00-325-2049
Manual Control Lever
Material, steel; finish, passivate; 1.500 in. lg; 1.406 in. w; 0.469 in. h
00-325-2192
Control Cam
Used on teletype and facsimile equip. steel; 4.375 in. l; 0.410 in. dia
00-325-3251
Rigid Connecting Link
7.557" overall length effective length: 6.760"; link info: threading length
00-325-3991
Straight Shaft
6.750" overall length
00-325-4121
Shouldered Shaft
2.187" overall length
00-325-4259
Control Cam
Used on 3810-00-937-3939.
00-325-4260
Control Cam
Used on 3810-00-937-3939.
00-325-6404
Body Hub
Mounted with 1 4-40 setscrew
00-325-7081
Bevel Gearshaft
00-325-7112
Spur Gearshaft
00-325-7128
Spur Gearshaft
00-325-7173
Spur Gearshaft
1.156" overall length
00-325-7957
Bell Crank
1.375" bore diameter raised face pivot
00-325-9920
Spur Gearshaft
3.744" overall length
00-326-0652
Shouldered Shaft
2.516" overall length
00-326-0695
Extension Shaft
0.187" outside diameter 44 stud thread quantity per inch unf stud thread series
00-326-3013
Rigid Connecting Link
00-326-3288
Rigid Connecting Link
00-326-3561
Flexible Shafting
00-326-3648
Flexible Shafting
00-326-3649
Flexible Shaft Assembly
4.375" overall length end item use is landing control central, an/mpn-13
00-326-3651
Flexible Shafting
0.604 feet overall length
00-326-3699
Manual Control Lever
Used on acft model f-14a. cres, S80d fscm U1604, 1.700 in. lg, o/a, 0.595 in. h o/a
00-326-3700
Manual Control Lever
Used on acft model f-14a.
00-326-4125
Spur Gearshaft
00-326-5935
Control Cam
Used on pump rty pwr 85.00gpm.
00-326-6062
Remote Control Lever
Used on f-100 engine.
00-326-6063
Shouldered Shaft
Used on f-100 engine. arm assy, compressor stator synchronizer
00-326-6448
Remote Control Lever
Flat, one hole link end
00-326-6555
Rigid Connecting Link
00-326-7494
Shouldered Shaft
00-326-8095
Remote Control Lever
Used on f-15 aircraft; u/o p/n 3u151-5. consist of bearing MS27841-3, lever 3151-021-1
00-326-8647
Shouldered Shaft
2.870" overall length
00-327-0335
Rigid Connecting Link
2.220" overall length
00-327-0688
Bevel Gearshaft
Used on aircraft, stratolifter c-135. first step has 14 involute splines, 16/32 diametral pitch; weapon system essential
00-327-0726
Shouldered Shaft
Used on c-135 aircraft. 7.890" overall length step behind sm. end is splined-14 splines, mates w/part no.6.72084; splined end has 3 threaded holes, equallyspaced
00-327-0740
Shouldered Shaft
Used on kc-135 aircraft. 7.420" overall length 7threaded end 9/16-18 unf-3a per mil-s-7742; step behind threaded end external involute spline, 14 teeth, mates w/6-72451, 0.87 in.l.; center of shaft inv. spline, 33 teeth, mate w/9-65416; splined end has threaded hole dr. thru splines .25 in. from end
00-327-1447
Rigid Connecting Link
00-327-1448
Rigid Connecting Link
00-327-1449
Rigid Connecting Link
00-327-1450
Rigid Connecting Link
00-327-1451
Rigid Connecting Link
00-327-1452
Rigid Connecting Link
00-327-1453
Rigid Connecting Link
00-327-1458
Rigid Connecting Link
00-327-1459
Rigid Connecting Link
00-327-1462
Rigid Connecting Link
