| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| 98S53805002-000 | EC REFERENCE STANDAR | 6 |
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 | |
| 10RS.47 | MD-11 Eddy current reference standard Section 2-1 Page 1 Figure 1.21 | 1 | |
| 145T09065-401 | REFERENCE STANDARD FOR FASTENER HOLE INSPECTION WITH PN 145T09065-401AND EMBRAER GSE NUMBER 606. | 1 | |
| 15-5 PH | CALIBRATION REFERENCE STANDARD, 15-5 PH STAINLESS STEEL, CONTAINING 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES, (MHIRJ OR EQUIVALENT) | 1 | |
| 15−5 PH | Calibration reference standard 15−5 PH stainless steel containing 0.008 in. (0.20 mm)0.020 in. (0.51 mm) and 0.040 in. (1.02 mm) deep electrical discharge machined notches (Bombardier Inc. or equivalent) | 1 | |
| 171-00844-601 16E1 | REFERENCE STANDARD - LWR AFT ATG ANTENNA ( SPEC. ALUMINIUM 7475 T7351). | 1 | |
| 204-94034-1 | Boeing Reference Standard- Lower Lug APE-1 Primary , D204-12769-6 ASIP Inspection Program. Material: 4340 Steel. Includes Test Report and Certificate of Conformance. | 1 | |
| 2683301-1 | Cessna reference standard 55-10-02-0 (Rev 1).Model 208 Inspection of Horizontal Stabilizer Spars. | 4 | |
| 27-95031-001 | Fairchild METRO 23, Model SA227-CC, METRO 23, Model SA227-DC,Reference standard for inspection of the MLG and NLG Yoke Assembly. Material: 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance. | 2 | |
| 27F-000-212-57-10-1204 | REFERENCE STANDARD FOR DYNAMIC INSPECTION | 1 | |
| 27F-2-212-57-10-1204 | REFERENCE STANDARD FOR DYNAMIC INSPECTION | 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 | |
| 412B5MHZ35R80FE | CUSTOM 5MHz 35° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR WIT A 80mm RADIUS. USED WITH AIRBUS REFERENCE STANDARD PART NUMBER 98A54003096 Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-20 | 1 | |
| 412B5MHZ40R75FE | CUSTOM 5MHz 40° TRANSVERSE WAVE TRANSDUCER WITH END MOUNT MICRODOT CONNECTOR WIT A 75mm RADIUS. USED WITH AIRBUS REFERENCE STANDARD PART NUMBER 98A54003069 Includes Test Report and Certificate of Conformance. REFERENCE: AIRBUS A300-600 PART 4 54-50-20 | 1 | |
| 412E5MHZ60FE | CUSTOM 5MHz 60° IN FE TRANSVERSE WAVE BACKSHOOTING TRANSDUCER WITH A SIDE MOUNTED MICRODOT CONNECTOR. CASE SIZE: .690" x .354" x .354 Includes Test Report and Certificate of Conformance. REFERENCE STANDARD: 98A54003077 | 1 | |
| 7637987-9 | Eddy Current Inspection Reference standard | 1 | |
| 7947479-10 | REFERENCE STANDARD - AL 7075-T6, SPEC USAF T.O. 33-B-1-1 | 3 | |
| 7947479-10-304 | PH TOOL REFERENCE STANDARD STAINLESS SPEC USAF TO 33-B-1-1 | 1 | |
| 7947479-10-T | PH TOOL REFERENCE STANDARD TITANIUM SPEC USAF TO 33-B-1-1 | 2 | |
| 80RS10 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 80RS14 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 80RS15 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 80RS18 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 80RS19 | Ultrasonic Inspection Reference standard MD-80 | 1 | |
| 80RS21 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 80RS22 | Ultrasonic Inspection Reference standard MD-80 | 3 | |
| 80RS4 | Ultrasonic Inspection Reference standard MD-80 | 1 | |
| 80RS6 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 80RS7 | Ultrasonic Inspection Reference standard MD-80 | 1 | |
| 98A52003000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98A52003001 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98A52003002 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98A52003003 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 98A52003004 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98A53003003 | Ultrasonic Inspection reference standard A300 | 1 | |
| 98A53803016 | Ultrasonic Inspection reference standard A300 | 1 | |
| 98A53803018000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 98A53803019000 | Ultrasonic Inspection Reference standard A300 | 3 | |
| 98A53803020000 | Ultrasonic Inspection Reference standard A300 | 3 | |
| 98A54003069 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98A54003098000 | Ultrasonic Inspection Reference standard A300-600 | 1 | |
| 98A57103016 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98A57103016001 | Ultrasonic Inspection Reference standard A300-600 | 2 | |
| 98A57103020000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 98A57103023000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 98S53005021-000 | LFEC CALIBRATION REFERENCE STANDARD | 3 | |
| 98S53805002-000 | ATR REFERENCE STANDARD 53-61-18 PT 6 FIGURE 603 PAGE 609. INSPECTION OF REAR PRESSURE BULKHEAD PERIPHERY OF DOME SKIN AND CONNECTION WITH VERTICAL FLANGE OF DOME VERTICLAL CHORD. Includes Test Report traceable to NIST and Certificate of Conformance. | 6 | |
| 99A53003002000 | Ultrasonic Inspection Reference standard A310 | 1 | |
| 99A53107251000 | Ultrasonic Inspection Reference standard A310 | 2 | |
| 99A53307274000 | Ultrasonic Inspection Reference standard A318-312-320-321 | 5 | |
| 99A53803009000 | Ultrasonic Inspection Reference standard A300 | 2 | |
| 99A54403002000 | Ultrasonic Inspection Reference standard A300 | 3 | |
| 99A54403003000 | Ultrasonic Inspection Reference standard A300-600 | 2 | |
| 99A55107288000 | Ultrasonic Inspection Reference standard A300-600 | 2 | |
| 99A55107289000 | Ultrasonic Inspection Reference standard A300-600 | 2 | |
| 99A55109003000 | Ultrasonic Inspection Reference standard A300-600 | 1 | |
| 99A55109005000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A55507222000 | Ultrasonic Inspection Reference standard A300-600 | 1 | |
| 99A55507240000 | Ultrasonic Inspection Reference standard A300-600 | 1 | |
| 99A55507253000 | Ultrasonic Inspection Reference standard A300-600 | 1 | |
| 99A57004001285 | Ultrasonic Inspection Reference standard A300 | 2 | |
| 99A57004001320 | Ultrasonic Inspection Reference Standard A310 | 2 | |
| 99A57004009000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57004010000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57004012000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57103000 | Ultrasonic Inspection Reference standard A310 | 1 | |
| 99A57103001000 | Ultrasonic Inspection Reference Standard A310 | 1 | |
| 99A57103003000 | Ultrasonic Inspection Reference Standard A310 | 1 | |
| 99A57103005002 | Ultrasonic Inspection Reference standard A310 | 3 | |
| 99A57103007000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 99A57103009000 | Ultrasonic Inspection Reference standard | 2 | |
| 99A57103010000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 99A57103011000 | Ultrasonic Inspection Reference Standard A300 | 2 | |
| 99A57103012000 | Ultrasonic Inspection Reference Standard A300 | 2 | |
| 99A57103025001 | Ultrasonic Inspection Reference Standard A300 | 3 | |
| 99A57103028000 | Ultrasonic Inspection Reference Standard A300-600 | 3 | |
| 99A57103029000 | Ultrasonic Inspection Reference Standard A300 | 4 | |
| 99A57103030000 | Ultrasonic Inspection Reference standard A300 | 4 | |
| 99A57103031000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 99A57103033000 | Ultrasonic Inspection Reference Standard A310 | 2 | |
| 99A57103036000 | Ultrasonic Inspection Reference standard A310 | 2 | |
| 99A57103037000 | Ultrasonic Inspection Reference standard A310 | 1 | |
| 99A57103038000 | Ultrasonic Inspection Reference Standard A310 | 2 | |
| 99A57103041000 | Ultrasonic Inspection Reference Standard A300-600 | 3 | |
| 99A57103042000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 99A57103043000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 99A57103044000 | Ultrasonic Inspection Reference Standard A300-600 | 2 | |
| 99A57104331000 | Ultrasonic Inspection Ultrasonic Reference standard A300 | 1 | |
| 99A57104332000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A57104333000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A57104334000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A57104335000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57104336000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A57104337000 | Ultrasonic Inspection Reference standard A300 | 2 | |
| 99A57104338000 | Ultrasonic Inspection Reference standard A300 | 2 | |
| 99A57104340000 | Ultrasonic Inspection Reference standard A300 | 2 | |
| 99A57104359000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57104361000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57204360000 | Ultrasonic Inspection Reference standard A300 | 2 | |
| 99A57204375000 | Ultrasonic Inspection Reference Standard A300 | 2 | |
| 99A57204379000 | Ultrasonic Inspection Reference Standard A300 | 2 | |
| 99A57204387000 | Ultrasonic Inspection Reference standard A310 | 3 | |
| 99A57204390000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A57204390001 | Ultrasonic Inspection Reference Standard A300-600 | 1 | |
| 99A57204392000 | Ultrasonic Inspection Reference standard A300 | 1 | |
| 99A57204394000 | Ultrasonic Inspection Reference standard A310 | 4 | |
| 99A57204400000 | Ultrasonic Inspection Reference Standard A310 | 1 | |
| 99A57204401000 | Ultrasonic Inspection Reference standard A310 | 3 | |
| 99A57204402000 | Ultrasonic Inspection Reference Standard A310 | 2 | |
| 99A57204403000 | AIRBUS REFERENCE STANDARD (WING INSPECTION) | 3 | |
| 99A57204403001 | Ultrasonic Inspection Reference standard A310 | 5 | |
| 99A57204406000 | Ultrasonic Inspection Reference Standard A300 | 2 | |
| 99A57204408000 | Ultrasonic Inspection Reference Standard A300 | 2 | |
| 99A57204409000 | Ultrasonic Inspection Reference Standard A300 | 1 | |
| 99A57204410000 | Ultrasonic Inspection Reference standard | 2 | |
| 99A57204425000 | Ultrasonic Inspection Reference Standard A300-60 | 2 | |
| 99A57703000000 | Ultrasonic Inspection Reference Standard A310 | 2 | |
| 99D51107295000 | Ultrasonic Inspection Reference Standard A310 | 5 | |
| 99D51407291001 | AIRBUS CARBON LAMINATE THICKNESS REFERENCE STANDARD SET A318-A321 51-10-06-PB4 Multidirectional Fabric Material, BLOCKS 01-06 includes waterproof case. Nominal Thicknesses of 1mm, 3mm, 5mm, 9mm, 15mm, 19mm. Includes Test Report and Certificate of Con... | 7 | |
| 99D52103001000 | Ultrasonic Inspection Reference standard A318-319-320-321 | 3 | |
| 99D53103000000 | Ultrasonic Inspection Reference standard A318-319-320-321 | 5 | |
| 99D53207304000 | Ultrasonic Inspection Reference standard A318-319-320-321 | 5 | |
| 99D54403000004 | Ultrasonic Inspection Reference standard A318-319-320-321 | 7 | |
| 99D54403002000 | Ultrasonic Inspection Reference standard A318-319-320-321 | 4 | |
| 99D54403003000 | Ultrasonic Inspection Reference standard A318-319-320-321 | 4 | |
| 99D57103002000 | Ultrasonic Inspection Reference Standard A300 | 3 | |
| 99D57103002001 | Ultrasonic Inspection Reference standard A318-319-320-321 | 5 | |
| 99D57103004000 | Ultrasonic Inspection Reference Standard Ultrasonic Inspection A318-319-320-321 | 4 | |
| 99D57103005001 | Ultrasonic Inspection Reference standard A318-319-320-321 | 5 | |
| 99D57103008000 | Ultrasonic Inspection Reference Standard A318-319-320-321 | 6 | |
| 99D57103009000 | Ultrasonic Inspection Reference Standard A318-319-320-321 | 4 | |
| 99D57103010000 | Ultrasonic Inspection Reference Standard A318-319-320-321 | 5 | |
| 99D57204107000 | Ultrasonic Inspection Reference Standard A318-319-320-321 | 6 | |
| 99D57504109000 | Ultrasonic Inspection Reference Standard A318-319-320-321 | 3 | |
| 99F53303020000 | Ultrasonic Inspection Reference standard A300 | 3 | |
| 99F53303115000 | AIRBUS REFERENCE STANDARD A330 53-30-54 PAGE 6. US INSPECTION OF FUSELAGE INTERNAL STRUCTURE, SKIN PANEL JUNCTION WITH FR53.2 BULKHEAD FWD FACE BETWEEN STR39 AND STR42. 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 | |
| 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 | |
| 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 | |
| 9RS12 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 9RS13 | MD-80 REFERENCE STANDARD...FIG.9 SHEETS 1-5, MD-80 SID SECTION 2-1. Includes Test Report and Certificate of Conformance. | 1 | |
| 9RS17 | Ultrasonic Inspection Reference standard MD-80 | 2 | |
| 9RS22 | Ultrasonic Inspection Reference standard MD-80 | 1 | |
| A27288 | Eddy Current Inspection Reference standard SB DC9-27A235 R03 | 3 | |
| ACRS3-172942 | CALIBRATED CONDUCTIVVITY REFERENCE STANDARD SET OF 3. KIT CONSISTS OF MAGNESIUM, 6061-T6 AL AND 2024-T3 AL ( IACS Nominal values of 17%, 29% and 42% respectively) | 1 | |
| AF- 4120 | LOW FREQUENCY RING PROBE, 10KHZ-100KHZ, REFLECTION, .405"ID, .800"OD, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE. USED WITH REFERENCE STANDARD: NDT1102-100 TI | 1 | |
| AF-4041/4F | LOW FREQUENCY DIFFERENTIAL PROBE , 1-40KHZ. Maximum height of .50" inches and diameter of .300" to .320" inches, 4 Pin Fischer Connector. Flat at the end. Used with ANDT3016-B reference standard. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4084 | LOW FREQUENCY REFLECTION RING PROBE, 800HZ-10KHZ, .320"Ø ID,.600"Ø OD x .700"H, WITH TRIAX FISCHER CONNECTOR. REFERENCE: 767 PART 6 53-10-22, NDT6075 REFERENCE STANDARD. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4092 | LOW FREQUENCT RING PROBE, 500Hz-3KHz. REFLECTION, 1.00" OD, .510" ID, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT3255 | 1 | |
| AF-4101 | LOW FREQUENCT RING PROBE, 1-10KHz. REFLECTION, .700" OD, .350" ID, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT3255 | 1 | |
| AF-4102 | LOW FREQUENCT RING PROBE, 50Hz-5KHz. REFLECTION, .700" OD, .350" ID, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT3255 | 1 | |
| AF-4109/TI | LOW FREQUENCY REFLECTION RING PROBE, ID .470, OD.900, 3-10KHZ. For reference standard NDT 3259. Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4120 | LOW FREQUENCY RING PROBE, 10KHz-100KHz, REFLECTION, .405"ID, .800"OD, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. USED WITH REFERENCE STANDARD: NDT1102-100 Ti | 1 | |
| AF-4124/300H | REFLECTION RING PROBE TRIAX FISHER CONNECTOR, 1.25"OD .75" ID(19.6mm) 300HZ-1KHZ. 737 PART 6 57-10-53, pg.2, USED WITH REFERENCE STANDARD NDT3168 AND NDT3176-X. Includes test report and Certificate of Conformance. | 1 | |
| AF-4125/100H | CUSTOM REFLECTION RING PROBE 1.2" OD, .605" ID, 50Hz-3KHz TRIAX FISHER CONNECTOR. 737 PART 6 57-10-58, pg.2. and 737 PART 6 57-10-54, pg.2 USED WITH NDT3153-X AND 3167-X SERIES REFERENCE STANDARDS. Includes Test Report and Certificate of Conform... | 1 | |
| AF-4153/TI | LOW FREQUENCY RING PROBE 1-15KHz, REFLECTION, ID.565" OD.910",SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes Test Report and Certificate of Conformance. For Reference Standard NDT 3225. | 1 | |
| AF-4202 | LOW FREQUENCY REFLECTION RING PROBE, 500HZ-5KHZ, ID 0.325", OD 0.790" (MAX). 1.05" HEIGHT. TRIAX FISCHER CONNECTOR. USED WITH NDT6097 REFERENCE STANDARD Includes Test Report and Certificate of Conformance. | 1 | |
| AF-4334 | Low Frequency Reflection Ring Probe, 40Hz-500Hz. 1.3"Ø I.D. 2.0"Ø O.D., supplied with a Triax Fischer Connector. REFERENCE STANDARD: NDT7035. Includes test report and Certificate of Conformance. | 1 | |
| AF-4335 | LOW FREQUENCY REFLECTION RING PROBE, 300Hz-1KHz .425"Ø ID SUPPLIED WITH A TRIAX FISCHER CONNECTOR. Includes test report and Certificate of Conformance.....USED WITH 717-200 REFERENCE STANDARD P/N: 717RS10-C | 1 | |
| AF-5272 | CUSTOM COUNTERBORE ROTARY ADJUSTABLE X STYLE PROBE WITH THE COIL LOCATED AT THE EDGE OF THE PROBE TIP, .936'-1.0" 2.0"WL, SUPPLIED WITH A 4 PIN FICHER CONNECTOR, 100 KHz-2MHz Includes Test Report and Certificate of Conformance REFERENCE STANDARD - NDT3117 | 1 | |
| AF-5278/TF | HIGH FREQUENCY SURFACE PROBE, Twin Coil Differential 50-500KHZ. 4.0" Long 0.375" Diameter with Triax Fischer connector. For use with Boeing Reference Standard 497 767 Part 6 53-00-04. IncludesTest Report and Certificate of conformance. | 1 | |
| AF-6006 | SLIDING PROBE, REFLECTION, 1-40KHZ TRIAX FISHER CONNECTOR. REFERENCE STANDARD USED ( NDT1099) 757 PT. 6, 53-30-14. Includes Certification Report and COC. | 1 | |
| AFK-1017 | Custom Eddy Current Inspection Kit. Includes the following probes, Reference Standard and cables.AUR-.125SE/1.75WL-LF, AUR-.156SE/1.75WL-LF, AUR-.187SE/1.75WL-LF, AUR-.250SE/2.0WL-LF, AUR-.312SE/2.0WL-LF, AUR-.375SE/2.0WL-LF, AUR-.437SE/2.0WL-LF, AUR-... | 1 | |
| AFK-1030 | Cusom Ultrasonic Inspection Kit for Boeing 787. Kit contents include: NDT815 reference standard. Transducer part numbers: AFS-0570-1R, AFS-0570-1L, AFS-0570-2R, AFS-0570-2L, AFS-0570-3R, AFS-0570-3L, AFS-0570-4R, AFS-0570-4L, AFS-0570-5R, AFS-0570-5L | 1 | |
| AFK-SS | PH TOOL REFERENCE STANDARD STAINLESS SPEC USAF TO 33-B-1-1 | 1 | |
| AFNDT-1002 | CUSTOM 3 HOLE 7075-T6 ALUM. EC REFERENCE STANDARD WITH a .020x.020" CORNER NOTCH IN EACH HOLE. HOLE SIZES 1.063", .687", .625" DIA. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-1012 | Bombardier / Challenger 300 Custom UT Thickness Reference Standard Figure 2 Part 1 Section 4 page 11. Material: 2024-T351 Clad. Standard machine milling, no Chemical mill. Step Tolerance: +/-.002". Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-1016-6S-TI | CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6, 51-00-02 PROCEDURE 1..... Hole Sizes: .188", .250", .313", .375" .438" .500". MATERIAL: 6AL-4V Titanium. Inc... | 1 | |
| AFNDT-1080-2/840 | CUSTOM REFERENCE STANDARD PER SPECS. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2003-1AL | "EC REFERENCE STANDARD U8860405 | 1 | |
| AFNDT-2013AL | 12 HOLE REFERENCE STANDARD 7075-T6 (3/16" x 2), 13/64", 7/32", 15/64" ,(1/4" x 2 ), 17/64",9/32", 19/64",5/16", 21/64" .020"x.020" and .030"x.030" x .005"W +/-.002" CORNER EDM NOTCH PER BOEING SPECIFICATION 747 PART 6 51-00-00 PAGE 8 FIGURE 3. Includes Te | 1 | |
| AFNDT-2054AL-2 | CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. WITH HOLE DIAMETERS: .125" .156", .187", .250",.375",.500". CORNER... | 1 | |
| AFNDT-2054CS-1 | CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .156",.250",.312",.375",.437",.500". CORN... | 1 | |
| AFNDT-2054CS-2 | CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .125", .156", .187" ,.250",.375", .500". ... | 1 | |
| AFNDT-2116 | CUSTOM EC REFERENCE STANDARD BRT189-080 REV A, STEEL 15-5PH. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-2124 | CUSTOM REFERENCE STANDARD PER SPEC, 2024-T42. Includes Test Report and Certificate of Conformance. | 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-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-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-3264 | Custom Reference Standard for the Boeing Lead Screw inspection, equivalent to 7903385. Material: 4150 Alloy Steel, 1.5 Outside Diameter and 1.069" Inside Diameter with 3 EDM Flaws per BSS 7048 page 2 Table 1. Includes Test Report and Certificate of Confor | 1 | |
| AFNDT-3286 | 12 HOLE REFERENCE STANDARD 7075-T6 (Hole Sizes 3/8", 7/16", 1/2", 9/16", 5/8", 11/16", 3/4", 13/16", 7/8", 15/16", 1.0", 1-1/8",) .020"x.020" and .030"x.030" x .005"W +/-.002" CORNER EDM NOTCH PER BOEING SPECIFICATION 747 PART 6 51-00-00 PAGE 8 FIGURE 3 | 1 | |
| AFNDT-3292AL | CUSTOM 20 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .(1/8", 5/32",3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8",13/32" | 1 | |
| AFNDT-3320AL | 6 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-02 Part 6 Procedure 1 or 2. Hole Sizes: 15/32", 17/32", 9/16", 11/16", 5/8", 3/4" ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002 | 1 | |
| AFNDT-3321AL | 5 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-16 Part 6 Page 9 Figure 3. Hole Sizes: 11.5mm, 14.4mm, 14.6mm, 17.4mm and 17.5mm. Corner EDM Notches ( .020" x .020" x .005" +/- .002), ( .030" x .0 | 1 | |
| AFNDT-3329ST | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(. | 1 | |
| AFNDT-3329TI | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(. | 1 | |
| AFNDT-3347CS | EDDY CURRENT WELD SURFACE REFERENCE STANDARD. EDM NOTCHES: 0.5mm, 1.0mm, 2.0mm (.1mm (.004") WIDE ± .05mm( .002") MAX WIDTH .152mm (.006"). MATERIAL: 4340 CARBON STEEL. SIZE: 1.0"W x 4.0"L Includeds 4 piece .020" thick shim and Key Ring set. Includes Tes | 1 | |
| AFNDT-3390AL | CUSTOM 10 HOLE FLAT BOTTOM REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .218", .250", 312", .375" .437" .500",.562", .625", | 1 | |
| AFNDT-3391AL | CUSTOM 10 HOLE FLAT BOTTOM HOLE REFERENCE STANDARD ASSEMBLY PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .875", 1.00", 1.125", 1.250" 1.375", 1.500", | 1 | |
| AFNDT-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-3405AL | CUSTOM 15 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(. | 1 | |
| AFNDT-3456AL | CUSTOM 19 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00 Procedure16 Figure 3 , 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Total of 19 Hole Sizes: .128", .159", .189", .2 | 1 | |
| AFNDT-3476CS | CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION..737 PART 6 51-00-00 FIG.3 PG. 8, 757 PT 6 51-00-17 PAGE 7 FIG 3 and 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance..... Hole Sizes: .188", .250", .313", .3... | 1 | |
| AFNDT-3504TI | 12 HOLE REFERENCE STANDARD MANUFACTURED TO SPECIFICATION USAF T.O. 33-B-1-1. MATERIAL: 6AL-4V TITANIUM. HOLE SIZES: 3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8", 7/16", 1/2", 9/ 16" 5/8", 3/4" 0.020" x 0.004" +/-.001" Wide thru EDM NOTCHES. 4 tot... | 1 | |
| AFNDT1016-12S-2024 | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", . | 1 | |
| AFNDT1016-12S-7075 | CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .6 | 1 | |
| AFS-1175 | 70°. ANGLE BEAM TRANSDUCER in ALUMINUM, SIDE MOUNT MICRODOT CONNECTOR, .187" x .187" ELEMENT. CASE SIZE: .67'L x .26"W x .33"H. Includes Test Report and Certificate of Conformance. Reference: B767 Part 4 53-50-05. Standard Part number NDT679 | 1 | |
| AFS-1175T | 70°. ANGLE BEAM TRANSDUCER in ALUMINUM, .187" x .187" ELEMENT, TOP MOUNTED MICRODOT CONNECTOR. CASE SIZE: .67'L x .26"W x .33"H. Includes Test Report and Certificate of Conformance. Reference: B767 Part 4 53-50-05. Standard Part number NDT679 | 1 | |
| AFS-1346 | CUSTOM 2 ELEMENT RING TRANSDUCER FOR BORE HOLE INSPECTION WITH BOEING REFERENCE STANDARD 55-10-13 PAGE 9 FIGURE 2. TWO MICRODOT CONNECTORS "A" and "B" | 1 | |
| AFS-5826 | Custpm 5MHz 31° shear wave transducer .375" element. 2.0"(51mm) radius. Case Size: ..75"L x .50"W x .25"H end mounted microdot connector. Used with reference standard NDT3196. | 1 | |
| AFS-5827 | Custpm 5MHz 33° shear wave transducer .375" element. 2.0"(51mm) radius. Case Size: ..75"L x .50"W x .25"H end mounted microdot connector. Used with reference standard NDT3197. | 1 | |
| AFS-5828 | Custpm 5MHz 26° shear wave transducer .375" element. 2.0"(51mm) radius. Case Size: ..75"L x .50"W x .25"H end mounted microdot connector. Used with reference standard NDT3197. | 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 | CALIBRATION REFERENCE STANDARD (CRS), BLOCK, ALUMINUM ALLOY, WITH CONDUCTIVITY BETWEEN 35% AND 45% IACS (20.3 MS/M TO 26.1 MS/M), THAT CONTAINS 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED NOTCHES, ( | 8 | |
| AN670-55-31-102 | CALIBRATION REFERENCE STANDARD (CRS), MADE OF ALUMINUM WITH MULTIPLE LAYERS CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| AN670-55-31-110 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| ANDT3004 | LFEC REFERENCE STANDARD | 3 | |
| ANDT3019 | MFEC REFERENCE STANDARD | 3 | |
| APB-NDT001 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-02 Page 6 Frigure 2. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes | 1 | |
| APB-NDT003 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-02 Page 9-10 Figure 5. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Include | 1 | |
| APB-NDT004 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-01 Page 5-6 Figure 2. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Include | 1 | |
| APB-NDT005 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-02 Page 13-14. Figure 7. Material: 7150-T6 (34-39.5% IACS), 7050-T7 (40-44% IACS), and 2324-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Inclu | 1 | |
| APB-NDT006 | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-53 Page 5-6 Figure 2. Material: 7075-T7 (40-44% IACS), 2324-T3 (29.5-33.5% IACS), and 2224-T3 (29.5-33.5% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Inclu | 2 | |
| APB-NDT011A | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 8-9 Figure 3. Material: 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT011B | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 11-12 Figure 5. Material: 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT011C | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 14-15 Figure 7. Material: 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT011D | AVIATION PARTNERS BOEING REFERENCE STANDARD 767 Part 6 57-20-08 Page 17-18 Figure 9. Material: 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT015 | BOEING AVIATION PARTNERS REFERENCE STANDARD 767 Part 6 57-20-09 Page 21-22 Figure 10. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Ce | 1 | |
| APB-NDT016 | BOEING AVIATION PARTNERS REFERENCE STANDARD 767 Part 6 57-50-09 Page 24-25. Figure 12 Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Ce | 1 | |
| APB-NDT3301 | AVIATION PARTNERS BOEING REFERENCE STANDARD 737 Part 6 57-20-34 Page 7-8 Figure 2. Material: 2024-T3 (28.5-32% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT5203 | AVIATION PARTNERS REFERENCE STANDARD 737 Part 6 57-20-02 Page 7-8 Figure 2. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate | 2 | |
| APB-NDT5204 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-02 Page 11-12 Figure 4. Material: 2224-T3 and 2324-T3 or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 2 | |
| APB-NDT5205 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-02 Page 15-16 Figure 6. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Cer | 2 | |
| APB-NDT5206 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-03 Page 8-9 Figure 2. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certi | 2 | |
| APB-NDT5207 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-03 Page 12-13 Figure 4. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Cer | 2 | |
| APB-NDT5208 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-03 Page 16-17 Figure 6. Material: 2224-T3 (29.5-33.5% IACS) and 2324-T3 (29.5-33.5% IACS), or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Cer | 2 | |
| APB-NDT5301 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-01 Page 15-16 Figure 6. Material: 7050-T7 (40-44% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT5302 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-01 Page 11-12 Figure 4. Material: 7050-T7 (40-44% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| APB-NDT5303 | AVIATION PARTNERS BOEING REFERENCE STANDARD 757 Part 6 57-20-01 Page 7-8 Figure 2. Material: 7050-T7 (40-44% IACS) or Airplane Quality Material with an Electrical Conductivity Between ±5%. Includes Test Report and Certificate of Conformance. | 1 | |
| ARP-.385/.720 | LOW FREQUENCY REFLECTION RING PROBE, 500Hz-5KHz.385"Ø ID .720"Ø OD, SUPPLIED WITH A TRIAX FISCHER CONNECTOR. FOR REFERENCE STANDARD APB-3302. Includes Test Report and Certificate of Conformance. | 1 | |
| ARP-.75-1.25/300Hz | REFLECTION RING PROBE, 1.25"OD .75" ID(19.6mm) TRIAX FISHER CONNECTOR 300HZ-1KHZ. REFERENCE STANDARD NDT3176-X 737 PT 6 57-10-59, 737 PART 6 57-10-53 NDT3168. Includes Test Report and Certificate of Conformance. | 1 | |
| ARP-.85/1.40-200Hz | LOW FREQUENCY REFLECTION RING PROBE .85" I.D. 1.40" O.D. TRIAX CONNECTOR 100Hz-500Hz. REFERENCE STANDARD NDT3176-X 737 PT 6 57-10-59. Includes test report and Certificate of Conformance. | 1 | |
| ARP-1.2/100H-7 | LOW FREQUENCY REFLECTION RING PROBE 1.2" OD, .605" ID, 50Hz-3KHz TRIAX FISHER CONNECTOR. 737 PART 6 57-10-58, pg.2. and 737 PART 6 57-10-54, pg.2 USED WITH NDT3153-X AND 3167-X SERIES REFERENCE STANDARDS. Includes Test Report and Certificate of ... | 1 | |
| ARP-1.25-.75-300H | REFLECTION RING PROBE TRIAX FISHER CONNECTOR, 1.25"OD .75" ID(19.6mm) 300HZ-1KHZ. 737 PART 6 57-10-53, pg.2, USED WITH REFERENCE STANDARD NDT3168 AND NDT3176-X. Includes test report and Certificate of Conformance... | 1 | |
| ARP-1.40/.85-200Hz | LOW FREQUENCY REFLECTION RING PROBE .85" I.D. 1.40" O.D. TRIAX FISCHER CONNECTOR 100Hz-500Hz. REFERENCE STANDARD NDT3176-X 737 PT 6 57-10-59. Includes test report and Certificate of Conformance. | 1 | |
| 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 | |
| C12-DEL-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance... | 3 | |
| C12-PCS-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED HOLE and SPLICE CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance... | 3 | |
| C12-POT-3C1N | REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED CORE and CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance... | 3 | |
| 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 ST.01 | 4340 Mil-Spec. 5000 Steel Multi-purpose Reference Standard | 1 | |
| DAC GSET Ti.01-N1-N2 | General Surface Titanium HFET Reference Standard MD-11 section 2-1 page 1 figure 1.2 | 1 | |
| DC3-1 | DC-3 REFERENCE STANDARD ..SECTION 3 PAGE 2 FIGURE 1.1 | 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 | |
| EX601R51093 | Calibration reference standard (CRS) multiple layers fastened assembly containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EX604-60024 | CALIBRATION REFERENCE STANDARD MULTI-LAYERED ALUMINUM ALLOY FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 2 | |
| EX604−60024 | 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 | |
| EXBC670-59066−001 | CALIBRATION REFERENCE STANDARD CONTAINS 0.250 IN (6.35 MM) LONG0.005 IN. (0.127 MM) WIDE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59089-001 | CALIBRATION REFERENCE STANDARD SIMILAR IN MATERIAL AS THE INSPECTION AREA CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ) | 1 | |
| EXBC670-59089−001 | CALIBRATION REFERENCE STANDARD SIMILAR IN MATERIAL AS THE INSPECTION AREA CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59133 | CALIBRATION REFERENCE STANDARD MADE FROM ALUMINUM ALLOY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59141 | CALIBRATION REFERENCE STANDARD MULTI LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59142 | CALIBRATION REFERENCE STANDARD MADE FROM ALUMINUM ALLOY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59143-001 | CALIBRATION REFERENCE STANDARD, ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES. (MHIRJ) | 1 | |
| EXBC670-59145 | CALIBRATION REFERENCE STANDARD ALUMINUM ALLOY MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59148 | CALIBRATION REFERENCE STANDARD (CRS) MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES. (BOMBARDIER INC.) | 1 | |
| EXBC670-59156 | CALIBRATION REFERENCE STANDARD MADE FROM MULTIPLE ALUMINUM ALLOY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59157-003 | CALIBRATION REFERENCE STANDARD, MULTIPLE LAYERED FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (MHIRJ) | 1 | |
| EXBC670-59159 | CALIBRATION REFERENCE STANDARD(CRS), MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM)NOTCHES (MHIRJ). | 1 | |
| EXBC670-59160 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERED FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| EXBC670-59161 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59162 | CALIBRATION REFERENCE STANDARD, ALUMINUM ALLOY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCH. (MHIRJ OR EQUIVALENT) | 1 | |
| EXBC670-59163 | CALIBRATION REFERENCE STANDARD TITANIUM ALLOY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCH. (BOMBARDIER INC.EQUIVALENT) | 1 | |
| EXBC670-59164 | CALIBRATION REFERENCE STANDARD MULTIPLE LAYERS ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59174 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59176 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59177 | CALIBRATION REFERENCE STANDARD ALUMINUM MULTIPLE LAYER FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59178 | CALIBRATION REFERENCE STANDARD, MULTIPLE LAYER FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (MHIRJ) | 1 | |
| EXBC670-59179 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ). | 1 | |
| EXBC670-59180 | CALIBRATION REFERENCE STANDARD ALUMINUM ALLOY MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXBC670-59181 | CALIBRATION REFERENCE STANDARD ALUMINUM MULTIPLE LAYER FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES. (BOMBARDIER INC.) | 1 | |
| EXBC670-59182 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ). | 1 | |
| EXBC670-59183-001 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) TRANSDUCER - ANGLE BEAM, 5.0 MHZ, 0.375 IN. (9.53 MM) H X | 1 | |
| EXBC670-59185 | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERS FASTENED ASSEMBLY CONTAINING ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ) | 1 | |
| EXBC670−59044 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined (EDM) notches. (Bombardier Inc.) | 1 | |
| EXBC670−59045 | Calibration reference standard assembly aluminum alloy contains 0.250 in. (6.35 mm) long electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59046 | Calibration reference standard assembly aluminum alloy contains 0.250 in. (6.35 mm) long electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59065 | Calibration reference standard assembly aluminum and steel alloy contains 0.250 in. (6.35 mm) long electrical discharge machined notches (Bombardier inc.) | 1 | |
| EXBC670−59066−001 | Calibration reference standard contains 0.250 in (6.35 mm) long0.005 in. (0.127 mm) wide electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59068 | Calibration reference standard multiple layered assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59089−001 | Calibration reference standard similar in material as the inspection area containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59094 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59098 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59099 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59101 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59125 | Calibration reference standard assembly contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59133 | Calibration reference standard made from aluminum alloy containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59134 | Calibration reference standard aluminum alloy that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59139−001 | Calibration reference standard made from aluminum alloy that contains electrical discharge machined notches (Bombardier inc.) | 1 | |
| EXBC670−59141 | Calibration reference standard multi layers fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59142 | Calibration Reference Standard made from aluminum alloy containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59143 | Calibration Reference Standard assembly that contains electrical discharge machined notches. (Bombardier Inc.) | 1 | |
| EXBC670−59145 | Calibration reference standard aluminum alloy multiple layers fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59148 | Calibration Reference Standard (CRS) multiple layers fastened assembly that contains electrical discharge machined (EDM) notches. (Bombardier Inc.) | 1 | |
| EXBC670−59153 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59154 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59156 | Calibration Reference Standard made from multiple aluminum alloy containing electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59157 | Calibration reference standard multiple layered fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59158 | Calibration Reference Standard (CRS) multiple layers fastened assembly containing electrical discharge machined (EDM) notches (Bombardier Inc.). | 1 | |
| EXBC670−59159 | Calibration Reference Standard (CRS) multiple layers fastened assembly containing electrical discharge machined (EDM) notches (Bombardier Inc.). | 1 | |
| EXBC670−59161 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59162 | Calibration Reference Standard aluminum alloy that contains electrical discharge machined notch. (Bombardier Inc. or equivalent) | 1 | |
| EXBC670−59163 | Calibration Reference Standard titanium alloy that contains electrical discharge machined notch. (Bombardier Inc. or equivalent) | 1 | |
| EXBC670−59164 | Calibration Reference Standard multiple layers assembly that contains electrical discharge machined (EDM) notches (Bombardier Inc.) | 1 | |
| EXBC670−59174 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59176 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59177 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59178 | Calibration reference standard multiple layer fastened assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59180 | Calibration reference standard aluminum alloy multiple layers fastened assembly containing electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXBC670−59181 | Calibration reference standard aluminum multiple layer fastened assembly containing electrical discharge machined (EDM) notches. (Bombardier Inc.) | 1 | |
| EXSH670-31001-1 | CALIBRATION REFERENCE STANDARD, STGR15R BUTT JOINT, CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ) | 1 | |
| EXSH670-31001−1 | CALIBRATION REFERENCE STANDARD STGR15R BUTT JOINT CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-31002-1 | CALIBRATION REFERENCE STANDARD STGR1L AND STGR20L BUTT JOINTS CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-31011−1 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH670-35910-1 | CALIBRATION REFERENCE STANDARD, ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES | 1 | |
| EXSH670-35910−1 | CALIBRATION REFERENCE STANDARD ASSEMBLY THAT CONTAINS ELECTRICAL DISCHARGE MACHINED NOTCHES | 1 | |
| EXSH670−31001−1 | Calibration reference standard STGR15R butt joint contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31002−1 | Calibration reference standard STGR1L and STGR20L butt joints contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31011−1 | Calibration reference standard assembly that contains electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH670−31014−1 | Calibration reference standard pressure bulkhead machined frames FS693.00 and FS847.00 contains subsurface electrical discharge machined notches. (Bombardier Inc.) | 1 | |
| EXSH670−35910−1 | Calibration Reference Standard assembly that contains electrical discharge machined notches | 1 | |
| EXSH690-31003−11 | CALIBRATION REFERENCE STANDARD EMERGENCY EXIT DOOR SURROUND STRUCTURE CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH690-31023-1 | CALIBRATION REFERENCE STANDARD, CIRCUMFERENTIAL SKIN JOINT STGR7 TEST PIECE, CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (MHIRJ) | 1 | |
| EXSH690-31023−1 | CALIBRATION REFERENCE STANDARD CIRCUMFERENTIAL SKIN JOINT STGR7 TEST PIECE CONTAINS SURFACE AND SUBSURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES (BOMBARDIER INC.) | 1 | |
| EXSH690−31003−11 | Calibration reference standard emergency exit door surround structure contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| EXSH690−31023−1 | Calibration reference standard circumferential skin joint STGR7 test piece contains surface and subsurface electrical discharge machined notches (Bombardier Inc.) | 1 | |
| F12-DEL-3C1N | REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance. | 1 | |
| KC10-7025-3 ASSEMBLY | CUSTOM MANUFACTURED BOEING REFERENCE STANDARD FOR ULTRASONIC INSPECTION 101/201 | 1 | |
| KC10-7027 | BOEING REFERENCE STANDARD KC10 FUEL COMPENSATOR CUTOUT-INSPECTION.( 301 GUIDE AND 302 GUIDE ARE PART OF INSPECTION AND SOLD SEPARATELY) | 1 | |
| KC10RS-7007 | KC10 Reference Standard, NDI Inspection | 1 | |
| KC10RS-7008 | KC10 Reference Standard, NDI Inspection | 1 | |
| KC10RS-7009 | KC10 Reference Standard, NDI Inspection | 1 | |
| KC10RS-7010 | KC10 Reference Standard, NDI Inspection | 1 | |
| KC10RS-7011 | KC10 Reference Standard, NDI Inspection | 1 | |
| KC10RS-7012 | KC10 Reference Standard, NDI Inspection | 1 | |
| MD11-04-210 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K225) FIGURE 1.29, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance. | 1 | |
| MD11-04-325 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 FIGURE 1.30, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance. | 1 | |
| MD11-04-400 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K225) FIGURE 1.31, PG.1 SECTION 2-1. 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 | |
| MD11-09 | MD11 REFERENCE STANDARD MDC-K5225 SECTION 2-1 FIG 1.22. 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 | |
| MD11-11 | McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 FIGURE 1.27 SHEETS 1-6, PG.1-6 SECTION 2-1 | 1 | |
| MD90-01 | MD-90 REFERENCE STANDARD, SECTION 2-1 FIG 1.1 FASTENER (HL19PB-6-4 +NAS1252-10L + NAS679A3) Includes Test Report and Certificate of Conformance. | 1 | |
| MHS-10-1A-1 | EC Reference Standart | 1 | |
| MHS-12-1A-0 | "EC REFERENCE STANDARD U8860405 | 1 | |
| NDETECH-7048 | STEEL MUTLI HOLE REFERENCE STANDARD>>> THE NOTCH SPECIFICATION IS 0.030'' X 0.030'' (45° ) CORNER NOTCH | 1 | |
| NDT1016 3.2-5.5MM | Special Boeing Type Reference Standard, PT6 51-00-00 PG 10, Fig 16 Detail III | 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-T1/T2 | BOEING REFERENCE STANDARD NDT1039-T1/T2 X 1SET OF 5 PIECES | 2 | |
| NDT3267-T1/T2 | BOEING REFERENCE STANDARD NDT3267-T1/T2 X 1SET OF 4 PIECES | 1 | |
| NDT3316 | REFERENCE STANDARD FOR INSPECTION USE ON B737 AS PER B737 NDTM PART 4 53-10-16 | 2 | |
| NDT4153 | BOEING 747 REFERENCE STANDARD PART 4 57-30-08 PAGE 6 FIGURE 2. PROCEDURE FOR INSPECTING CRACKED RIVET PART NUMBER BACR15FH10DD17 | 1 | |
| NDT4243 | BOEING REFERENCE STANDARD 747 Part 6 57-10-31 Page 4 Figure 1. Material: 2024-T3 or An Airplane Quality with an Electrical Conductivity of 28-43% IACS. Fasteners: Non-Magetic Fastener. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT5089 | REFERENCE STANDARD FOR UT INSPECTION | 1 | |
| NDT518 | Ultrasonic Inspection Reference standard 757 | 1 | |
| NDT520 | Eddy Current Inspection Reference standard 757 | 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 | |
| NDT6048 | BOEING REFERENCE STANDARD 767 Part 4 27-40-02 horizontal stab inspection. Includes Test Report and Certificate of Conformance. | 1 | |
| NDT6052 | BOEING REFERENCE STANDARD 767 P4, 57-50-27. UT INSPECTION OF MAIN LANDING GEAR FORWARD TRUNNION SUPPORT SIDE LOAD FITTING | 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 | |
| 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 | |
| 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 | |
| NEC-6252 | boeing ec reference standard w/cert | 1 | |
| RD11-01A | MD-11 REFERENCE STANDARD MDC-K5225 SECTION 2-1 PAGES 1-2, FIG 1.3 SHEETS 1&2. Includes Test Report and Certificate of Conformance. | 1 | |
| RD11-02 | MD REFERENCE STANDARD MDC-K5225 SECTION 2-1 FIG 1.6 | 1 | |
| RD11-03 | MD11 REFERENCE STANDARD MDC-K5225 SECTION 2-1 | 1 | |
| RH12-T40-7075T6 | CALIBRATION REFERENCE STANDARD (CRS), ALUMINUM ALLOY, CONDUCTIVITY VALUE OF 35% TO 45% IACS THAT CONTAINS VARIOUS HOLE SIZES WITH 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (TECHNA NDT OR EQUIVALENT) | 1 | |
| RM120-C30-2024T3-1 | "EC REFERENCE STANDARD U8860405 | 1 | |
| RM17-C23-2024T3 | Special Boeing Type Reference Standard, per PT6 51-00-00 Fig 16, | 1 | |
| RM200-T40-T6AL4V | CALIBRATION REFERENCE STANDARD, TITANIUM ALLOY, CONDUCTIVITY 1.1 % IACS, CONTAINS 0.010 IN. (0.25 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP SURFACE ELECTRICAL DISCHARGE MACHINED NOTCHES, AND VARIOUS SIZE HOLES WITH 0.040-IN (1.02 MM) EDM NOTC | 1 | |
| RSAF-304 | PH TOOL REFERENCE STANDARD STAINLESS SPEC USAF TO 33-B-1-1 | 1 | |
| RSAF-T6AL4V | PH TOOL REFERENCE STANDARD TITANIUM SPEC USAF TO 33-B-1-1 | 1 | |
| SB09270209-5 | Eddy Current Inspection Reference standard SB DC9-27-209 R07 | 1 | |
| SB09530016-5 | Eddy Current Inspection Reference standard SB MD-A27-320 R01 | 2 | |
| SB09530186-9 | Eddy Current Inspection Reference standard SB DC9-53-186 R06 | 1 | |
| SB09570184-7 | Ultrasonic Inspection Reference standard | 1 | |
| SK601R-30008A | CALIBRATION REFERENCE STANDARD (CRS), MULTIPLE LAYERED FASTENED ASSEMBLY, EQUIVALENT IN MATERIAL AND THICKNESS AS THE INSPECTION AREA CONTAINING SUBSURFACE ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ). | 6 | |
| SRS-0824A | REFERENCE STANDARD FOR ECI, 6 ALUMINUM | 3 | |
| SRS-0824M | REFERENCE STANDARD FOR SURFACE INSPECTION | 1 | |
| SRS-0824S | REFERENCE STANDARD FOR SURFACE INSPECTION | 3 | |
| SRS-0824SS | REFERENCE STANDARD FOR SURFACE INSPECTION | 1 | |
| SRS-0824T | REFERENCE STANDARD FOR SURFACE INSPECTION | 3 | |
| SRSM-2510A | ec reference standard w/certs | 1 | |
| ST4130 | CALIBRATION REFERENCE STANDARD, CARBON STEEL 4130 ALLOY, CONTAINING 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED (EDM) NOTCHES (MHIRJ OR COMMERCIALLY AVAILABLE). | 1 | |
| ST4340 | CALIBRATION REFERENCE STANDARD BLOCK - MADE FROM 4340 STEEL, MIL-S-5000, CONTAINS 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED NOTCHES, (MHIRJ OR COMMERCIALLY AVAILABLE). | 5 | |
| ST8870-1 | BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 20 FIGURE 7. GR/EP SKIN/NOMEX CORE DISBOND DEFECT | 4 | |
| ST8870-4 | BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 19 FIGURE 6. GR/EP SKIN/NOMEX CORE DISBOND DEFECT | 4 | |
| 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 | |
| TEK-5154 | CUSTOM 2 ELEMENT RING TRANSDUCER FOR BORE HOLE INSPECTION WITH BOEING REFERENCE STANDARD 55-10-13 PAGE 9 FIGURE 2. TWO MICRODOT CONNECTORS "A" AND "B" | 1 | |
| TEK-9087L | 5 MHZ SURFACEWAVE TRANSDUCER, REFERENCE STANDARD NDT3310, LEFT SOUND DIRECTION | 1 | |
| TEK-9087R | 5 MHZ SURFACEWAVE TRANSDUCER, REFERENCE STANDARD NDT3310, RIGHT SOUND DIRECTION | 1 | |
| TEK810 | TECNAM REFERENCE STANDARD | 1 | |
| TEK812 | REFERENCE STANDARD TECNAM | 1 | |
| TEK814-A | TECNAM REFERENCE STANDARD | 1 | |
| TEK814-B | TECNAM REFERENCE STANDARD | 1 | |
| TI-6AL-6V-2SN | CALIBRATION REFERENCE STANDARD, NO.TI-6AL-6V-2SN, MADE FROM TITANIUM ALLOY (1.1% IACS), CONTAINS 0.008 IN. (0.20 MM), 0.020 IN. (0.51 MM), AND 0.040 IN. (1.02 MM) DEEP ELECTRICAL DISCHARGE MACHINED NOTCHES, (BOMBARDIER INC. OR EQUIVALENT) | 3 | |
| 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 | |
| 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.
