00-181-2972
Rigid Connecting Link
9.820" overall length effective length: 8.480 to 8.540"; end attachment diameter: 1.310 to 1.370"
00-181-2973
Rigid Connecting Link
49.711" overall length effective length: 48.700"; link threading length anodize surface treated
00-181-2974
Rigid Connecting Link
Used on ch-47 chinook airframe unit.
00-181-2975
Rigid Connecting Link
00-181-2977
Rigid Connecting Link
11.455" overall length
00-181-2978
Rigid Connecting Link
00-181-2979
Rigid Connecting Link
00-181-2980
Rigid Connecting Link
00-181-2981
Rigid Connecting Link
14.015" overall length effective length: 12.900"; link threading length cadmium alloy surface treated
00-181-2983
Rigid Connecting Link
00-181-2984
Rigid Connecting Link
1.961" overall length 0effective length: 40.950"; link threading length anodize surface treated
00-181-2985
Rigid Connecting Link
33.631" overall length effective length: 32.620"; link threading length anodize surface treated
00-181-2986
Rigid Connecting Link
59.541" overall length effective length: 58.530"; link threading length anodize surface treated
00-181-2988
Shouldered Shaft
00-181-2994
Rigid Connecting Link
41.153" overall length eeffective length: 40.000"; link thread info: right hand, length 1.090 7/16-20 nf; end attachment info: 2nd end upper jaw diameter 0.4388 to 0.4393 inch; 2nd end lower jaw diameter 0.312 to 0.313 inch; diameter 1.125 1st end, 1.180 2nd end; material steel, surface treatment cadmium plated, locknut included, fork depth 1.693 1st end, 1.710 2nd end, fork span width 0.440 1st end, 0.590 2nd end; fork end to hole center 0.563 1st end, 0.590 2nd end anodize surface treated
00-181-2996
Rigid Connecting Link
00-181-2997
Rigid Connecting Link
41.120" overall length effective length: 40.000"; link thread info; right hand, length 1.090 inch 7/16-20 nf, diameter 1.060 1st end, 1.180 2nd end; end attachment info: 2nd end clevis upper jaw has drilled hole diameter of 0.4388 to 0.4393 inch, 2nd end clevis lower jaw has drilled hole diameter of 0.3120 to 0.3130 inch; material steel, mil-s-5000 comp 4340 cond f both ends, surface treatment anodized, mil-c-6541 both ends, locknut included, fork depth 1.650 1st end, 1.710 2nd end; fork span width 0.297 1st end, 0.590 2nd end; fork end to hole center 0.530 1st end, 0.590 2nd end anodize surface treated
00-181-2998
Rigid Connecting Link
00-181-2999
Rigid Connecting Link
34.468" overall length effective length: 33.250"; link thread info: right hand; end attachment info: material stainless steel, AMS5643; surface treatment passivated 1st end, cadmium plated 2nd end; connecting hole bearing location both ends, locknut included, rockwell c 42.0, diameter 1.066 1st end, 1.406 2nd end; 1st end thread length 1.220 to 1.310 3/8-24 unf, 2nd end thread length 1.375 1/2-20 nf anodize surface treated
00-181-3115
Multiple Gears Gearshaft
00-181-3116
Multiple Gears Gearshaft
Used on j-52 aircraft engine.. weapon system essential
00-181-3185
Straight Shaft
3.062" overall length internally thd longitudionally drilled hole on 2nd end 0.060-80 thds, unf, class 2b, tapped, 0.250 in. deep
00-181-3186
Straight Shaft
2.468" overall length
00-181-3193
Spur Gearshaft
1.918" overall length
00-181-3197
Retaining Shaft Plate
1.625" overall length 0.750" overall width 1.187 in. between mtg holes
00-181-3204
Remote Control Lever
0.250" bore diameter offset height: 1.312 in. ; surface treatment: olive drab paint paint surface treated
00-181-3214
Shouldered Shaft
1.250" overall length
00-181-3225
Rigid Connecting Link
7.000" overall length
00-181-3226
Rigid Connecting Link
00-181-3508
Rigid Connecting Link
00-181-3569
Shouldered Shaft
Used on C-54. steel 4130 mil-s-6758
00-181-4216
Counterbalance Weight
00-181-4234
Bevel Gearshaft
00-181-4302
Shouldered Shaft
Used on 1650-00-225-1878,motor hydraulic.
00-181-4305
Mechanical Drive Housing
00-181-4453
Counterbalance Weight
00-181-5606
Rigid Connecting Link
00-181-5838
Shouldered Shaft
1.250" overall length
00-181-6063
Counterbalance Weight
00-181-6173
Manual Control Lever
0.780 in. lg, 0.153 in. w, 0.025 in. thk, matl no. 238 alloy (yellow brass) , special shape
00-181-7667
Shaft Collar
0.250" outside diameter 0.0940" bore diameter bore round stepped
00-181-8811
Rigid Connecting Link
13.000" overall length second end square w/a second hole located 1.062 c to c from first hole
00-181-8812
Rigid Connecting Link
00-181-9400
Rigid Connecting Link
00-181-9401
Rigid Connecting Link
00-181-9402
Rigid Connecting Link
00-181-9804
Rigid Connecting Link
00-182-3209
Retaining Shaft Plate
2.752" outside diameter mtg holes equally spaced on 2.000 in. dia bolt circle
00-182-4830
Flexible Shaft Assembly
Used on sikorsky aircraft; engine, aircraft, t64-ge-3/7 (h-53b/c/h, hh-53b); helicopter, rh-53; helicopter, sof/hh-53h pave low; helicopter, super jolly h-53; helicopter, ch-53a/d/e. 50.068" overall length weapon system essential
00-182-4834
Control Cam
Steel; 1.750 in. l; 1.000 in. w; 1.000 in. h
