ALUMINUM REFERENCE STANDARD | 7 | |
| AFNDT-3151AL | ALUMINUM REFERENCE STANDARD | 1 | |
| HRS-15A | ALUMINUM REFERENCE STANDARD | 1 | |
| NDT1085-036 | ALUMINUM REFERENCE STANDARD | 3 | |
| RM150 | ALUMINUM REFERENCE STANDARD | 1 | |
| RM150-C30-2024T3 | ALUMINUM REFERENCE STANDARD | 1 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 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 | |
| 10RS-52-2-MLG-FTG-AF | MD-10 REFERENCE STANDARD FIGURE 1.3, SHEET 1&2. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. MDC-99K1082 | 1 | |
| 10RS.51-MLG-FTG-FF | MD-10 REFERENCE STANDARD FIGURE 1.1, SHEET 1&2. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. MDC-99K1082 | 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 | |
| 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 | |
| 145-44131-001 | REFERENCE STANDARD, GENERAL EDDY CURRENT TESTING, ALUMINUM ALLOY | 6 | |
| 171-00844-601 16E1 | EMBRAER REFERENCE STANDARD 7075-T7 ALUMINUM.Includes Test Report and Certificate of Conformance. | 1 | |
| 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 | |
| 1920166 (NRK-3AL) | REFERENCE STANDARD ALUMINUM 7075 | 1 | |
| 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 | |
| 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. | 2 | |
| 2213E | REFERENCE STANDARD-7075-T6 ALUMINUM | 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 | |
| 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 PROCEDURE 2 Figure 1 (Sheets 1- 2) Pages 4- 5. Material: 7075-T6 Aluminum and AL-NI Bronze Bushing Per AMS 4640. Includes Test Report and Certificate of Conformance. | 1 | |
| 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 | |
| 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 | |
| 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 | |
| 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. | 6 | |
| 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 | |
| 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 | |
| 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 | |
| 1920166 | OLYMPUS REFERENCE STANDARD ALUMINUM 7075-T651 / 7075-T73 | 1 | |
| 55-36-01 | UT CALIBRATION REFERENCE STANDARD , STEP WEDGE, 7000 SERIES ALUMINUM, GENERIC AS PER ATR 72 NTM 55-36-01 | 1 | |
| 57-10-119/1 | 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 | |
| 57-54-103C | CUSTOM BOEING REFERENCE STANDARD 7075-T6 ALUMINUM | 1 | |
| 7075-T6 | REFERENCE STANDARD, GENERAL EDDY CURRENT TESTING, ALUMINUM ALLOY | 1 | |
| 717RS10-C | 717-200 REFERENCE STANDARD FOR THE LOWER CENTER WING SKIN PANELS AT STRINGER 16 &18. PAGES 1-11. MATERIAL: 2024-T3, 7075-T6 &7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS12 | 717-200 REFERENCE STANDARD...FIG. 1.16 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS15 | 717-200 REFERENCE STANDARD...FIG. 1.4 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS20 | 717-200 REFERENCE STANDARD...FIG. 1.21 SHEET 1-3, PAGES 1-3. MATERIAL: 2014-T6 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS23 | 717-200 REFERENCE STANDARD...FIG. 1.8 SHEET 1-5, PAGES 1-5. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS2A | 717-200 REFERENCE STANDARD...FIG. 1.12 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS2B | 717-200 REFERENCE STANDARD...FIG. 1.13 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS2C | 717-200 REFERENCE STANDARD...FIG. 1.14 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS2D | 717-200 REFERENCE STANDARD...FIG. 1.15 SHEET 1-4, PAGES 1-4. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS4 | 717-200 REFERENCE STANDARD FIGURE 1.17 SHEETS (1-4 ), PAGES 1-4. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS7 | 717-200 REFERENCE STANDARD...FIG. 1.22 SHEET 1-7, PAGES 1-7. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RS8 | 717-200 REFERENCE STANDARD...FIG. 1.23 SHEET 1-6, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RST5 | 717-200 REFERENCE STANDARD...FIG. 1.18 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 717RST6 | 717-200 REFERENCE STANDARD...FIG. 1.19 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 7637987-9 | A53-142 Douglas DC-9 7637987-9 Reference Standard Assembly 2024-T3 Clad Aluminum. Figure 1, Sheets 2&3 | 1 | |
| 7947479-10 | REFERENCE STANDARD ALUMINUM 7075-T6 MULTI-PURPOSE TESTING PHTOOLSP/N 7947479-10, NRK-3A (REFERENCE USAF TO-33B-1-1) | 3 | |
| 80RS14 | 717-200 REFERENCE STANDARD...FIG. 1.6 SHEET 1-4, PAGES 1-4. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| 80RS18 | 717-200 REFERENCE STANDARD...FIG. 1.5 SHEET 1-5, PAGES 1-5. MATERIAL: 7075-T6 CLAD ALUMINUM, 2014-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.53.80.003 | 2 | |
| 80RS19 | 717-200 REFERENCE STANDARD...FIG. 1.2 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 or 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 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 | |
| 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 | |
| 98S51605001-218 | 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 | |
| 98S51605001-224 | 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 | |
| 98S53305004-000 | ATR REFERENCE STANDARD PT 5 53-51-01 Figure 501, Page 506 Does not include Stringer Hook. Material: 2024-T3 Aluminum. | 5 | |
| 98S57205024-200 | ATR REFERENCE STANDARD PT 4 57-24-09 PAGE 403 FIGURE 401. MATERIAL: 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 3 | |
| 98S57205030.004 | UT CALIBRATION REFERENCE STANDARD , STEP WEDGE, 7000 SERIES ALUMINUM, GENERIC | 5 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 99D57103009000 | AIRBUS REFERENCE STANDARD. MATERIAL: 7175-T7 ALUMINUM ANODIZED. PAINT WITH PRIMER | 4 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 99F53303096000 | AIRBUS REFERENCE STANDARD A330/A340-200/-300 53-30-29-PB4. MATERIAL: 2024-T351 ALUMINUM. 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 | |
| 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 | |
| 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 | |
| 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 | |
| 99F57103051000 | AIRBUS REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM WITH PROTECTIVE FINISH 13-002 and PAINT PRIMER 16-006. APPLY TOP COAT 16-008 | 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 | |
| 99F57203002000 | AIRBUS REFERENCE STANDARD A330 PT 4 57-20-86-991-003-A. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204105000 | AIRBUS REFERENCE STANDARD PT 4 57-20-49-991-006-A, 57-20-49-270-801-A01 & 57-20-49-270-802-A01. Material: 2024-T351 Aluminum. lncludes Test Report and Certificate of Conformance. | 3 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 99L53103000000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-11-03-991-009-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103001000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-11-12-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103002000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-11-03-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103004000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-09-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103005000 | A380 REFERENCE STANDARD 7010 ALUMINUM; FIGURE:53-11-23-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103006000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-07-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103008000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-11-11-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103010000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-31-24-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103012000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.53-11-22-991-009-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53103013000 | A380 REFERENCE STANDARD 7010 OR EQUIVALENT ALUMINUM; FIG.53-11-20-991-003-A SHEET 1. 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 | |
| 99L53303002000 | A380-800 REFERENCE STANDARD 2024 ALUMINUM; FIGURE:53-31-22-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303009000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIGURE:53-31-20-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303016000 | A380 REFERENCE STANDARD 7075-T6 OR 7075-T7 ALUMINUM; FIGURE:53-31-30-991-003-A. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L53303017000 | A380 REFERENCE STANDARD 7050-T73 OR 7075-T73 ALUMINUM; FIG.53-31-30-991-009-A. 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 | |
| 99L53303032000 | A380-800 REFERENCE STANDARD 7075 ALUMINUM; FIGURE:53-31-53-991-003-A. 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 | |
| 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 | |
| 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 | |
| 99L55209001000 | AIRBUS REFERENCE STANDARD 55-21-03-991-003-1. 7050-T7451 ALUMINUM | 1 | |
| 99L57103002000 | A380-800 REFERENCE STANDARD FIGURE:53-11-03-991-008-A. Material: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 99L57203005000 | A380 REFERENCE STANDARD 2024-T351 ALUMINUM; FIG.57-11-03-991-008-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 | |
| 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 | |
| 9RS11 | 717-200 REFERENCE STANDARD...FIG. 1.3 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| 9RS5 | DC-9 REFERENCE STANDARD PAGES 17-20, SHEETS 1-4. MATERIAL: 2024-T3 CLAD ALUMINUM | 2 | |
| 9RST1 | 717-200 REFERENCE STANDARD...FIG. 1.11 SHEET 1-3, PAGES 1-3. MATERIAL: 2024-T3 and 2024-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.FASTENER (MS20470AD8, NAS1478-6 + NAS1080-8) | 1 | |
| 9RST8 | 717-200 REFERENCE STANDARD FIGURE 1.10 SHEETS (1-6 ), PAGES 1-6. MATERIAL: 2024-T3 ALUMINUM and PHENOLIC(DMS1558). Includes Test Report and Certificate of Conformance. FASTENER (NAS1203 + NAS1252-10H + NAS679-A3, S432867-8 + NAS1080-8) | 1 | |
| 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 | |
| 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 | |
| AFHS20-2A-5 | Aluminum Multi-hole reference standard with certificate. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains two EDM corner... | 1 | |
| AFNDT-1000/SA | 12 HOLE REFERENCE STANDARD ALUMINUM WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-1000SA-1 | 12 HOLE REFERENCE STANDARD ALUMINUM WITH A .020" MID WALL NOTCH, .030" CORNER NOTCH, .050" CORNER NOTCH, .010" ,.020", .040: .050" SURFACE NOTCH. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-1025AL | Multi-Hole reference standard. Material: 7075-T6 Aluminum. 12 Holes 3/16", 7/32", 1/4" ,9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4" .020" x .020" x .005" Wide ± .002" Through EDM Notches in each hole. Standard also includes 3 surface EDM n | 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-1035/7075 | 5 hole reference standard sizes; 1/4", 5/16", 3/8", 7/16" and1/2" inch diameters.( .030" X .030" x .005" +/-.001" corner EDM notch. 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2005A | 12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001". Includes Test Report and Certificate o | 1 | |
| AFNDT-2006A | 12 HOLE REFERENCE STANDARD 7075-T6 aluminum. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X. 030" x.004" ±.002" WIDE CORNER EDM NOTCH in EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010", .020",... | 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-2030/2014-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2014-T6 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2030/2014-T651 | DDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2014-T651 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2030/2024 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T3 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2030/2024-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T6 ALUMINUM. SIZE: 4.0"L x 1.0"W x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2030/6061-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008"(0.2mm), .020"(0.5mm), .040"(1.0mm) (.004"W +/- .002), 6061-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance and Material Certification. | 1 | |
| AFNDT-2030/7075-T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2030/7075-T7 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008", .020", .040" (.004"W +/- .002), 7075-T7 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2035 | 6 Hole reference standard (Aluminum 7075-T6 with certifications). Hole Sizes: 1.0", 1.125", 1.250" ,1.500", 1.625", 1.750", ( .030 x .030 x .006 +/- .001) Corner EDM Notches and .010, .020, .040 Surface notches).. Includes Test Report and Certificate | 1 | |
| AFNDT-2042/AL | CUSTOM 5 HOLE REFERENCE STANDARD MADE OF 7075-T6 ALUMINUM WITH (0.5mm X 0.5mm +/- .05mm) CORNER EDM FLAWS. HOLE SIZE : 13/64", 19/64", 23/64", 7/16" & 31/64". Includes Test Report and Certificate of Conformance. | 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-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-2065 | Olympus Aluminum multi-hole reference standard. Contains 5 hole sizes; 7/16, 1/2, 9/16, 3/4 and 1.0" inch hole diameters.( .030" x.030" corner EDM notch in each hole). Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2066A | 12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .001" WIDE THRU NOTCH. .008", .020", .040" SURFACE NOTCHES. .005" +/-.001". Includes Test Report and | 1 | |
| AFNDT-2069AL | 13 HOLE REFERENCE STANDARD 7075-T6 aluminum. Hole Sizes: 3/16(.1875), 13/64(.203), 7/32(.218), 15/64(.234),1/4(.250), 17/64(.265), 9/32(.281), 19/64(.297), 5/16(.312),21/64(.328),11/32(.343), 23/64(.359), 3/8(.375). EDM NOTCH: .030" X. 030" x.005" ±.... | 1 | |
| AFNDT-2073AL | 12 HOLE REFERENCE STANDARD 7075-T6 aluminum. Hole Sizes: 25/64(.390), 13/32(.406), 27/64(.421),7/16(.437), 29/64(..453), 15/32(..468), 31/64(.484),1/2(.500), 33/64(.515),17/32(.531), 35/64(.546), 9/16(.562). EDM NOTCH: .030" X. 030" x.005" ±.001" WIDE... | 1 | |
| AFNDT-2074 | CUSTOM SURFACEREFERENCE STANDARD, 3 EDM SLOTS .008",.020",.040" .007" MAX WIDTH. MATERIAL: 7075-T6 ALUMINUM. SIZE: 4.0 x 1.5 x .25". Includes Test Report and Certifictate of Conformance. | 1 | |
| AFNDT-2076AL | 10 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. Hole Sizes: 1/8", 5/32", 3/16", 7/32" ,1/4", 9/32", 5/16", 3/8", 7/16", 1/2", .030" X. 030" x.005" +/- .001" WIDE. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2106 | 3 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM.. HOLE SIZES: 5/32", 3/16", 1/4" TOTAL OF 3 EDM CORNER NOTCHES .030" x .030".N Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2107/7075T6 | EDDY CURRENT SURFACE REFERENCE STANDARD. EDM FLAWS: .008", .020", .040" (.005" Maximum Width). MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25"H. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2109 | 15 Hole aluminum reference standard, material 7075-T6, hole sizes: 1/8, 5/32, 11/64, 3/16, 13/64, 7/32, 15/64, 1/4, 17/64, 9/32, 19/64, 5/16, 21/64, 11/32, 23/64. With .030 x .030 and .020 x .020 Corner EDM Notches. Includes Test Report and Certificat | 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-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-2132/2024-T3 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8, 5/32, 11/64, 3/16, 13/64, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 17/32, 9/16, 5/8, 11/16, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001. MID-WALL EDM NOTC | 1 | |
| AFNDT-2132/7075-T6 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8, 5/32, 11/64, 3/16, 13/64, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 17/32, 9/16, 5/8, 11/16, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001. MID-WALL EDM NOTC | 1 | |
| AFNDT-2133/7075T6 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001. Inclu | 1 | |
| AFNDT-2133AL-1 | 20 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 9/16, 1/2, 17/32, 9/16,19/32, 5/8, 21/32, 11/16, 23/32, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001 NOTCH | 1 | |
| AFNDT-2140/7075 | 11 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH .030"x.030" CORNER EDM NOTCH IN EACH HOLE.. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2141AL | 12 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .030" x .030" CORNER EDM NOTCH and .020" MID-WALL EDM NOTCH IN EACH HOLE. Tolerance: .005" +/-.001". Includes Test Repo | 1 | |
| AFNDT-2151AL | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.005"W + .001"), MATERIAL: 5086 H32 ALUMINUM. (29.0% IACS. SIZE: 80mm(3.15") L +5mm(.197") x 30mm(1.18") W +5mm(.197") x 8mm(.315") THICK +3mm(.118"). Includes Mill Certifica... | 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-3024AL | 12 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .030" X .030" X .005" +/- .001" WIDE CORNER EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG . | 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-3027AL | MHS style Multi-Hole reference standard (Aluminum 7075-T6 with certifications). 12 Holes 3/16", 7/32", 1/4" ,9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 11/16" ( .030 x .030 x .006 +/- .001) Corner Notches and .010, .020, .040 Surface notch... | 1 | |
| AFNDT-3028AL | 3i-Hole reference standard (Aluminum 7075-T6 with certifications). Hole Sizes , 7/16", 1/2" and 11/16" ( .030 x .030 x .006 +/- .001) Corner Notches. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3032 | 3 HOLE 100° COUNTERSINK REFERENCE STANDARD 2024-T3 ALUMINUM, PLATE SIZE: 3.0" x 2.0" x 1/4" . HOLE SIZES: 5/32", 3/16" and 1/4" TOTAL OF 3 EDM NOTCHES .040" +0.004"/-0.000" Long x .007" Max Width Through the Depth of the Countersink. | 1 | |
| AFNDT-3032-1 | 3 HOLE 100° COUNTERSINK REFERENCE STANDARD 7075-T6 ALUMINUM, PLATE SIZE: 3.0" x 2.0" x 1/4" . HOLE SIZES: 3/16", 7/32" and 1/4" TOTAL OF 3 CORNER EDM NOTCHES: .030" +0.004"/-0.000" Long x .007" Max Width Through the Depth of the Countersink. Includes Tes | 1 | |
| AFNDT-3036AL | CUSTOM 2 HOLE EDDY CURRENT REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES: .250" and .875" WITH a .030" x .030" x .007" MAX WIDTH CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3051AL | (Aluminum Multi-hole reference standard with certificate. Contains 2 rows of 6 hole sizes. The first row has no flaws or side drilled holes. The second row includes side drilled holes. Hole Sizes: 3/16", 1/4", 5/16", 3/8", and 1/2". Material: 7075-T6 ... | 1 | |
| AFNDT-3052AL | (Aluminum Multi-hole reference standard with certificate. Contains 2 rows of 29 hole sizes. The first row has no flaws or side drilled holes. The second row includes side drilled holes. Hole Sizes: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32"... | 1 | |
| AFNDT-3056AL | 10 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. Hole Sizes: 3/16", 7/32" ,1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16', 5/8". Corner EDM Notches: .020" x .020" x .005" +/- .001" Wide and Mid-Wall EDM Notches .020" x .020" x .005" +/- .001" Wide in Each... | 1 | |
| AFNDT-3061AL | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .005", .010", .020" (.004"W +/- .002), 7075-T7 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 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-3074AL | 12 Hole reference standard. Material: 2024-T3 Aluminum. Contains 12 hole sizes; 3/16 inch (4.74mm) 7/32 inch (5.53mm) 1/4 inch (6.35mm) 9/32 inch (7.13mm) 5/16 inch (7.92mm) 11/32 inch (8.71mm) 3/8 inch (9.52mm) 7/16 inch (11.09mm) 1/2 inch (12.7mm) 9/16 | 1 | |
| AFNDT-3081AL | 3 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM.. HOLE SIZES: 5/16", 3/8", 7/16" TOTAL OF 3 EDM CORNER NOTCHES .030" x .030". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3116 | 16 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM. 2 OF EACH HOLE SIZES: 3/16", 13/64" 7/32" , 1/4", 17/64", 9/32", 7/16", 9/16". .030" x .030" CORNER NOTCH IN 1st HOLE SET and .060" x .020" MID-WALL NOTCH IN 2nd HOLE SET. Tolerance: .006" +/-.001". Inclu... | 1 | |
| AFNDT-3120AL | 11 hole Reference Standard 7075-T6 Aluminum. Contains 10 hole sizes; 7/64, 1/8, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 5/8, 3/4 and 1.0 inch diameters.( .030X.030 Corner EDM Notch and 3 Surface EDM Notches at .010", .020", .040" DEEP x .750" LONG.) Includes T... | 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-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-3147AL | 7 HOLE 100° COUNTERSINK REFERENCE STANDARD 2024-T3 ALUMINUM, PLATE SIZE: 3.0" x 2.5" x 3/8" . HOLE SIZES: 5/32", 3/16", 7/32",1/4", 5/16",3/8", 7/16". TOTAL OF 7 EDM NOTCHES .030" +0.002"/-0.002" Long x .007" Max Width Through the Depth of the Countersin | 1 | |
| AFNDT-3148AL | 13 HOLE REFERENCE STANDARD, 7075-T6 ALUMINUM. HOLE SIZES: 5/32", 3/16", 7/32", 1/4", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4", 7/8" & 1". THRU EDM NOTCHES IN EACH HOLE, Depth: 0.040" +/- 0.001 x Width : 0.005" + 0 - 0.002". Includes Certification R... | 1 | |
| AFNDT-3151AL | 15 HOLE REFERENCE STANDARD 7075-T6 ALUMINUM, HOLE SIZES: 1/8, 5/32, 3/16, 7/32 ,1/4, 9/32, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4,,7/8,1.0" .030" x .030" CORNER NOTCH .005+/-.001, 3 SURFACE NOTCHES .750"L x .010",.020",.040" DEEP. Includes Test Report and | 1 | |
| AFNDT-3153/7075T6 | 11 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (1/8, 5/32, 3/16, 7/32, 1/4, 9/32, 5/16, 3/8, 7/16, 1/2, 9/16), WITH .050"x.050" .005±.001 CORNER EDM NOTCH IN EACH HOLE. | 1 | |
| AFNDT-3159AL | 8 HOLE REFERENCE STANDARD, MATERIAL: 2024-T3 ALUMINUM., HOLE SIZES: 1/8", 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", .020" THROUGH NOTCH .005+/-.001. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3166AL | CUSTOM 13 HOLE REFERENCE 3 PLATE STANDARD, 7075-T6 ALUMINUM. HOLE SIZES: 5/32, 3/16, 7/32, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 3/4, 7/8, 1.0". Includes Test Report and Certificate of Conformance. | 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-3189AL | 11 HOLE REFERENCE STANDARD IN 2024-T3 ALUMINUM; HOLE SIZES: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH .020" x .020" x .005" +/-.001" CORNER EDM NOTCH IN EACH HOLE. Includes Certification Report and Certificate of Conformance. | 1 | |
| AFNDT-3204/7075 | 8 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (1/8, 5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2), WITH .020"x.020" CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3210 | SURFACE REFERENCE STANDARD, ONE EDM NOTCH .030" Deep x .040" wide x .060 long ( +/- .002), MATERIAL: 2024-T3 ALUMINUM. SIZE: 2.0"L x 2.0"W x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3212AL | 13 HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. HOLE SIZES: 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 3/8", 7/16", 1/2", 9/16", 5/8", 23/32". EACH HOLE CONTAINS A CORNER EDM NOTCH 030" x .030" x Width : 0.005" +/- 0.002". Includes Certif... | 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-3225AL | 12 HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 ALUMINUM. Hole Sizes: (3/16", 7/32" ,1/4", 9/32", 5/16",11/32", 3/8", 7/16", 1/2", 9/16", 5/8", 3/4"), .020" X .004" +/- .002" WIDE THROUGH EDM NOTCH IN EACH HOLE and 3 SURFACE EDM NOTCHES .750" LONG .010"... | 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-3231-1 | Custom McDonnell Douglas Low Frequency Eddy Current reference standard, 06-20-01 Figure 9 sheets 1-4. Material: 2024-T3 or 7075-T6 Aluminum.Fasteners: (CR3223-5 & MS21141-5). Includes Test Report and Certificate of Confromance. | 1 | |
| AFNDT-3239AL | 3 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM. HOLE SIZES: 1/4", 5/16", 3/8" TOTAL OF 3 EDM CORNER NOTCHES .030" x .030". 3 EDM SURFACE NOTCHES 0.008", 0.020", 0.040". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3240AL | Aluminum multi-hole reference standard. Contains 5 hole sizes; 1/8, 5/32, 3/16, 7/32 and 1/4" inch hole diameters.( .030" x.030" corner EDM notch in each hole). Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3241AL | Aluminum Multi-hole reference standard. Material: 7075-T6 Aluminum. Contains 20 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 1.0" inch. Each hole contains on the | 1 | |
| AFNDT-3251AL | 12 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM. HOLE SIZES: 1/8", 3/16" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8",11/16", 3/4", 13/16" .030" x .030" CORNER NOTCH and .020" x .020" CORNER NOTCH IN EACH HOLE. Tolerance: .005" +/-.001", 4 SURFACE EDM NOTCH | 1 | |
| AFNDT-3255AL | 11 HOLE REFERENCE STANDARD in 7075-T6 Aluminum; Hole Sizes: (5/32, 3/16,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), With a .020" x .020" x .005" +/-.002" Corner EDM Notch in each hole. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3260AL | Olympus Style Aluminum multi-hole reference standard. Contains 5 hole sizes; 2.0mm, 2.5mm, 3.0mm, 3.5 and 4.0mm hole diameters. EDM notch 0.5mm deep in each hole, length is half of the material thickness. Material: 7075-T76 Aluminum 15mm Thick. Includes T | 1 | |
| AFNDT-3261AL | Olympus Style Aluminum multi-hole reference standard. Contains 11 hole sizes; 16.5mm, 17.0mm, 17.5mm, 18.0mm, 18.5mm, 19.0mm, 19.5mm, 20.0mm, 20.5mm, 21.0mm, and 21.5mm hole diameters. EDM notch = 0.5mm corner EDM notch and 0.5mm deep in each hole, length | 1 | |
| AFNDT-3262AL | Olympus Style Aluminum multi-hole reference standard. Contains 21 hole sizes; 4.0mm, 4.5mm 5.0mm, 5.5mm, 6.0mm, 6.5mm, 7.0mm, 7.5mm, 8.0mm, 8.5mm, 9.0mm, 9.5mm, 10.0mm, 10.5mm, 11.0mm, 11.5mm, 12.0mm, 13.0mm, 14.0mm, 15.0mm and 16.0mm hole diameters. EDM | 1 | |
| AFNDT-3262TI | Olympus Style Aluminum multi-hole reference standard. Contains 21 hole sizes; 4.0mm, 4.5mm 5.0mm, 5.5mm, 6.0mm, 6.5mm, 7.0mm, 7.5mm, 8.0mm, 8.5mm, 9.0mm, 9.5mm, 10.0mm, 10.5mm, 11.0mm, 11.5mm, 12.0mm, 13.0mm, 14.0mm, 15.0mm and 16.0mm hole diameters. EDM | 1 | |
| AFNDT-3270AL | Aluminum Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 3 | 1 | |
| AFNDT-3271AL | Aluminum Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 3 | 1 | |
| AFNDT-3273TI | Aluminum Multi-hole reference standard. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/8", 29/32", 15/16", 3 | 1 | |
| AFNDT-3287AL | Custom multi-hole 100° countersink reference standard Material: 7075-T6 Aluminum. Hole sizes: 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2". Countersink holes opposite side. Thru hole EDM notches in each hole, .020" Deep x .005" Wide +/-.001". Includes T | 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-3299/7075-T6 | 12 HOLE REFERENCE STANDARD . HOLE SIZES: 1/8", 5/32", 3/16", 7/32" 1/4" , 5/16", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .005" +/- .002" WIDE MID-WALL EDM NOTCH. Material: 7075-T6 Aluminum. Includes Test Report and Certificate of Conformance. | 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-3304/7075-T6 | 12 Hole reference standard. Material: 7075-T6 Aluminum. Contains 12 hole sizes; 3/16 inch (4.74mm) 7/32 inch (5.53mm) 1/4 inch (6.35mm) 9/32 inch (7.13mm) 5/16 inch (7.92mm) 11/32 inch (8.71mm) 3/8 inch (9.52mm) 7/16 inch (11.09mm) 1/2 inch (12.7mm) 9/16 | 1 | |
| AFNDT-3306/2024T3 | EDDY CURRENT SURFACE REFERENCE STANDARD, METRIC NOTCHE SIZES: 0.2mm, 0.5mm &1.0mm. WIDTH = .005" +/- .002" MATERIAL: 2024-T3 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3306/7075T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, METRIC NOTCHE SIZES: 0.2mm, 0.5mm &1.0mm. WIDTH = .005" +/- .002" MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3312AL | 12 HOLE REFERENCE STANDARD, 7075-T6 Aluminum. HOLE SIZES: 3/16", 7/32" 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/16" 5/8", 3/4" .020" x .004" +/- .001" Wide Thru EDM Notch. A Total of 4 Surface EDM Notches .005", .010" .020", .040" Tolerance: . | 1 | |
| AFNDT-3315AL | EDDY CURRENT SURFACE REFERENCE STANDARD, 4 EDM NOTCHES .005", .010", .020" and .050" x (.004"W +/- .002). MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 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-3332AL | 20 HOLE REFERENCE STANDARD 2024-T3 ALUMINUM. HOLE SIZES: 1/8, 5/32, 11/64, 3/16, 13/64, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 17/32, 9/16, 5/8, 11/16, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001. TOTAL OF 20 SURFA | 1 | |
| AFNDT-3357/2024T4 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .008"(0.2mm), .020"(0.5mm), .040"(1.0mm) (.004"W +/- .001), 2024-T4 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance and Material Certification. | 1 | |
| AFNDT-3369/7075T6 | Custom 8 hole 100° countersink reference standard Material: 7075-T6 Aluminum. Hole sizes: 5/32", 3/16", 7/32" 1/4", 5/16", 3/8", 7/16", 1/2". Countersink holes opposite side. Thru hole EDM notches in each hole, .020" Deep x .005" Wide +/-.001". Includes | 1 | |
| AFNDT-3370/7075T6 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .010"(0.25mm), .020"(0.5mm), .030"(0.76mm) (.004"W +/- .002), 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3378-1AL | 20 HOLE REFERENCE STANDARD. MATERIAL: 7075-T6 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, 9/16, 17/32, 9/16,19/32, 5/8, 11/16, 3/4. TOTAL OF 20 CORNER EDM NOTCHES .030 x .030 x .005 +/-.001. Inc... | 1 | |
| AFNDT-3378AL-1 | 20 HOLE REFERENCE STANDARD. MATERIAL: 2024-T3 ALUMINUM . HOLE SIZES: 1/8, 5/32, 11/64, 3/16, 13/64, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 17/32, 9/16, 5/8, 11/16, 3/4. TOTAL OF 40 CORNER EDM NOTCHES .020 x .020 X .005 ±.001 & .03... | 1 | |
| AFNDT-3387AL | 6 Hole Metric reference standard. Material: 7075-T6 Aluminum. Hole Sizes: 20mm, 21mm, 22mm, 23mm, 24mm and 25mm. Corner EDM Notches: 1mm x 1mm x .15mm(.039" x .039" x .006"±.001"). Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3395 | CUSTOM EC SKIN INSPECTION REFERENCE STANDARD. Contains various EDM Nothes in the Upper and Lower Skin. Upper Skin Thickness of .080" and Lower Skin Thickness of .100" Thick. Standard Physical Size = 13.5" Long x 5.15" Wide. MATERIAL: 2024-T3 ALUMINUM. I | 1 | |
| AFNDT-3402AL | Metric Aluminum multi-hole reference standard. Contains 11 hole sizes; 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, and 20mm hole diameters. EDM notch = 0.5mm x 0.5mm deep corner EDM notch in each of the Countersink Holes, 1mm x 1mm corner | 1 | |
| AFNDT-3402AL-1 | Metric Aluminum multi-hole reference standard. Contains 11 hole sizes; 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, and 20mm hole diameters. EDM notch = 0.5mm x 0.5mm deep corner EDM notch in each of the Countersink Holes, 1mm x 1mm corner | 1 | |
| AFNDT-3402TI | Metric Aluminum multi-hole reference standard. Contains 11 hole sizes; 10mm, 11mm, 12mm, 13mm, 14mm, 15mm, 16mm, 17mm, 18mm, 19mm, and 20mm hole diameters. EDM notch = 0.5mm x 0.5mm deep corner EDM notch in each of the Countersink Holes, 1mm x 1mm corner | 1 | |
| AFNDT-3421/7075T6 | 12 HOLE REFERENCE STANDARD IN 7075-T6 ALUMINUM; HOLE SIZES: (5/32, 3/16, 7/32,1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8,11/16, 3/4), WITH A .020"x.020" and .030"x.030" CORNER EDM NOTCH IN EACH HOLE. Includes Test Report and Certificate of Conformance | 1 | |
| AFNDT-3423 | Eddy Current Reference Standard. Dimensions: 4" x 0.25" x 1" Material: Aluminum 7075-T7. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3442AL | Aluminum Multi-hole reference standard. Material: 7075-T6 Aluminum. Contains 10 hole sizes; 1/8 inch (3.175mm), 3/16 inch (4.74mm),1/4 inch (6.35mm), 5/16 inch (7.92mm), 3/8 inch (9.52mm), 7/16 inch (11.09mm), 1/2 inch (12.7mm), 9/16 inch (14.27mm), 5/8 i | 1 | |
| AFNDT-3474AL | 12 Hole reference standard. Material: 7075-T6 Aluminum. Contains 12 hole sizes; 1/8 inch (3.175mm), 5/32 inch (3.96mm), 3/16 inch (4.74mm), 1/4 inch (6.35mm), 5/16 inch (7.92mm), 3/8 inch (9.52mm), 7/16 inch (11.09mm), 1/2 inch (12.7mm), 9/16 inch (14.... | 1 | |
| AFNDT-3481AL | Metric Aluminum Multi-hole reference standard. Material: 2024-T3 Aluminum. Contains 28 holes; 3.6mm, 4.0mm, 4.4mm, 4.8mm, 5.2mm, 5.6mm, 6.0mm, 6.4mm, 6.8mm, 7.2mm, 7.6mm, 8.0mm, 8.4mm, 8.8mm, 9.2mm, 9.6mm, 10.0mm, 10.4mm, 10.8mm, 11.0mm, 11.4mm, 11.8mm... | 1 | |
| AFNDT-3503AL | Aluminum Multi-hole reference standard. Material: 7075-T6 Aluminum. Contains 12 hole sizes; .154" (3.9mm), .189" (4.8mm) .217"(5.50mm), .248"(6.3mm), .281"(7.13mm), .312"(7.92mm), .344" (8.71mm), .375"(9.52mm), .437" (11.09mm), .500"(12.7mm), .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-3522AL | CUSTOM EDDY CURRENT SURFACE REFERENCE STANDARD, 3 EDM SLOTS .008",.020",.040" .006" ±.001". MATERIAL: 7075-T6 ALUMINUM. SIZE: .312" THICK x 1.375 WIDE x 3.156". Includes Test Report and Certifictate of Conformance. | 1 | |
| AFNDT-3524AL | 4 HOLE REFERENCE STANDARD. Material: 7075-T6 Aluminum 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-3534/2024T3 | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHES .010"(0.254mm), .020"(0.5mm), .030"(.762mm) (.004"W +/- .002), 2024-T3 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3546AL | EDDY CURRENT SURFACE REFERENCE STANDARD, NOTCHE SIZES: .005"(.127mm) , .020"(0.5mm), .050"(1.27mm) (.005"W +/- .001). MATERIAL: 7075-T6 ALUMINUM. SIZE: 1.0"W x 4.0"L x .25". Includes Test Report and Certificate of Conformance. | 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-CRJ200/CRS | SURFACE REFERENCE STANDARD, ALUMINUM, .005W x .008", .020", .040" EDM NOTCH DEPTHS . MATERIAL 2024-T3 AL...CRJ200 PART1 51-20-06 PG.9 | 1 | |
| AFS-0506 | 5MHZ 51° SHEAR WAVE IN ALUMINUM. CASE SIZE .50" W x .80"L x .37"H, REFERENCE STANDARD NDT624 | 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-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-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-02001-401 | REFERENCE STANDARD, GENERAL EDDY CURRENT TESTING, ALUMINUM ALLOY | 1 | |
| AGE-04362-401 | REFERENCE STANDARD, P/N 145-44131-001,ALUMINUM 7050-T7451 | 1 | |
| AGE-04900-401 | EDDY CURRENT INSTRUMENT - IMPEDANCEPLANE DISPLAY OR SIMILAR REFERENCE STANDARD, NDI, ALUMINUM7050-T7451 | 4 | |
| AHS29-1A-0 | (Aluminum Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/... | 1 | |
| AHS29-1A-2 | (Aluminum Multi-hole reference standard with certificate. Contains 29 holes; 1/8", 5/32", 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 13/32", 7/16", 15/32", 1/2", 17/32", 9/16", 19/32", 5/8", 21/32", 11/16", 23/32", 3/4", 25/32", 13/16", 27/32", 7/... | 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 | CALIBRATION REFERENCE STANDARD, BLOCK, 2024-T3 ALUMINUM ALLOY, CONDUCTIVITY BETWEEN 29% AND 32% IACS, CONTAINS 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP SURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ OR EQUIVALENT) | 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 | |
| AN670-55-31-102 | CALIBRATION REFERENCE STANDARD (CRS), MADE OF ALUMINUM WITH MULTIPLE LAYERS CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| 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 | |
| ARS-0824-7050 | Surface reference standard, 7050-T7 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | 1 | |
| ARS-0824-7050T74 | Surface reference standard, 7050-T74 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches (0.2mm, 0.51mm and 1.02mm). Reference standard overall dImensions 1 X 4 X 0.25 inches (2.54cm X 10.1cm X 6.35mm). EDM notches .007" W MAX | 1 | |
| ARS-0824-7075T6 | Surface reference standard, 7075-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 | 1 | |
| ARS-0824-7075T7 | Surface reference standard, 7075-T7 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | 1 | |
| ARS-0824-7075T73 | Surface reference standard, 7075-T73 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 | 1 | |
| ARS-0824/2024-T3 | Surface reference standard, 2024-T3 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | 1 | |
| ARS-0824/2024-T6 | Surface reference standard, 2024-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 | 1 | |
| ARS-0824/2024T6 | Surface reference standard, 2024-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .004" +/-.002" Wide EDM notches, .006" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.25 | 1 | |
| ARS-0824/6061T6 | Surface reference standard, 6061-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | 1 | |
| ARS-0824/7475-T7 | Surface reference standard, 7475-T7 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | 1 | |
| ARS-0824A | Surface reference standard, 7075-T6 Aluminum, with EDM notch depths of 0.008", 0.020" and 0.040" inches +/-.001 (0.2mm, 0.51mm and 1.02mm), Notch Width: .005" +/-.002" Wide EDM notches, .007" Wide MAX. Reference standard overall dImensions 1 X 4 X 0.... | 1 | |
| ASRS-123A | REFERENCE STANDARD ALUMINUM .008, .010, .040 | 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 | |
| CA12-1508A | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T7 ALUMINUM, 54-10-11 PAGE 634A FIG.603 SHEET 21B | 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 | |
| DAC ETBS AL-1T 2024-T3 0.063 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5, 06-10-02.005. MATERIAL: 2024-T3 ALUMINUM 0.063". Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETBS AL-1T 7075-T6 0.120 | DC Reference Standard, ETLF PROC 5, 06-10-02.005:FIG1 PG F1, 7075-T6 Aluminum | 1 | |
| DAC ETBS AL-1T 7075-T6 0.120:DAC ETBS AL-1T 7075-T73 0.120 | DC Reference Standard, ETLF PROC 5, 06-10-02.005:FIG1 PG F1, 7075-T73 Aluminum | 1 | |
| DAC ETBS AL-1T/ 0.032 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 7075-T7 ALUMINUM .032". Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETBS AL-1T/ 0.071 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 2024-T3 ALUMINUM .071". Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETBS AL-1T/ 0.090 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 7075-T6 ALUMINUM .090". Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETBS AL-1T/0.080 | MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 2024-T3 ALUMINUM .080". Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH AL | 7075-T6 Aluminum Multi-purpose Reference Standard 1/8" to 3/4" holes similar to RH120 | 1 | |
| DAC ETOH-AL-1/2 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 1/2 (0.500) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-1/4 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 1/4 (0.250) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-1/8 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 1/8 (0.125) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-11/16 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 11/16 (0.6875) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-3/16 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 3/16 (0.1875) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-3/4 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 3/4 (0.750) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-3/8 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 3/8 (0.375) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-5/16 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 5/16 (0.3125) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-5/8 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 5/8 (0.625) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-7/16 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 7/16 (0.4375) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL-9/16 | McDonnell Douglas Open Hole Eddy Current Reference Standard Part 6 06-20-01 Page F10 Figure 4. Material: Aluminum. 9/16 (0.5625) Inch Hole. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC ETOH-AL.04 | 717-200 OPEN HOLE REFERENCE STANDARD. FIG. 1.20, PAGE 1. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| DAC GSET AL.01 | 7075-T6 Aluminum Multi-purpose Reference Standard | 1 | |
| DAC GSET AL.01-MV | 7075-T6 Aluminum Multi-purpose Reference Standard, Modified Version, Surface notches are only .125"long from edge of standard | 1 | |
| DAC GSET AL.01-N1-N2 | General Surface Aluminum HFET Reference Standard MD-11 section 2-1 page 1 figure 1.1 | 1 | |
| DAC GSET MG.01 | Aluminum-Broze (10%-20% IACS) Reference Standard | 1 | |
| DAC GSET-AL.01 | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 7075-T6 ALUMINUM PER QQ-Q-250/12. | 1 | |
| DAC GSET-MG | MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 ALUMINUM BRONZE | 1 | |
| DC-10 FIG603/23 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 635 FIG.603 SHEET 23 | 1 | |
| DC-10 FIG603/24-Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 636C FIG.603 SHEET 24 | 1 | |
| DC-10 FIG603/27Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 639 FIG.603 SHEET 27 | 1 | |
| DC-10 FIG603/28LOWER/Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER) | 1 | |
| DC-10 FIG603/28UPPER/Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER) | 1 | |
| DC-10 FIG603/29Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 641 FIG.603 SHEET 29 | 1 | |
| DC-10 FIG603/30-AL | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 642 FIG.603 SHEET 30 | 1 | |
| DC-10 FIG603/43 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 655 FIG.603 SHEET 43 | 1 | |
| DRT74469 | Messier-Dowty Reference Standard, Aluminum, Appendix A Service Bulletin No. 146-32-174 Pg 4 Fg A2 | 2 | |
| E53-002A | EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance...Skin Thickness = .031"..Doubler = .040"..Filler = .031"..Stringer = .063" | 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 | |
| E53-004 | 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 | 2 | |
| 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 | |
| EX604-60024 | CALIBRATION REFERENCE STANDARD MULTI-LAYERED ALUMINUM ALLOY FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 2 | |
| EX604−60024 | Calibration reference standard multi−layered aluminum alloy fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 2 | |
| 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 | |
| EXBC670-59133 | CALIBRATION REFERENCE STANDARD MADE FROM ALUMINUM ALLOY CONTAINING 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 | |
| EXBC670-59145 | CALIBRATION REFERENCE STANDARD ALUMINUM ALLOY MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING 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 | |
| EXBC670-59162 | CALIBRATION REFERENCE STANDARD, ALUMINUM ALLOY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCH. (MHIRJ OR EQUIVALENT) | 1 | |
| EXBC670-59177 | CALIBRATION REFERENCE STANDARD ALUMINUM MULTIPLE LAYER FASTENED ASSEMBLY CONTAINING 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 | |
| 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 | |
| EXBC670−59133 | 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 | |
| EXBC670−59142 | Calibration Reference Standard made from aluminum alloy containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59145 | Calibration reference standard aluminum alloy multiple layers fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59153 | Calibration reference standard aluminum multiple layer fastened assembly containing 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 | |
| EXBC670−59162 | Calibration Reference Standard aluminum alloy that contains electrical discharge machined notch. (Bombardier Inc. or equivalent) | 1 | |
| EXBC670−59177 | Calibration reference standard aluminum multiple layer fastened assembly containing 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 | |
| GSE 333 | REFERENCE STANDARD, P/N 145-44131-001,ALUMINUM 7050-T7451 | 1 | |
| IIW TYPE 2 | CALIBRATION REFERENCE STANDARD BLOCK, ALUMINUM. (GE OR EQUIVALENT) | 1 | |
| M346 SPAR 4 STD-1 | CUSTOM REFERENCE STANDARD, H346 SPAR 4 STD-1 HOLE INTERFACE WITH FLAPS HINGE REWORK. MATERIAL: 7050-T7451 ALUMINUM. Includes Test Report and Certificate of Conformance. | 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 | |
| MD11-10 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 SECTION 2-1 PG.1 FIG.1.23.. 2024-T3 ALUMINUM | 1 | |
| MHS-12-1A-2 | ALUMINUM (7075-T6) MULTI-HOLE REFERENCE STANDARD WITH CERTIFICATE TRACEABLE TO NIST | 1 | |
| 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-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 | |
| 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 | |
| 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 | |
| NDT1039-0.016/0.016 | 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 | |
| NDT1039-0.030/0.030 | 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 | |
| NDT1039-0.032/0.050 | 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 | |
| NDT1039-0.040/0.050 | 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-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 | |
| NDT1048 | REFERENCE STANDARD (MADE OF 7075 T6 ALUMINUM MATERIAL) | 4 | |
| NDT1084-1.750-7075T6 | Boeing Reference Standard,737 PT6 51-00-00: FIG16 PG10 DETAILIII, 7075T6 Aluminum | 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 | |
| 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 | |
| NDT126 | REFERENCE STANDARD (MADE OF 7075 T6 ALUMINUM MATERIAL) | 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 | |
| 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 | |
| NDT188A | REFERENCE STANDARD (MADE OF 7075 T6 ALUMINUM MATERIAL) | 1 | |
| 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 | |
| NDT2015 | BOEING REFERENCE STANDARD 727 PT 4 54-30-27. Material: 2024-T3 Aluminum. 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| NDT3276 | BOEING REFERENCE STANDARD 737 PART 4 53-20-02 FIGURE 2 PAGE 9. MATERIAL: 2024-T3 ALUMINUM WITH RUBBER FEET ON BOTTOM FOR SUPPORT. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT3276A | BOEING REFERENCE STANDARD 737 PART 4 53-20-02 FIGURE 3 PAGE 10. MATERIAL: 2024-T3 ALUMINUM WITH RUBBER FEET ON BOTTOM FOR SUPPORT. Includes Test Report and Certificate of Conformance. . | 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| NDT528 | BOEING REFERENCE STANDARD 757 Part 4 55-10-04 Page 10 Figure 2. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT542 | BOEING REFERENCE STANDARD 757 Part 4 55-10-07 Page 11 Figure 3. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT562 | BOEING REFERENCE STANDARD 757 Part 4 57-25-01 Page 11 Figure 2. Material: Aircraft Qualtiy Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| 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 | |
| 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 | |
| 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 | |
| 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 Part 4 57-50-13 Page 7 Figure 2. Material: 7075 Aluminum. Includes Test Report and Certificate of Conformance. | 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 | |
| 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 | |
| NDT6058 | BOEING 767 REFERENCE STANDARD PART 4 53-50-01 FIGURE 2 PAGE 10. MATERIAL: 7075 ALUMINUM. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6060 | BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT6061 | BOEING REFERENCE STANDARD 767 PART 6 57-20-03 FIGURE 3 PAGE 9. MATERIAL: 7075-T6 or 2024-T3 ALUMINUM. Includes Test Report and Certificate of Conformance. | 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | |
| NDT6105 | BOEING REFERENCE STANDARD 767 PT 6 53-50-16 PAGE 5 FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. Includes Certification Report | 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 | |
| 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 | |
| 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 | |
| NDT651 | BOEING REFERENCE STANDARD 767, 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance. | 2 | |
| 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 | |
| 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 | 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 | |
| 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 | |
| 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 | |
| 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 | |
| NDT817 | BOEING REFERENCE STANDARD 787 Part 4 51-00-23 Page 5 Figure 2. Material: Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| QO-QTS-TI-03-001 | Air Force reference standard Detail#1. Material 7075-T6 Aluminum. EDM Notch size: .050" x .050" x .005" Max Width, 10 Flaws total. Includes Test Report and Certificate of Conformance. | 1 | |
| RH-4-37 | 4-37 Reference Standard, 7075-T6 Aluminum, per drawing | 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 NDTEQUIVALENT) | 1 | |
| RH120-C30-2024T3 | 12 Hole Reference Standard, 3/16" to 3/4", with .030" corner notch, 2024-T3 Aluminum | 1 | |
| RH120-C30-7075T6 | 12 Hole Reference Standard, 3/16" to 3/4", with .030" corner notch, 7075T6 Aluminum | 1 | |
| RH120-C30M20-2024T3 | 12 Hole Reference Standard, 3/16" to 3/4", with .030" corner notch and .020 midwall notch, 2024-T3 Aluminum | 1 | |
| RH120-C30M20-7075T76 | 12 Hole Reference Standard, 3/16" to 3/4", with .030" corner notch and .020 midwall notch, 7075-T76 Aluminum | 1 | |
| RH120-C30T20-7075T6 | 12 Hole Reference Standard, 3/16" to 3/4", with .030" corner notch and .020 thru notch, 7075T6 Aluminum | 1 | |
| RH121-C30-2024T3 | 12 Hole Reference Standard, 1/8" to 3/4", with .030" corner notch, 2024-T3 Aluminum | 1 | |
| RH121-C30-7075T6 | 12 Hole Reference Standard, 1/8" to 3/4", with .030" corner notch, 7075-T6 Aluminum | 1 | |
| RH121-C30C20-7075T6 | 12 Hole Reference Standard, 1/8" to 3/4", with .030" corner notch & .020" corner notch, 7075-T6 Aluminum | 1 | |
| RH121-M20-7075T6 | 12 Hole Reference Standard, 1/8" to 3/4", with .020" Mid Wall notch, 7075-T6 Aluminum | 1 | |
| RH122-T20-2024T3 | 12 Hole Reference Standard, 5/32" to 13/16", with .020" thru notch, 2024-T3 Aluminum | 1 | |
| RH122-T40-7075T6 | 12 Hole Reference Standard, 5/32" to 13/16", with .040" thru notch, 7075-T6 Aluminum | 1 | |
| RH70-T20-2024T3 | Hole Reference Standard, 7 holes, 5/32” thru 1/2” w/ .020” thru-wall notches, Aluminum | 1 | |
| RH70-T20-7075T6 | Hole Reference Standard, 7 holes, 5/32” thru 1/2” w/ .020” thru-wall notches, Aluminum | 1 | |
| RH73-C20C30-7075T6 | Multi Hole Reference Standard,.188, .250, .313, .375, .438, .500, .875", .030" Corner and .020" Corner (opposite side), 7075-T6 Aluminum | 1 | |
| RM120-C30-7075T6-1 | GENERAL PURPOSE EDDY CURRENT REFERENCE STANDARD, 7075-T6 ALUMINUM, 12 HOLES 3/16” TO ¾” DIAMETERS, EACH HOLE CONTAINS A .030” X .030” CORNER EDM NOTCH, THREE SURFACE NOTCHES - .010”, .020” & .040” DEEP X ¾” LONG | 1 | |
| RS0824-.060-2024T3 | Surface Reference Standard, .008", .020", .040" x .060" Long, 2024T3 Aluminum | 1 | |
| RS0824-.060-7075T6 | Surface Reference Standard, .008", .020", .040" x .060" Long, 7075-T Aluminum | 1 | |
| RS0824-2024T3 | EDDY CURRENT SURFACE REFERENCE STANDARD, EDM NOTCHES .008", .020", .040" (.004W +/- .002), MATERIAL: 2024-T3 ALUMINUM. SIZE: 4.0"L X 1.0"W X .25". INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| RSN-2024T3 | Navy Reference Standard, 2024T3 Aluminum | 1 | |
| RSN-2024T3-1 | Navy Reference Standard, 2024T3 Aluminum *.040" +004/-000 countersink notches, similar to Boeing 194 standard* | 1 | |
| RSN-7075T6 | Navy Reference Standard, 7075T6 Aluminum | 1 | |
| S0143 | Fokker 50/60 Reference Standard PART 6 53-30-03 PAGE 9. Material: 2024-T3 Alclad Aluminum. | 1 | |
| S46-G1A/G2A | BOEING REFERENCE STANDARD FIGURE 2. MATERIAL: 2024-T3 ALUMINUM. FASTENERS: BACR15CE6D 2 PLACES. Includes Certification Report. | 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 | |
| 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 | |
| SB11530001-5 | DOUGLAS MD-11 REFERENCE STANDARD. MD11-53-001 FIGURE 1 SHEET 1. MATERIAL: 7075-T6 ALUMINUM | 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 | |
| SRS-0824A | REFERENCE STANDARD FOR ECI, 6 ALUMINUM | 3 | |
| ST8870D | BOEING PERFORATED BONDED REFERENCE STANDARD ALUMINUM HONEYCOMB ALL PT4 78-30-01; PG.18 FIG.3 | 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 | |
| T.53.03 | SHORTS REFERENCE STANDARD Shorts SD 3-30, 53 pages 3-8. Material: 2024-T3 or 2014 AluminumIncludes Test Report and Certificate of Conformance. | 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 | |
| TRS-6-10A | THICKNESS REFERENCE STANDARD, 6 STEP ALUMINUM | 1 | |
| U8860407 | ALUMINUM (7075-T6) MULTI-HOLE REFERENCE STANDARD WITH CERTIFICATE TRACEABLE TO NIST | 1 | |
| V1 | V1 STANDARD REFERENCE STANDARD IIW 1 (TYPE V1), MADE FROM ALUMINUM | 3 | |
| V2 | V2 STANDARD REFERENCE STANDARD TYPE V2), MADE FROM ALUMINUM | 2 | |
| V2 ALUMINUM STANDARD | V2 STANDARD REFERENCE STANDARD TYPE V2), MADE FROM ALUMINUM | 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 | |
| VM89A | GENERAL PURPOSE EDDY CURRENT REFERENCE STANDARD, 7075-T6 ALUMINUM, 12 HOLES 3/16” TO ¾” DIAMETERS, EACH HOLE CONTAINS A .030” X .030” CORNER EDM NOTCH, THREE SURFACE NOTCHES - .010”, .020” & .040” DEEP X ¾” LONG | 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 |
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