| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 38-3131-02 | TEST PROCEDURE | 1 | |
| 7919970 | TEST PROCEDURE | 1 | |
| 7923395 | TEST PROCEDURE | 1 | |
| 7925143 | TEST PROCEDURE | 1 | |
| 7953927 | TEST PROCEDURE | 1 | |
| 7962515 | TEST PROCEDURE | 1 | |
| DZZ7540 | TEST PROCEDURE | 1 | |
| DZZ7601 | TEST PROCEDURE | 1 | |
| TR0580-10TP | TEST PROCEDURE | 1 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 004-50337-05XX | ACCEPTANCE TEST PROCEDURE SETUP DISK | 1 | |
| 185 | BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 & 777-200/300 51-00-04 PROCEDURE 1 PAGE 8. Includes Test Report and Certificate of Conformance. | 2 | |
| 189 | BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4 PG.13 & 737 PT 6 51-00-00 PROCEDURE 23 PG.11 FIG.7. Includes Test Report and Certificate of Conformance. | 7 | |
| 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 | |
| 36-3131-01 | AUTOMATIC TEST TAPE AND TEST PROCEDURE | 1 | |
| 36-3131-03 | AUTOMATIC TEST PROCEDURE | 1 | |
| 36-3131-04 | TEST PROCEDURES | 1 | |
| 36-3131-11 | AUTOMATIC TEST PROCEDURES | 1 | |
| 36-3214-02 | AUTOMATIC TEST PROCEDURE | 1 | |
| 8011486-508 | SUPPORT FOR DISASEMBLY AND ASSEMBLY (TEST PROCEDURES) | 1 | |
| 998-2232-506 | ACCEPTANCE TEST PROCEDURE | 1 | |
| 998-2551-508 | ACCEPTANCE TEST PROCEDURE SETUP DISK | 1 | |
| 998-2687-504 | ACCEPTANCE TEST PROCEDURE SETUP DISK | 1 | |
| 99A51107300000 | AIRBUS A330 REFERENCE STANDARD FOR SUBSURFACE CRACKS IN AL-ALLOY 51-10-16-991-011-A. PART 6, PAGE 615 FIGURE 610PROCEDURE B. Includes Test Report and Certificate of Conformance... | 5 | |
| 99A53403003001 | AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance. | 3 | |
| 99A53803004001 | AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance. | 1 | |
| 99D57204188000 | AIRBUS A320 CALIBRATION STANDARD FIGURE 2 PROCEDURE D. A320 FWD SPAR LOWER FLANGE RIB 22-27. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-5257G | PROBE GUIDE Material: Lucite. Diameter 1.50" ±0.02 . Used in Boeing procedure 55-10-27 Part 6. Includes Test Report and Certificate of Conformance | 1 | |
| AF-MBB403-7-1 | CUSTOM STAINLESS STEEL EDDY CURRENT ROTARY PROBE INCLUDING COLLAR, FREQUENCY 100KHz-2MHz WITH 4 PIN FISCHER CONNECTOR. REFERENCE: AIRBUS A300-600 FIGURE 603 PART 6 53-19-27 PAGE 604 PROCEDURE A. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2008/SS | AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 & 32-42-05 FIGURE 11 PROCEDURE 1 PAGE 15. MATERIAL: 304 STAINLESS STEEL. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3187AL | METRIC 10 STEP CALIBRATION BLOCK, 0.6mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm ± .05mm. Pad Size: 20mm X 20mm. Per Airbus Procedure A 51-10-04. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3187TI | METRIC 10 STEP CALIBRATION BLOCK, 0.6mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm ± .05mm. Pad Size: 20mm X 20mm. Material: 6AL-4V Titanium. Per Airbus Procedure A 51-10-04. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3507 | Custom 2 hole BOEING REFERENCE STANDARD MANUFACTURED PER 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. ....HOLE SIZES: 0.344" (11/32''),0.562"... | 1 | |
| AFNDT-3669-1043 | BOEING COUNTERSINK REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER 100° COUNTERSINK HOLE. MATERIAL: 43404340M STEEL. SIZE: 2.0" X .375" THICK( ROUNDSQUARE. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 1 | |
| ANDT1079 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. Includes Test Report and Certificate of Conformance. FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, BACR15BB7AD-4, BACR15BB8AD-4, ALL ALODINE) | 4 | |
| ANDT1080 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. Includes Test Report and Certificate of Conformance. FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, BACR15BB7AD-4, BACR15BB8AD-4, ALL ALODINE) | 2 | |
| ANDT1081 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENER (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | 2 | |
| ANDT1082 | BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENERS: (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance. | 3 | |
| 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/ 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 | |
| DZZ7411 | TEST PROCEDURE | 1 | |
| DZZ7553 | INSP TEST PROCEDURE | 1 | |
| F27404000 | SUPPORT-ASSY DISASSY AND TEST PROCEDURE | 1 | |
| FA02242TL5 | SUPPORT FOR TEST PROCEDURES | 1 | |
| GSB3411011 | BARFIELD PITOT–STATIC TEST SET (PROCEDURE TWO) | 3 | |
| Model #2019 | Hydraulic Test Stand (Hydraulic and leak testing procedures 10 GPM minimum) | 1 | |
| NDT 1017 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 2 | |
| NDT1016 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1017 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1018 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1019 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | 3 | |
| NDT1020 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1021 | BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1041 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.250” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1042 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.313” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1043 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1043CS | BOEING COUNTERSINK REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER 100° COUNTERSINK HOLE. MATERIAL: 43404340M STEEL. SIZE: 2.0" X .375" THICK( ROUNDSQUARE. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. | 1 | |
| NDT1044 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.438” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1045 | BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.500” DIAMETER. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT1083-.157 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-.5625 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-.630 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.5620 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.563 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.625 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.630 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.688 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.695 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.750 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 2 | |
| NDT1083-0.787 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.812 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.813 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.875 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-0.938 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-1.000 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-1.286 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT1083-1.347 | BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert | 1 | |
| NDT297 | BOEING REFERENCE STANDARD 727 PART 4 32-30-27 PROCEDURE 5 PAGE 10 FIGURE 1. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT298 | BOEING REFERENCE STANDARD 727 PART 4 32-30-27 PROCEDURE 5 PAGE 11 FIGURE 1. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT298PL | BOEING TRANSDUCER POSITIONER 727 PART 4 32-30-27 PROCEDURE 5 PAGE 9 FIGURE 1. Includes Test Certificate of Conformance. | 1 | |
| NDT298PR | BOEING TRANSDUCER POSITIONER 727 PART 4 32-30-27 PROCEDURE 5 PAGE 8 FIGURE 1. Includes Test Certificate of Conformance. | 1 | |
| PDL 1036 | C-130 TRUSS MOUNT UPPER LUG INSPECTION TRANSDUCER, 5MHz., "A" & "B" SMP 515-C INSPECTION PROCEDURE FOR WINGS CHAPTER 57. Includes Test Report and Certificate of Conformance. | 2 |
Aviapool (Aviation Tool Pooling LLC) is a global company providing around the clock assistance for the planning, supply, and sourcing of tooling equipment to the commercial aviation marketplace.
We are making available to our customers a comprehensive one-stop solution in ensuring the right tooling equipment reaches you on time for your planned input needs. With a fully researched tooling database of over 600,000 items, across multiple aircraft types available to you, we are in a perfectly placed position to get you what you need on time and on budget.
We take your tooling requests, and source the items on your behalf. Just submit your items, and we do the rest.
