| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 99A57204394000 | UT REFERENCE STANDAR | 4 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 1/N-02-384 | Nomad Series N22 & N24 Reference Standard. for the inspection of Wing Strut Upper Fittings, Figure 27 Page 51. Includes Test Report and Certificate of Conformance. | 1 | |
| 301 GUIDE | BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION | 1 | |
| 302 GUIDE | BOEING REFERENCE STANDARD GUIDE PLATE KC10 FUEL COMPENSATOR CUTOUT-INSPECTION | 1 | |
| 55-36-01 | UT CALIBRATION REFERENCE STANDARD , STEP WEDGE, 7000 SERIES ALUMINUM, GENERIC AS PER ATR 72 NTM 55-36-01 | 1 | |
| 70700-25603-101 | UT REFERENCE STANDARD | 1 | |
| 98S53305004-000 | UT BOND TESTER REFERENCE STANDARD | 5 | |
| 98S53305005-000 | UT BOND TESTER REFERENCE STANDARD | 5 | |
| 98S53505006-000 | UT CALIBRATION REFERENCE STANDARD | 4 | |
| 98S54305002-200 | UT CALIBRATION REFERENCE STANDARD | 5 | |
| 98S57105004-200 | UT CALIBRATION REFERENCE STANDARD | 4 | |
| 98S57105006-200 | UT CALIBRATION REFERENCE STANDARD | 3 | |
| 98S57105015-200 | UT CALIBRATION REFERENCE STANDARD | 3 | |
| 98S57205030.004 | UT CALIBRATION REFERENCE STANDARD , STEP WEDGE, 7000 SERIES ALUMINUM, GENERIC | 5 | |
| 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 | |
| 99D57504102000 | AIRBUS REFERENCE STANDARD OUTBOARD LUG A318/A319/A320/A321 PART 4: 57-52-50 FIGURE 403 PAGE 404 Material: 2024-T351. Includes Test Report and Certificate of Conformance. | 4 | |
| 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 | |
| 99F53303105000 | AIRBUS A330 REFERENCE STANDARD. 53-30-30-991-003-A , PAGE 6. FUSELAGE LONGITUDINAL BUTT JOINT ATSTR 30, FROM 38 TO FR 40, LH/RH. Includes Test Report and Certificate of Conformance. | 1 | |
| 99F57204173000 | AIRBUS A330 REFERENCE STANDARD 57-20-46-270-801-A-01 PAGE 12. OUTER WING REAR SPAR UPPER & LOWER FLANGES BETWEEN RIB7 and RIB12 LH/RH. MATERIAL: 7010 ALUMINUM. Includes Test Report and Certificate of Conformance. | 3 | |
| 99F57204174000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57204175000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57204176000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | 2 | |
| 99F57204177000 | AIRBUS REFERENCE STANDARD A330 57-20-46-991-005-A PAGE 13. US INSPECTION OF OUTER WING REAR SPAR FWD FACE BETWEEN RIB 7 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES Includes Test Report and Certificate of Conformance. | 2 | |
| 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 | |
| ACWM-E175-OB | Outer Wheel Standard, Embraer..175 90000582-1. Contains a Total of 3 EDM Flaws in the Bead Seat Area of the Reference Standard. Flaw sizes: 1.52mm Long x 0.76mm Deep x 0.10mm Wide Tolerance= +/- 0.05mm. Includes Test Report and Certificate of Conform... | 1 | |
| AFNDT-1012 | Bombardier / Challenger 300 Custom UT Thickness Reference Standard Figure 2 Part 1 Section 4 page 11. Material: 2024-T351 Clad. Standard machine milling, no Chemical mill. Step Tolerance: +/-.002". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3264 | Custom Reference Standard for the Boeing Lead Screw inspection, equivalent to 7903385. Material: 4150 Alloy Steel, 1.5 Outside Diameter and 1.069" Inside Diameter with 3 EDM Flaws per BSS 7048 page 2 Table 1. Includes Test Report and Certificate of Confor | 1 | |
| AFNDT-VL769-1A | TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(.800"THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES) | 1 | |
| AFNDT-VL769-2A | TITANIUM VERTICAL(INBOARD LUG) ULTRASONIC REFERENCE STANDARD(1.500" THICK, 3.56" OUTSIDE RADIUS WITH A 1.312" BORE DIAMETER. COPPER BERYLLIUM NON FLANGED BUSHING WITH A 1.128 BORE DIA. ( 2 EACH .100" x .100" CORNER NOTCHES) | 1 | |
| AGE-05546-401 | REFERENCE STANDARD FOR BAGGAGE DOOR CUTOUT, NDI | 2 | |
| BA CRS EXBC670-59046 | REFERENCE STANDARD UT | 1 | |
| BACRS EX605-60037-001 | REFERENCE STANDARD UT | 1 | |
| BACRS EXBC670-59046 | REFERENCE STANDARD UT | 1 | |
| BASE PLATES 717RS2 1/4 | BOEING UT REFERENCES STANDARD | 1 | |
| BASE PLATES 717RS2 1/8 | BOEING UT REFERENCES STANDARD | 1 | |
| EC-PHT-MHS-12-1CS-O | STEEL MUTLI HOLE REFERENCE STANDARD>>> THE NOTCH SPECIFICATION IS 0.030'' X 0.030'' (45° ) CORNER NOTCH | 1 | |
| EO13829.001/1 | Aeronautical Engineers Australia Reference Standard Fig.2 Page 5 DOC NO: MMS13829.001/1 and REF EO: EO13829.001/1 | 1 | |
| EX605-60037-001 | REFERENCE STANDARD UT | 1 | |
| EXBC670-59040-005 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 3.000 IN. (76.20 MM)OUTSIDE DIAMETER 1.563 IN. (39.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−001 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 4.224 IN. (107.29 MM)OUTSIDE DIAMETER 2.311 IN. (58.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−003 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 3.374 IN. (85.70 MM)OUTSIDE DIAMETER 2.311 IN. (58.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−007 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.000 IN. (50.80 MM)OUTSIDE DIAMETER 1.032 IN. (26.21 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−009 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.000 IN. (50.80 MM)OUTSIDE DIAMETER 1.332 IN. (33.83 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−011 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.500 IN. (63.50 MM)OUTSIDE DIAMETER 1.563 IN. (39.70 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59040−013 | CALIBRATION REFERENCE STANDARD ASSEMBLY 6AI-6V−2SN TITANIUM ALLOY 2.500 IN. (63.50 MM)OUTSIDE DIAMETER 1.332 IN. (33.83 MM) INSIDE DIAMETER (BOMBARDIER INC.) | 1 | |
| EXBC670-59046 | REFERENCE STANDARD UT | 1 | |
| EXBC670−59040−001 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 4.224 in. (107.29 mm)outside diameter 2.311 in. (58.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−003 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 3.374 in. (85.70 mm)outside diameter 2.311 in. (58.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−005 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 3.000 in. (76.20 mm)outside diameter 1.563 in. (39.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−007 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.000 in. (50.80 mm)outside diameter 1.032 in. (26.21 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−009 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.000 in. (50.80 mm)outside diameter 1.332 in. (33.83 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−011 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.500 in. (63.50 mm)outside diameter 1.563 in. (39.70 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXBC670−59040−013 | Calibration reference standard assembly 6AI−6V−2Sn titanium alloy 2.500 in. (63.50 mm)outside diameter 1.332 in. (33.83 mm) inside diameter (Bombardier Inc.) | 1 | |
| EXSH670-31001-1 | CALIBRATION REFERENCE STANDARD, STGR15R BUTT JOINT, CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ) | 1 | |
| EXSH670-31001−1 | CALIBRATION REFERENCE STANDARD STGR15R BUTT JOINT CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-31002-1 | CALIBRATION REFERENCE STANDARD STGR1L AND STGR20L BUTT JOINTS CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670−31001−1 | Calibration reference standard STGR15R butt joint contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31002−1 | Calibration reference standard STGR1L and STGR20L butt joints contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| F15-AL-UT-0.175-2 | F15 REFERENCE STANDARD. MATERIAL: 2024-T3, OUTBOARD TORQUE BOX REAR SPAR, 68A115101, LOWER FLANGE FASTENER HOLES. Includes Test Report and Certificate of Conformance. | 1 | |
| GENERAL BLOCK 29A032 | TITANIUM REFERENCE STANDARD 3 EDM CUT DEPTH 0.2 MM, 0.5 MM AND 1MM WITH WIDTH 0.05 MM – 0.25 MM | 1 | |
| GENERAL BLOCK 29A49 | STEEL REFERENCE STANDARD 3 EDM CUT DEPTH 0.2 MM, 0.5 MM AND 1MM WITH WIDTH 0.05 MM – 0.25 MM | 1 | |
| KC10-7027 | BOEING REFERENCE STANDARD KC10 FUEL COMPENSATOR CUTOUT-INSPECTION.( 301 GUIDE AND 302 GUIDE ARE PART OF INSPECTION AND SOLD SEPARATELY) | 1 | |
| NDETECH-7048 | STEEL MUTLI HOLE REFERENCE STANDARD>>> THE NOTCH SPECIFICATION IS 0.030'' X 0.030'' (45° ) CORNER NOTCH | 1 | |
| NDT3050 | BOEING REFERENCE STANDARD PT 6 53-30-20 FIG 2. Includes Test Report and Certificate of Conformance. (SCREW AND NUT) | 4 | |
| NDT3286 | UT REFERENCE STANDARD | 2 | |
| NDT3287 | UT REFERENCE STANDARD | 2 | |
| NDT3288 | UT REFERENCE STANDARD | 2 | |
| NDT5089 | REFERENCE STANDARD FOR UT INSPECTION | 1 | |
| NDT6025-1 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6025-2 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6025-3 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6025-4 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6025-5 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6025-6 | BOEING REFERENCE STANDARD 767 PART 4 57-50-17 FIGURE 2 PAGE 6. MATERIAL MUST BE MANUFACTURE OUT OF 7075-T6 PLATE WITH GRAIN DIRECTION. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT6052 | BOEING REFERENCE STANDARD 767 P4, 57-50-27. UT INSPECTION OF MAIN LANDING GEAR FORWARD TRUNNION SUPPORT SIDE LOAD FITTING | 1 | |
| NDT676 | BOEING REFERENCE STANDARD FOR PW4000 and JT9D-7R4D/E STRUTS FIGURE 2 Part 4 54-50-07 page 9 Figure 2. Material: 2024-T3. Includes Test Report and Certificate of Conformance. | 2 | |
| NDT709 | Boeing 777 Reference Standard, UT, Part 4, 57-60-01 | 1 | |
| NDT776 | Boeing Reference Standard 777 PT4 54-51-03 PG 7 FG 2 *make part out of 2024-T3, heat treat to 2024-T8 | 2 | |
| 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 | |
| STANDARD-B | 2/64" FLAT BOTTOM HOLE EQUIVALENT SURFACE NOTCH STANDARD (*ABOVE DESCRIPTION MUST BE ENGRAVED ON THE REFERENCE STANDARD) ..DRAWING "B" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR) MATERIAL=7075-T6 | 1 | |
| TEK-1538-UTRS | UT Reference standard, 4130 Steel | 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 | |
| ZNDT-2003-1S | STEEL MUTLI HOLE REFERENCE STANDARD>>> THE NOTCH SPECIFICATION IS 0.030'' X 0.030'' (45° ) CORNER NOTCH | 1 |
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.
