AIRCRAFT CONTROL DEVICES Parts 1680-00-171-6988 through 1680-00-179-6017 |
|
|
| Leading Edge Sourcing Services |
 |
|
We solve sourcing challenges for parts like 1680-00-171-6988, 1680-00-171-7592, 1680-00-172-3835, 1680-00-172-3836, 1680-00-172-3840, 1680-00-172-5975, 1680-00-172-6003, 1680-00-172-6005, 1680-00-172-6006, 1680-00-175-3848 -- hard to find, long lead time, and obsolete part requirements.
|
 |
|
|
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 >>>
|
| Part number | Description | Category | Details |
1680-00-171-6988 | CONTROL COLUMN, AIRCRAFT | END ITEM IDENTIFICATION | ACFT MODEL C-130 |
1680-00-171-7592 | HARNESS ASSEMBLY, ELECTRICAL, CONTROL | | |
1680-00-172-3835 | ARM, IDLER, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,7.124 IN.LG,1.947 IN. W |
1680-00-172-3836 | SECTOR ASSEMBLY, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,5.907 IN. GROOVE RADIUS,2.160 IN. O/A THK |
1680-00-172-3840 | HUB ASSEMBLY, DIRECTION CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,6.000 IN. O/A LG,3.290 IN. O/A W,5.415 IN. O/A H |
1680-00-172-5975 | BELL CRANK ASSEMBLY, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,COMPOSITION 7075,TEMPER T73,4.000 IN. CENTER TOCENTER DISTANCE BETWEEN FULCRUM AND FIRST ARM END HOLE,4.569 IN.CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND SECOND ARM END HOLE,5.000 IN. CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND THIRD ARM ENDHOLE,1.518 IN. O/A LG |
1680-00-172-6003 | HANDLE, PEDAL ADJUSTING, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY 7075-T7351 QQ-A-250/12,4.749 IN. LG,3.968 IN. W,0.509 IN. THK |
1680-00-172-6005 | ARM, IDLER, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,7.124 IN. LG,2.072 IN. W,1.125 IN. H |
1680-00-172-6006 | TRUNNION, RATIO CHANGER, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,2.031 IN. LG,1.437 IN. W,0.625 IN. THK |
1680-00-175-3848 | LEVER, REMOTE CONTROL | | |
1680-00-175-6648 | CONTROL ASSEMBLY, PUSH-PULL | III END ITEM IDENTIFICATION | T-38 ACFT |
1680-00-176-0959 | CONTROL ASSEMBLY, PUSH-PULL | CORE MATERIAL | STEEL |
1680-00-176-0976 | HANDLE ASSY, CONTROL | | |
1680-00-176-1267 | CONTROL WHEEL, AIRCRAFT | | |
1680-00-176-1269 | CONTROL WHEEL, AIRCRAFT | | |
1680-00-176-1668 | GRIP ASSEMBLY, CONTROLLER, AIRCRAFT | | |
1680-00-176-2636 | GRIP ASSEMBLY, CONTROLLER, AIRCRAFT | | |
1680-00-176-8475 | CONTROL, VALVE ASSEM | III END ITEM IDENTIFICATION | AIRCRAFT MODEL A-4 |
1680-00-178-8275 | CONTROL CABLE, FLIGHT CONTROL | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O1 CABLE 67.187 IN. LG |
1680-00-178-8465 | PEDAL, CONTROL | | |
1680-00-178-9222 | LEVER, REMOTE CONTROL | MATERIAL | STEEL CORROSION RESISTING |
1680-00-179-0349 | SOCKET ASSY, CONTROL | | |
1680-00-179-1229 | TUBE ASSY, CONTROL S | | |
1680-00-179-4013 | CONTROL ASSEMBLY, PUSH-PULL | | |
1680-00-179-6017 | CONTROL STICK, AIRCRAFT | | |