AIRCRAFT SEAT RELATED Parts 1680-00-005-1428 through 1680-00-008-0086 |
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We solve sourcing challenges for parts like 1680-00-005-1428, 1680-00-005-1432, 1680-00-006-0897, 1680-00-006-2112, 1680-00-006-2114, 1680-00-006-2115, 1680-00-006-2116, 1680-00-006-4373, 1680-00-006-4438, 1680-00-006-4456 -- hard to find, long lead time, and obsolete part requirements.
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| Part number | Description | Category | Details |
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1680-00-005-1428 | FITTING ASSEMBLY, SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CADMIUM PLATED FINISH,1.015 IN. DIA HOLE IN CONNECTOR BLOCKPART NO. A-8727,0.316 IN. DIA HOLE IN CENTER OF CONNECTOR TUBE PARTNO. A-8726,0.1935 IN. DIA HOLE IN ADAPTER TUBE PART NO. A-8725,HOLECENTERS TO BE IN SAME PLANE WITHIN 0.015 IN.,HH-1H ACFT |
| 1680-00-005-1432 | FORK END ASSEMBLY, SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ITEM CONSISTS OF FORK END PART NO. A-MBEU-36439,STUD PART NO.A-MBEU-1766H5,0.093 IN. DIA INDENT PIN PART NO. DS9-A10,0.062 IN.DIA RIVET PART NO. AS155-206,USED ON SEAT ASSY PART NO. MBEU36726,SEAT INSTALLATION PILOT EJECTION PART NO. 32-82026-301,F/4C ACFT |
1680-00-006-0897 | PLATE ASSY, SEAT, PIL | | |
| 1680-00-006-2112 | WEDGE ASSEMBLY, SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 20.38 IN. LG,18.14 IN. W,F-120 FABRIC |
| 1680-00-006-2114 | STRUCTURAL ASSEMBLY, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 49.00 IN. LG,11.75 IN. W,2.00 IN. THK,SKIN WITH HONEYCOMB CORE |
| 1680-00-006-2115 | LEVER, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,0.38 IN. THK,3.75 IN. LG STOCK SIZE |
| 1680-00-006-2116 | CAM, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,0.380 IN. THK,2.000 IN. W,3.000 IN. LG |
| 1680-00-006-4373 | GUIDE, SEAT PAN PIPE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 2.250 IN. LG,0.970 IN. W,0.430 IN. H |
| 1680-00-006-4438 | INSERT, VALVE, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,1.125 IN. LG,0.550 IN. DIA |
| 1680-00-006-4456 | INSERT, CONTAINER ASSEMBLY, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,ANODIZED,MIL-A-8625,TYPE II,CLASS 2,COLORBLACK,1.900 IN. LG,0.250 IN. W,0.160 IN. H |
| 1680-00-006-4462 | CLAMP, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | NYLON 0.62 IN. THK,1.12 IN. H,5.02 IN. LG |
| 1680-00-006-5155 | PLATE ASSY, SEAT, PIL | | |
| 1680-00-007-0448 | HOUSING, SEAT | | |
| 1680-00-007-0450 | COVER ASSY, SEAT CUS | | |
| 1680-00-007-0451 | CUSHION ASSY, SEAT B | | |
| 1680-00-007-0452 | CUSHION ASSY, SEAT B | | |
| 1680-00-007-0453 | ARMCAP ASSY, SEAT | | |
| 1680-00-007-0457 | CUSHION ASSY, SEAT, A | | |
| 1680-00-007-0458 | CUSHION ASSY, SEAT, A | | |
| 1680-00-007-1432 | RELEASE, EJECTION SEAT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,CADMIUM PLATED,1.250 IN. LG,1.250 IN. W |
| 1680-00-007-6518 | SEAT INSTALLATION H | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY |
| 1680-00-007-8663 | SEAT, SPRING POSITION | III END ITEM IDENTIFICATION | AIRCRAFT MODEL AV-8A |
| 1680-00-007-9773 | COVER, SEAT PAN QUADRANT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | BLACK ANODIC FINISH,0.562 IN. THK |
| 1680-00-008-0085 | CUSHION ASSY, SEAT B | | |
| 1680-00-008-0086 | COVER ASSY, SEAT BAC | | |
