| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| AGE-00862-401 | STAND WING | 4 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| (CALIB) 954-2399 | STANDARD COMPASS FOR COMPASS SWING CALIBRATION (CALIBRATION) | 1 | |
| 012568 | C-130 WING AND HORIZONTAL STAB “TRIPOD” STYLE SUPPORT STANDS | 1 | |
| 03-5808-0000 | Stand, Tail Casa/Wing Atp | 2 | |
| 03-5814-0000 | Stand, Wing Dornier 328 | 1 | |
| 03-5818-5000 | Stand, Wing J-41 | 1 | |
| 03-5839C0000 | Stand, Wing Stand Lear 45 (Ce) | 1 | |
| 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 | |
| 1409-00-2 | KIT REFERENCE STANDARD NDI- TORQUE BOX. NDI WING ASSY. | 11 | |
| 145-44130-401 | KIT REFERENCE STANDARD NDI- TORQUE BOX. NDI WING ASSY. | 3 | |
| 17P9M2007 | Douglas Reference Standard Assembly For the Ultrasonic Calibration of Upper Wing Skin to common Stringer, Figure24-4 sheets 253. Material: 7075 Aluminum. Includes Test Report Traceable to NIST and Certificate of Conformance. | 1 | |
| 2-531-01 | TAIL STAND WING JACK | 1 | |
| 2000DD10980-1 | Aluminum CAL Standard, United Airlines Drawing No. 2000DD10980 REV D | 1 | |
| 2000DD10980-3 | Steel CAL Standard, United Airlines Drawing No. 2000DD10980 REV D | 1 | |
| 2000DD10980-5 | Titanium CAL Standard, United Airlines Drawing No. 2000DD10980 REV D | 1 | |
| 2001100 | model 2187 5-23' working height wing maintenance stand. 5-17' platform height, 750 lb. weight capacity, 4' x 4' platform with 10' x 10' railing for protected working area. Overhang: In the lowest position 5', from the edge of the safety fence to the fron | 1 | |
| 2017837 | NB & WB Adjustable Fuel Stand. Provides a working height range of 112" to 209". Sturdy structural steel construction is powder coated for durability. Full bumpers on platform railings protect underwing of aircraft. High quality hydraulic lift allows easy | 1 | |
| 208 FRONT SPAR | CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 FRONT SPAR LOWER CAP. Drawing NO. 2683201 | 1 | |
| 208 REAR SPAR | CESSNA / TEXTRON AVIATION EDDY CURRENT REFERENCE STANDARD 208 REAR SPAR LOWER CAP. Drawing NO. 2683202 | 1 | |
| 262A | Boeing Standard, 727 PART6 53-10-27, Drawing No. Fig 11 Sheet 7 | 1 | |
| 2870020-001 | EDDY CURRENT STANDARD, WINGLET | 2 | |
| 3108AS600-1 | REMOVAL/INSTALLATION STAND - WING PYLON FAIRING | 1 | |
| 330 OWINGS-LTLR-FX | A330 OUTER WING STAND | 1 | |
| 330IWINGS-FX-LH | A330 INNER WING STAND, FIXED HEIGHT LH AND RH | 1 | |
| 330IWINGS-LTLR-FX | A330 INNER WING STAND | 1 | |
| 330MOWING LTLR-FX | MEDIUM OUTER WING STAND | 1 | |
| 330MOWINGS-LTLR-FX | A330 Outer wing stand L, fixed height, sloped floor LH and RH | 1 | |
| 330OWINGSLTRH-FX | A330 OUTER WING STAND R, FIXED HEIGHT, SLOPED FLOOR LH AND RH | 1 | |
| 330iwings-fx-LH | A330 Inner wing stand, fixed height LH and RH | 1 | |
| 330owingsLTRH-fx | A330 Outer wing stand R, fixed height, sloped floor LH and RH | 1 | |
| 45-128 | Custom 8 Hole Calibration Standard Test Coupon Assembly Figure 5 Page 10 to include the following Pieces. Figure 2 Page 7. Material .071" 2024-T3 Clad Aluminum, 7 EDM Flaws total. Figure 3 Page 8 .250" 4130or4340 Steel 0 EDM Flaws total and Figure 4... | 2 | |
| 48J20090 | WING STAND BIG | 1 | |
| 500.05.72.003 | WING STAND | 1 | |
| 57-12-501 | RIGHT AND LEFT WING REAR BEAM AT BL 35.8 — EDDY CURRENT INSPECTION CALIBRATION STANDARD, 1159W40007-1NDT (GULFSTREAM) | 1 | |
| 57-12-502 | RIGHT AND LEFT WING REAR BEAM AT RBS 103.3 — EDDY CURRENT INSPECTION PROBE :SPO 5053 PROBE :SPO 5054 CALIBRATION STANDARD, 1159W40005-1NDT (GULFSTREAM | 1 | |
| 57-12-504 | RIGHT AND LEFT WING REAR BEAM AT RBS 230.1 — EDDY CURRENT INSPECTION CALIBRATION STANDARD, 1159W40063-1NDT (GULFSTREAM | 1 | |
| 65B01461-1 | WING LANDING GEAR STAND | 1 | |
| 65B01461-9 | WING LANDING GEAR STAND | 1 | |
| 6B34 | STANDARD COMPASS FOR COMPASS SWING | 1 | |
| 71658-18-53/2&3 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39 | 1 | |
| 71658-7-35/1&4 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 651 FIG.603 SHEET 39 | 1 | |
| 717RS10-C | 717-200 REFERENCE STANDARD FOR THE LOWER CENTER WING SKIN PANELS AT STRINGER 16 &18. PAGES 1-11. MATERIAL: 2024-T3, 7075-T6 &7075-T7 ALUMINUM. Includes Test Report and Certificate of Conformance. | 1 | |
| 954-2399 | STANDARD COMPASS FOR COMPASS SWING | 5 | |
| 98A09001000000 | BAR-TOWING SUPSD BY STANDARD TOWBAR | 1 | |
| 98A57103017000 | Airbus Standard, A300-600 FIG4 see drawing provided | 1 | |
| 98D10203500000 | MOORING KIT-NLG (BASIC STANDARD TOWING BRACKET) | 7 | |
| 98D10203500004 | MOORING KIT - NLG (BASIC STANDARD TOWING B) | 8 | |
| 98S07003000001 | JACK PADS WING AND TAIL STAND (3) | 16 | |
| 98S53005021-000 | ATR72 Calibration Standard Drawing PT6 53-51-01 PG 608, Figure 601 | 3 | |
| 98S57105015 | Calibration Standard Drawing 57-14-03, Figure 401 | 1 | |
| 98S57105032-200 | ATR72 Calibration Standard Drawing PT4 57-12-12 PG 404, Figure 401 | 3 | |
| 98S57105032-202 | ATR72 Calibration Standard Drawing PT4 57-12-12 PG 405, Figure 402 | 3 | |
| 98S57105033-200 | ATR42 CALIBRATION STANDARD DRAWING PT4 57-12-11 PG 404, FIGURE 401 | 1 | |
| 98S57205030-004 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 5 | |
| 98S57205030.001 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 4 | |
| 98S57205030.004 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 5 | |
| 98S57205030000 | WING UPPER PANEL CALIBRATION STANDARD | 3 | |
| 98S57205030001 | CALIBRATION STANDARD, ATR72, DRAWING REF: 22S57213396 | 4 | |
| 98S57205030003 | CALIBRATION STANDARD, ATR72, DRAWING REF: 22S5721 | 2 | |
| 98S57205030004 | CALIBRATION STANDARD, ATR72, DRAWING REF: 22S57213396 | 5 | |
| 99A57204403000 | AIRBUS REFERENCE STANDARD (WING INSPECTION) | 3 | |
| 99A57204403001 | AIRBUS REFERENCE STANDARD (WING INSPECTION) | 5 | |
| 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 | |
| AFK-1014 | Custom Ultrasonic Kit, PART 4 53-10-13 for the WING REAR SPAR - STA 663.75 REAR SPAR BULKHEAD SIDE FRAME FITTING FAIL SAFE STRAP. Kit includes 1 of each AFM-560AT & AFS-0541 Transducers, 1 NDT3312 Reference Standard and 1 ABNC-MD6. Supplied with a waterpr | 1 | |
| AFK-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-ECS6 | EDDY CURRENT SURFACE PROBE KIT. Includes the Following Cable, Surface standards and probes: ACN16-TF6-B, AFNDT-2030/4340, AFNDT-2030/7075-T6, ATPN-45-5, ATPN-45-5FX, ATPN-5, ATPN-5FX, ATPN-95-5, ATPN-95-5, PELICAN STYLE WATERPROOF kIT BOX. Supplied wit... | 1 | |
| AFNDT-3019S | CUSTOM AIR FORCE EDDY CURRENT BOLT HOLE STANDARD PER CUSTOMER SUPPLIED DRAWING, 1/4" 8630 STEEL PLATE (4130 EQUIVALENT ALTERNATIVE). EDM: 0.030 x 0.030 CORNER NOTCH. HOLE DIAMETER= 0.437Ø. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3025AL | Eddy Current Surface Standard 7075-T6 Aluminum. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W x... | 1 | |
| AFNDT-3025CS | Eddy Current Surface Standard 4340 Carbon Steel. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W ... | 1 | |
| AFNDT-3025INC | Eddy Current Surface Standard 718 Inconel. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W x (25m... | 1 | |
| AFNDT-3025SS | Eddy Current Surface Standard 304 Stainless Steel. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)... | 1 | |
| AFNDT-3025TI | Eddy Current Surface Standard 6AL-4V Titanium. Block Size: 4.0"(101.6mm)L x 1.0"(25.4mm)W x .25"(6.35mm)H. Includes 3 EDM Flaws of the following sizes...1.) (0.5mm)D x (0.25mm)W x (25mm)L..2.) (1.0mm)D x (0.25mm)W x (25mm)L..3.) (2.0mm)D x (0.25mm)W x ... | 1 | |
| AFNDT-3059 | Custom Eddy Current 2 Hole Calibration Standard per Customer Supplied Drawing. Material: 7050-T7451. Hole Sizes: .516"Ø and .812"Ø with a total of 4 EDM Notches 0.021" x 0.021" x .004" Wide Max. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3060 | Custom Eddy Current 2 Hole Calibration Standard per Customer Supplied Drawing. Material: 7050-T7451. Hole Sizes: .252"Ø and .516"Ø with a total of 4 EDM Notches 0.021" x 0.021" x .004" Wide Max. Includes Test Report and Certificate of Conformance. | 1 | |
| AFNDT-3071 | Custom designed eddy current multi-layer aircraft aluminum skin test specimen, drawing 2, sheets 1-4. reference standard for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3072 | Custom designed eddy current aircraft calibration standard, Drawing 3, Sheets 1-3, for Central Piedmont Community College. Material: 2024-T3 Aluminum. Includes Certification Report Traceable to NIST. | 1 | |
| AFNDT-3290AL | Custom ST Aerospace Engineering Multi-Hole Standard 2 Plate Assembly, Manufactured to the Customer Supplied Drawing Specifications . Material: 7075-T6 Aluminum. 6 Total Hole Sizes to be determined. Includes Test Report and Certificate of Conformance. | 1 | |
| AGE-00862-401 | STAND - STABILIZING, WING | 4 | |
| AGE-01410 -401 | STAND,STABILIZING,WING | 8 | |
| AGE-01410-401 | STAND,STABILIZING,WING | 8 | |
| AGE00862-401 | STAND - STABILIZING, WING | 4 | |
| ALB1160/1 | Add. stand A319 ins.wing dock | 1 | |
| AMS2630C Custom | Custom Reference Standard Per SAE AMS2630C. material: Titanium Alloy, Ti6Al4V per AMS-4928R Annealed. Includes 2 EDM Flaws per customer supplied Drawing. Includes Test Report Traceable to NIST and Certificate of Conformance. | 1 | |
| AT518DWS | TWO LUG — DOUBLE WING STANDAR | 1 | |
| B26942102-101 | CENTER WING INTERNAL STAND COMPLETE | 1 | |
| BAT3518-A | Nutplate Jig - Double Wing - Standard Spacing - #6 Screw - MADE IN THE USA! | 1 | |
| BAT3518-B | Nutplate Jig - Double Wing - Standard Spacing - #8 Screw - MADE IN THE USA! | 1 | |
| BAT3518-C | Nutplate Jig - Double Wing - Standard Spacing - #10 Screw - MADE IN THE USA! | 1 | |
| BAT3518-D | Nutplate Jig - Double Wing - Standard Spacing - 1/4" Screw - MADE IN THE USA! | 1 | |
| BAT3518-G | Nutplate Jig - Single Wing - Standard Spacing - #6 Screw | 1 | |
| BAT3518-H | Nutplate Jig - Single Wing - Standard Spacing - #8 Screw | 1 | |
| BAT3518-J | Nutplate Jig - Single Wing - Standard Spacing - #10 Screw | 1 | |
| BAT3518-K | Nutplate Jig - Single Wing - Standard Spacing - 1/4" Screw | 1 | |
| C-130-WR | C-130 Outer Wing Rainbow Fitting Bolt Hole Standard C-130, 2 Layers, 3 HOLES, 3/4", 7/8" and 1.0" with .004" X .030" X .030" EDM Notches in each hole. Includes Test Report and Certificate of Conformance. | 1 | |
| C500-300 | WING COVERS (Standard model) (set of 2) | 1 | |
| CA12-1508A | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T7 ALUMINUM, 54-10-11 PAGE 634A FIG.603 SHEET 21B | 1 | |
| CA12-1683A | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 STEEL, 54-10-11 PAGE 632C FIG.603 SHEET 20C | 1 | |
| CE2-40 | KEY-STANDBY COMPASS,SWING COMPUTER | 24 | |
| D02016-002 | WING HYDRAULIC LIFT D02016-002 + 16A CEE, STANDARD 30 M: RAL 6018 YELLOW-GREEN, HYDRO | 1 | |
| D08504K3D1E01B0 | HYDRO Standard A330 /A340-200/-300 Wing Tripod Jack | 2 | |
| D08505K3D1E01B0 | HYDRO Standard B787 Wing Tripod Jack | 2 | |
| DC-10 FIG603/15C | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628B FIG.603 SHEET 15C | 1 | |
| DC-10 FIG603/15E/4340 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628D FIG.603 SHEET 15E | 1 | |
| DC-10 FIG603/15E/Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628D FIG.603 SHEET 15E | 1 | |
| DC-10 FIG603/15G | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628F FIG.603 SHEET 15G | 1 | |
| DC-10 FIG603/23 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 635 FIG.603 SHEET 23 | 1 | |
| DC-10 FIG603/24-Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 636C FIG.603 SHEET 24 | 1 | |
| DC-10 FIG603/24-Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 636C FIG.603 SHEET 24 | 1 | |
| DC-10 FIG603/25 | DOUGLAS DC-10 WING CLEVIS REFERENCE STANDARD 6AL-6V or 6AL-4 TITANIUM, 54-10-11 PAGE 637 FIG.603 SHEET 25 | 1 | |
| DC-10 FIG603/27Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 639 FIG.603 SHEET 27 | 1 | |
| DC-10 FIG603/27Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 639 FIG.603 SHEET 27 | 1 | |
| DC-10 FIG603/28LOWER/Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER) | 1 | |
| DC-10 FIG603/28LOWERTi | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER) | 1 | |
| DC-10 FIG603/28UPPER/Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER) | 1 | |
| DC-10 FIG603/28UPPER/Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER) | 1 | |
| DC-10 FIG603/29Al | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 641 FIG.603 SHEET 29 | 1 | |
| DC-10 FIG603/29Ti | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 641 FIG.603 SHEET 29 | 1 | |
| DC-10 FIG603/30-AL | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 642 FIG.603 SHEET 30 | 1 | |
| DC-10 FIG603/39-1 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #1 | 1 | |
| DC-10 FIG603/39-2 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #2 | 1 | |
| DC-10 FIG603/39-3 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #3 | 1 | |
| DC-10 FIG603/39-4 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #4 | 1 | |
| DC-10 FIG603/43 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 655 FIG.603 SHEET 43 | 1 | |
| DC-10 FIG603/5 | DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 617 FIG.603 SHEET 5 | 1 | |
| DHC-29444 | Q400 Reference Standard, De Havilland Drawing No DHC29444-01 | 1 | |
| DHC-29444-001 | Q400 Reference Standard, De Havilland Drawing No DHC29444-001 | 1 | |
| FEN351 | STANDARD TRIPOD-JACK SET A320 FAMILY INCL. NEO - WING | 1 | |
| FEN351A21 | HYDRO Standard A320 Family Wing Tripod Jack | 2 | |
| FEN352A21 | HYDRO Standard B737 Wing Tripod Jack | 2 | |
| FME65B0076 | BUILDUP STAND - WING AND BODY MAIN LANDING GEAR | 1 | |
| FME65B00761 | Buld-up stand wing & body main landing gear | 1 | |
| FME65B01201-1 | BUILDUP STAND - WING AND BODY MAIN LANDING GEAR | 1 | |
| GSE278 | STAND,STABILIZING,WING | 1 | |
| IV9635GL | BORESCOPE,FLEXIBLE: VIEWING DIAMETER: 6 MM; DISTANCE: 3/5 M; POWER: 10X; FIELD VIEW: 160 DEG MAX; STANDARD/SPECIFICATION: MIL STD 810G, MIL STD 461G, IP 65; ADDITIONAL DATA: ITEM ADDITIONAL DESCRIPTION: IPLEX G LITE, ULTRAPORTABLE INDUSTRIAL VIDEOSCOPE IP | 1 | |
| J15051G | WING SUPPORT STAND | 1 | |
| J25016-1 | TEST STAND - LATCH ACTUATOR, OFF-WING ESCAPE SLIDE COMPARTMENT DOOR | 3 | |
| L17-200 | WING COVERS, standard wingtip, WINTER USE (set of 2) | 1 | |
| L17-205 | WING COVERS, standard wingtip, ALL YEAR USE (set of 2) | 1 | |
| L90-210 | WING COVERS (STANDARD MODELS), WINTER USE (set of 2) | 1 | |
| L90-215 | WING COVERS (STANDARD MODELS), ALL YEAR USE (set of 2) | 1 | |
| MAU-220 | WING COVERS (standard tip), WINTER USE (set of 2) | 1 | |
| MAU-225 | WING COVERS (standard tip), ALL YEAR USE (set of 2) | 1 | |
| MPI-WS15-2 | WING ACCESS STAND 1)WATER PROOF LIGHTING 2) ELECTRICLA CONNETORS PER STAND 3)PNUEMATIC CONNETION | 1 | |
| MR-5304509 | WING LEADING EDGE PANEL STAND | 1 | |
| NDT 5203 | Wing Front Spar Standard ID # R0059591 | 1 | |
| NDT 5204 | wing front Spar Standard ID# R0059592 | 1 | |
| NDT 5205 | wing Front Spar Standard ID# R0059593 | 1 | |
| NDT 5206 | Wing rear Spar Standard ID# R0061094 | 1 | |
| NDT 5207 | wing Rear Spar Standard ID# R0061095 | 1 | |
| NDT 5208 | Wing Rear Spar Standard ID# R61096 | 1 | |
| NDT1088-036X2/050-B | Boeing Reference Standard, Bare, Drawing Provided | 1 | |
| NDT1088-036X2/050-C | Boeing Reference Standard, Drawing Provided | 1 | |
| NDT1088-250/250 | Boeing Standard, Drawing Provided, Figure 2 | 1 | |
| NDT1099G-P1 | BEOING REFERENCE STANDARD 757 Part 4 53-30-04 Page 15-17 Figure 3. Material: Delrin. *** SEE FINALIZED DRAWING*** | 1 | |
| NDT251 | Boeing Standard, 727 PT6 57-30-27:PG30 FIG3 SHEET6, engrave per drawing | 1 | |
| NDT262 | Boeing Standard, 727 PART6 53-10-27, Drawing No. Fig 11 Sheet 8 | 1 | |
| NDT263 | Boeing Standard, 727 PART6 53-10-27, Drawing No. Fig6, Page 29 | 1 | |
| NDT3038P1 | Reference Standard, 737 PART4 57-50-02 **SEE NEW DRAWING** (DM) | 3 | |
| 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 | |
| NDT650 | Boeing Standard, 767 PART6 57-04-01, Drawing No. FIG 2 | 2 | |
| NDT688 | Boeing Standard, 767 PT4 57-50-03:PG8 FIG2 **** USE NEW DRAWING**** | 3 | |
| Olympus Phased Array Weld Inspection Kit | Olympus Phased Array Weld Inspection Kit - he kit contains the following items:, qty 2 A12 5L64 PA probes with 5m cable., qty 2 SA12 N55S Standard Wedge with Removable IHC Ring, qty 1 ‘Y’ Splitter 64/64, for Omniscan MX2, 5m split conduit, Irrigation Tubi | 1 | |
| PA24-200 | WING COVERS (standard wingtips), WINTER USE (set of 2) | 1 | |
| PA24-205 | WING COVERS (standard wingtips), ALL YEAR USE (set of 2) | 1 | |
| PA24-240 | WING COVERS (standard wingtips), hail protection type, WINTER USE (set of 2) | 1 | |
| PA24-245 | WING COVERS (standard wingtips), hail protection type, ALL YEAR USE (set of 2) | 1 | |
| PDL 1034 | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26, engrave per drawing Standard | 1 | |
| PDL 1034/1040 | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26, engrave per drawing Standard + Guide | 1 | |
| PDL 1034J | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26, engrave per drawing Standard | 1 | |
| PDL 1034J/1040J | Calibration Standard, C130 SMP 515-C-NDI 20-40-00:FIG18 PG26 & PG27, engrave per drawing, Standard + Guide | 2 | |
| R-1807 | JACKSTAND PAD, WING | 7 | |
| R1807 | JACKSTAND PAD, WING | 7 | |
| R1808 | PAD WING JACKSTAND | 7 | |
| RH-4-37 | 4-37 Reference Standard, 7075-T6 Aluminum, per drawing | 1 | |
| S41-E1A | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1A NDI REF STD PER DRAWING SK667-00011. | 1 | |
| S41-E1C | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-E1C NDI REF STD PER DRAWING SK667-00012. | 1 | |
| S41-F1B | BOEING CUSTOM REFERENCE STANDARD MCU ESM S41-F1B NDI REF STD PER DRAWING SK667-00010. | 1 | |
| 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 | |
| SLS-123456-SS304 | BOEING REFERENCE STANDARD PER DRAWING STD-1. MATERIAL: 304 STAINLESS STEEL. CHEMICAL CONVERSION COATING PER MIL-DTL-5541, CLASS 1A. Includes Certification Traceable to NIST and Material Certs. | 1 | |
| SO111-7 | Custom FOKKER F28 Horizontal Stab. Drive Junction Fitting Eddy Current Standard per drawing # 28. 0-3210/2610-Material: 7075-T6. Includes Test Report and Certificate of Conformance. | 1 | |
| SRS-0824S-4340 | EC Reference. Wing to fuselage lateral attachement. Use to calibrate standard SRS-0824S to calibrate the instrument. | 1 | |
| ST8744 | Standard tool leak tracking inb'd wing assy | 2 | |
| STANDARD-B | 2/64" FLAT BOTTOM HOLE EQUIVALENT SURFACE NOTCH STANDARD (*ABOVE DESCRIPTION MUST BE ENGRAVED ON THE REFERENCE STANDARD) ..DRAWING "B" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR) MATERIAL=7075-T6 | 1 | |
| STD-1--AL | Custom Radius Channel Standard Material: 7075-T651 ALUMINUM. Standard to include a total of 62 EDM flaws identified as A, B,C, D, E, and F in the drawing. Includes test report traceable to NIST standards which comply with MIL-Q-9858A, Mil-4-45208A. | 1 | |
| STD-1-TI | Custom Radius Channel Standard Material: 6AL-4V Titanium. Standard to include a total of 62 EDM flaws identified as A, B,C, D, E, and F in the drawing. Includes test report traceable to NIST standards which comply with MIL-Q-9858A, Mil-4-45208A. | 1 | |
| T34-210 | WING COVERS (STANDARD MODELS), WINTER USE (set of 2) | 1 | |
| T34-215 | WING COVERS (STANDARD MODELS), ALL YEAR USE (set of 2) | 1 |
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