01-535-2933
Pressure Fuel Servicing Adapter
Used on astor airborne radar.
01-535-2934
Pressure Fuel Servicing Adapter
Used on astor airborne radar.
01-535-3228
Access Aircraft Cover
Panel assy, ceiling, access cover, mission area nha C99F32302
01-535-3237
Airfoil Rib
Used on KC-135. 6.800" overall length 5.100" overall width 0.082" material thickness 1 opposite; c/o doubler, rib, seal retainers, filler, misc. hardware; heat treat 0 & T6; clad sheet alum
01-535-3238
Structural Component Air Bracket
Used on joint stars. bracket
01-535-3241
Airfoil Rib
Used on KC-135. 7.900" overall length 4.700" overall width 0.040" material thickness rib instal opposite -13, c/o splice plates, rib, attach angle, seal retainer, filler; clad sht; heat treat 0 & T6; finish f-2.115
01-535-3242
Airfoil Rib
Used on KC-135. 7.900" overall length 4.800" overall width 0.040" material thickness rib instl c/o rib, nose rib; opposite -1; finish srf-2.30
01-535-3243
Airfoil Rib
Used on KC-135. 11.700" overall length 6.700" overall width 0.032" material thickness rib instl opposite -1; c/o rib, nose rib, rivets; heat treat T6
01-535-3286
Structural Component Air Fitting
Used on f-16 a/b, groundsystem. 22.000" overall length 14.000" overall width 0.063 " material thickness spacer, frame assembly, protective, fuel cell
01-535-3287
Vertical Stabilizer
Used on aircraft f16 a/b. technical document 1f-16am-4-51, 55-00-00
01-535-3354
Door Aircraft Hinge
01-535-3419
Aircraft Door
Used on mvj-22 aircraft. door assembly, mlg f; v-22
01-535-3616
Aircraft Stiffener
Used on av-8b night attack aircraft. 0.680" overall length 0.260" overall width 0.050" material thickness cover assembly-actuator, rudder, stabilizer, vertical
01-535-3617
Aircraft Stiffener
Used on av-8b night attack aircraft. 0.680" overall length 0.260" overall width 0.050" material thickness cover assembly-actuator, rudder, stabilizer, vertical
01-535-3618
Aircraft Stiffener
Used on av-8b night attack aircraft. 0.680" overall length 0.260" overall width 0.050" material thickness cover assembly-actuator, rudder, stabilizer, vertical
01-535-3780
Aircraft Skin
49.800" overall length 10.500" overall width dim. are stock material
01-535-3965
Aircraft Fairing
01-535-3983
Airfoil Rib
Used on KC-135. 9.000" overall length 5.300" overall width 0.025" material thickness rib instl clad sht alum; opposite -1; dim. are stocksize; c/o rib, nose rib, rivet-blind; heat treat T6 & 0; finish f-2.115
01-535-3984
Airfoil Rib
Used on KC-135. 9.400" overall length 5.500" overall width 0.051" material thickness rib instl opposite -1; c/o rib, splice plate, nose rib, angle stiffener, rivet-blind; clad sht; heat treat T6 & 0; dim. are stocksize; finish f-2.115
01-535-3985
Airfoil Rib
Used on KC-135. 10.100" overall length 5.900" overall width 0.025" material thickness rib instl heat treat T6 & 0; dim. are stocksize; c/o rib, nose rib, blind rivets; opposite -1
01-535-4012
Structural Component Air Bracket
01-535-4017
Aircraft Former
01-535-4024
Structural Component Air Support
U/o f-15e CUM2-209, f-15s CUM1-12
01-535-4065
Aircraft Spar
Used on b-52 stratofortress. 80.000" overall length spar matl al 7075-0 sheet clad; qq-a-287 T6 temper, bac 1493-330; u/o 58-188
01-535-4121
Structural Component Air Fitting
17.400" overall length 1.720" overall width core 1; skin 2; filler 3; doubler 2;
01-535-4145
Structural Component Air Support
Used on oh-58d 1520-01-125-5476. 0.090" material thickness strap
01-535-4148
Thermal Aircraft Insulation
Insulation blanket
01-535-4204
Aircraft Former
Y strake 364940 upper former
01-535-4208
Aircraft Former
Y strake 964940 upper former
01-535-4210
Supplemental Small Arms-fr Armor
01-535-4211
Supplemental Small Arms-fr Armor
01-535-4212
Supplemental Small Arms-fr Armor
01-535-4277
Aircraft Door
Used on f/a-22 raptor. finish assy c/o 1 (ref 5HA40101-112 door assy) , 2 coating appl
01-535-4287
Structural Component Air Support
Used on f/a-22 raptor.
01-535-4288
Structural Component Air Support
Used on f/a-22 raptor.
01-535-4308
Movable Canopy
Used on f/a-22 raptor. canopy same as-205, -207, except diff.effectivity; used on forward fuselage
01-535-4313
Structural Aircraft Panel
Used on f/a-22 raptor. 32.000" overall length 12.000" overall width panel, assy of c/o 1 (-115 panel) , 1 bracket instl, 1 gasket, 1 plate, 2 pin, 2 nut, 2oz. polythidether; ann. tit. sheet
01-535-4315
Structural Aircraft Panel
Used on f/a-22 raptor. 40.000" overall length 14.000" overall width panel assy c/o 1 (-119 panel) , 1 gsket, 2 plates, 4 pins, 4 nuts, 4 oz. ploythidether; ann. tit. sheet
01-535-4323
Structural Component Air Support
Post
01-535-4375
Fuel Aircraft Tank
Used on U2.
01-535-4378
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4383
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4386
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4444
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4447
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4448
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4450
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4452
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4455
Fuel Aircraft Tank
Used on u-2 aircraft.
01-535-4504
Aircraft Skin
Used on B-52. 12.800" overall width skin-fairing clad alum sheet; heat treat T6 & 0; finish f 2.115; dim. are stocksize
