00-893-1705
Straight Shaft
5.700" overall length
00-893-4324
Control Cam
Cres, 1 1/4 in. o/a lg, 5/8 in. w, 1/2 in. thk
00-893-4325
Control Cam
Steel, qq-s-763, class 7, type c, 0.3125 in. dia bore, 0.625 in. od of hub, 0.594 in. o/a lg
00-893-4479
Straight Shaft
5.875" overall length
00-893-4546
Rigid Connecting Link
43.178" overall length effective length: 42.500"; end attachment info: material aluminum both ends, surface treatment chemical film, fork depth 2.490 to 2.500", height 0.706 inch 1st end, 0.650 inch 2nd end, fork span width 0.817 inch 1st end, 0.692 inch 2nd end; used on forward fuselage section, aircraft
00-893-4811
Straight Shaft
1.875" overall length
00-893-4812
Straight Shaft
3.000" overall length
00-893-5305
Straight Shaft
7.750" overall length
00-893-5308
Straight Shaft
3.500" overall length
00-893-5457
Straight Shaft
21.687" overall length c/o shaft 1; socket 1; internal sq 1st end, 0.781 in. across flats by 0.875 in. lg int hexagon; 2nd end, 0.531 in. across flats by 0.875 in lg
00-893-6898
Shouldered Shaft
00-893-6920
Spur Gearshaft
00-893-8157
Mechanical Drive Housing
Used on aircraft, f-4(phantom).
00-893-8163
Bevel Gearshaft
Number of teeth-gear a: 150, gear b: 150; diametral pitch (cutter) -gear a: 7.650, gear b: 8.000; pitch diam-gear a: 19.6078, gear b: 18.750; full depth (max/min) gear a: 0.309/0.294, gear b: 0.294/0.281; backlash- both gear a
00-893-8175
Shouldered Shaft
6.120" overall length 2 splined shoulders; 23 teeth; 0.7188 pitch dia; 30 deg pressure angle; 2 cross drill holes; 0.093 in dia first end; 0.185 in dia second end
00-894-0133
Shouldered Shaft
14.490" overall length second end drilled 1.571 in. by 10.000 in. deep
00-894-0360
Manual Control Lever
Steel; four mounting holes
00-894-0581
Shouldered Shaft
00-894-1765
Spur Gearshaft
Used on aircraft model tf30.
00-894-1791
Shouldered Shaft
00-894-1897
Shouldered Shaft
00-894-2101
Shaft Collar
0.875" outside diameter 0.5000" bore diameter flat on od opposite thd hole 0.312 in fromcenterline plain round
00-894-4431
Worm Shaft
Used on pan tel 8587534. 0.320" second end, third portion thread length 5.688" overall length
00-894-4507
Control Cam
Lid assy, container; 1660004004222; wb-57f aircraft breathing oxygen system
00-894-4561
Shouldered Shaft
Used on uh-1 series helicopter.
00-894-4739
Hub Clamp
0.562" outside diameter 0.2500" bore diameter passivate surface treated round sectional, two bolt secured
00-894-5025
Retaining Shaft Plate
00-894-5814
Shouldered Shaft
1.955" overall length
00-894-6542
Rigid Connecting Link
Used on uh-1 series helicopter.
00-894-6655
Pawl
1.178" overall length 0.065" material thickness depth from pivot pinhole centerline to point of engagement:0.110 in.nom; length from pivot pinhole centerline to point of engagement:0.938 in.nom crescent, hook stop
00-894-6671
Rigid Connecting Link
Used on colt industries operating corp,diesel engine model 38nd8 1-8.
00-894-7075
Shouldered Shaft
00-894-7076
Worm Shaft
2.500X3.000inch-600lb oil operator-e/i
00-894-8749
Detent Plate
5.500" overall length cadmium surface treated
00-894-8750
Detent Plate
5.500" overall length
00-894-9594
Shouldered Shaft
1.797" overall length
00-894-9773
Shouldered Shaft
3.847" overall length
00-895-3051
Actuating Line Cylinder Assembly
00-895-3061
Shouldered Shaft
7.500" overall length
00-895-3407
Friction Lining
Used on general motors corp,diesel engine,series 71.
00-895-3727
Mechanically Actuated Spindle
Used on cannon,xm168. bconsistsof spring, p/n 7269432; 3 shims, p/N7268309, 7268313, and 7268314; 2 bushings, p/n 7268311, 8437230; 1 nut, p/n MASS1022A10; 1 body, p/n 7268311; material, steel; surface treatment, phosphate
00-895-4387
Pneumatic Accumulator
Used on an/ale-28.
00-895-6429
Actuating Line Cylinder Assembly
4.000" bore diameter
00-895-6496
Control Cam
Corrosion resisting steel, class 303, cond a, spec qq-s-763; dia .390 in.; lg .246 min, .256 max
00-895-7117
Rigid Connecting Link
00-895-8291
Friction Lining
Used on 2f78 training device. shoe included
