AIRCRAFT SEAT RELATED Parts 1680-00-216-9520 through 1680-00-228-2485 |
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We solve sourcing challenges for parts like 1680-00-216-9520, 1680-00-216-9521, 1680-00-217-7395, 1680-00-218-0889, 1680-00-220-2806, 1680-00-220-2808, 1680-00-220-2809, 1680-00-222-2546, 1680-00-223-5770, 1680-00-223-9869 -- hard to find, long lead time, and obsolete part requirements.
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| Part number | Description | Category | Details |
1680-00-216-9520 | SUPPORT, ADJUSTMENT, SEAT | III END ITEM IDENTIFICATION | ACFT MODEL C-5A |
1680-00-216-9521 | LEG ASSEMBLY, SEAT | III END ITEM IDENTIFICATION | ACFT MODEL C-5A |
1680-00-217-7395 | PLUG, AIRCRAFT SEAT | | |
1680-00-218-0889 | CABLE AND CONDUIT ASSEMBLY EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 29.500 IN. LG,CLEVIS AT ONE END,ROD AT OTHER END,TEFLON LINED |
1680-00-220-2806 | SEAT, AIRCRAFT | OVERALL WIDTH | 25.000 INCHES NOMINAL |
1680-00-220-2808 | SEAT, AIRCRAFT | OVERALL WIDTH | 30.370 INCHES NOMINAL |
1680-00-220-2809 | SEAT, AIRCRAFT | OVERALL WIDTH | 24.370 INCHES NOMINAL |
1680-00-222-2546 | SEAT, CONICAL, VARIAB | | |
1680-00-223-5770 | SURVIVAL KIT CONTAINER, AIRCRAFT SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O 2 TIE DOWN STRAP ASSY,LATCH FIXED LH,LATCH FIXED RH,2 LUG,2 SPRING TORSION,2 STANDOFF,3 BRACKET,2 PLATE,2 HINGE,CONTAINER ASSY SEAL,GUIDE HINGE LH,GUIDE HINGE RH,10 NUT HEX METAL CAP,6 SCREW BUTTON HEAD HEX SOCKET,18 WASHER,8 SCREW,2 BOLT,RETAINING COMPOUND,36 RIVET |
1680-00-223-9869 | CUSHION ASSY, SEAT | | |
1680-00-225-0429 | COVER, JUMP SEAT TRI | | |
1680-00-225-0446 | CUSHION ASSEMBLY, SEAT | III END ITEM IDENTIFICATION | U/O NUMBER 1050-530010-11,TRIM INSTALLATION-T39 AIRCRAFT |
1680-00-225-0598 | TUBE ASSY, SEAT, FRON | | |
1680-00-225-0665 | TUBE ASSY, SEAT, FRON | | |
1680-00-225-0669 | SEAT BOTTOM AND BAC | | |
1680-00-225-0675 | SUPPORT, SEAT TUBE, A | | |
1680-00-225-0676 | SUPPORT, SEAT TUBE, A | | |
1680-00-225-0677 | FRAME SECTION, SEAT, AIRCRAFT | III FSC APPLICATION DATA | ACFT ACCESSORIES AND COMPONENTS |
1680-00-225-0958 | CAM, CLAMP, SEAT TUBE | III END ITEM IDENTIFICATION | U/O NUMBER 3E52428-101 FITTING ASSEMBLY,SEAT TUBE-C141 AIRCRAFT |
1680-00-225-1250 | LINK, EJECTION SEAT | | |
1680-00-228-2452 | ADAPTER, PILOTS SEAT | | |
1680-00-228-2468 | YOKE ASSY, SEAT | | |
1680-00-228-2472 | ADAPTER ASSY, SEAT | | |
1680-00-228-2475 | ECCENTRIC, SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL MIL-S-5000 COMP 4340,2.660 IN. LG,1.120 IN. ACROSS FLATS,0.900 IN. DIA SHAFT,2.480 IN. LG OF SHAFT,0.625 IN. DIA OF ECCENTRIC HOLE |
1680-00-228-2485 | LEVER, EJECTION SEAT | | |