01-235-2338
Aircraft Skin
Used on C-130.
01-235-2339
Aircraft Skin
Used on C-130. cond a, rc-70
01-235-2340
Aircraft Skin
Used on F-15. T81
01-235-2342
Aircraft Skin
Used on F-15. T81
01-235-2344
Aircraft Skin
Used on F-15. T81
01-235-2345
Aircraft Skin
Used on F-15. T81
01-235-2346
Aircraft Spar
01-235-2348
Aircraft Spar
01-235-2349
Aircraft Spar
01-235-2845
Aircraft Skin
01-235-3358
Aircraft Bulkhead
01-235-3374
Structural Aircraft Plate
Used on acft model f-16. material per fms-3022-T81, 29.000 in. lg, 8.000 in. w, 0.125 in. thk
01-235-3375
Structural Aircraft Plate
Used on C-130. T6 clad
01-235-3377
Structural Component Air Support
Used on f-15 acft. p/o former, empennage support beam; fuselage station 721.830
01-235-3378
Structural Component Air Support
Used on f-15 acft. support-trunnion, nose landing gear
01-235-3379
Structural Component Air Support
Used on f-15 acft. support, mechanism-nose landing gear uplock, aft
01-235-3387
Longeron
Cond 0
01-235-3388
Aircraft Skin
Used on C-130. clad 0
01-235-3389
Aircraft Skin
Used on F-15.
01-235-3390
Aircraft Skin
Used on F-15.
01-235-3391
Aircraft Skin
Used on F-15. T81
01-235-3743
Aircraft Stiffener
28.000" overall length 6.000" overall width 0.063" material thickness engine lower access
01-235-3820
Aircraft Skin
01-235-4740
Aircraft Thrust Reverser Section
Used on sentry f22 aircraft. drum assembly thrust
01-235-4818
Access Aircraft Cover
Used on KC-135.
01-235-4820
Structural Component Air Support
Used on 1560-01-211-8559. type/model designation:AV8b/GRMK5 z cross section; 10.680 in. o/a lg; 1.797 in. o/a w; 21 bolt holes 0.190 in. min 0.193 in. max dia; right hand appl
01-235-4823
Control Surface Aircraft Fairing
Used on 1560-01-211-8560.
01-235-5032
Aircraft Fairing
Used on aircraft model av8b.
01-235-5033
Control Surface Aircraft Fairing
26.859" overall length 0.500" material thickness
01-235-5034
Control Surface Aircraft Fairing
20.547" overall length 0.500" material thickness
01-235-5035
Aircraft Fairing
Used on aircraft model av8b.
01-235-5036
Control Surface Aircraft Fairing
19.703" overall length 0.500" material thickness
01-235-5217
Structural Aircraft Plate
Used on acft model kc-135. 2024-T3 alum clad per qq-a-250/5; finish f-2.03; 3.0 in. lg, 1.2 in. wd, 0.080 in. thk
01-235-5218
Structural Component Air Support
Used on c-5b aircraft. matl 4340 steel comp per mil-s-8844 class 1, cond f-4; size 0.625X1.0X2.0; fitting-cable, power spring, aft service door; nha 4F61271
01-235-5219
Structural Component Air Support
Used on c-5b aircraft. bracket assembly-duct support, aft, cooling vent, nacelle to pylon; c/o: flange (1) , -703a bracket (1) c.p. titanium, size 0.050X4.0X10.0
01-235-5220
Structural Component Air Support
Used on c-5b aircraft. bracket assembly-duct support, aft, cooling vent, nacelle to pylon; c/o: flange (1) , -707a bracket (1) c.p. titanium, size 0.050X4.0X10.0
01-235-5221
Structural Component Air Support
Used on c-5b aircraft. bracket assembly, attach-actuator support, mlg inner door; c/o: -103a bracket (1) , bearing (4) ; nha 4F23031, 4F23032, 4F23033, & 4F23034
01-235-5222
Structural Component Air Support
Used on c-5b aircraft. bracket assembly, attach-actuator support, mlg inner door; c/o: -104a bracket (1) , bearing (4) ; nha 4F23031, 4F23032, 4F23033, & 4F23034
01-235-5223
Structural Component Air Support
Used on acft model kc-135. consist of 1 support, 2 cam follower, 1 lockwire, 1 insert, 1 roll pin; nha 458-58042
01-235-5224
Structural Component Air Support
Used on acft model kc-135. 7075-T6 forging per qq-a-367 comp 10; located at rudder sta 146.78; nha 5-89032; finish f-2.30
01-235-5227
Structural Aircraft Panel
Used on c-5b aircraft. panel, trim-lower opening, forward service door; nha 4E20001
01-235-5247
Aircraft Windshield Panel
01-235-5427
Structural Component Air Support
Type/model designation:AV8b aluminum alloy 7075-t, mms 159 cond T7351, matl 2.250 in. thk by 1.500 in. w by 1.859 in. lg
01-235-5838
Aircraft Floor
Used on ch-47 series acft.
01-235-6033
Structural Aircraft Plate
Type/model designation:AV8b aluminum alloy 7075 qq-a-250/24 cond T76, matl 0.125 in. thk by 0.500 in. w by 1.672 in. lg
01-235-6034
Structural Aircraft Plate
Type/model designation:AV8b aluminum alloy 7075 qq-a-250/24 cond T76, matl 0.125 in. thk by 0.500 in. w by 1.750 in. lg
01-235-6035
Structural Aircraft Plate
Type/model designation:AV8b aluminum alloy 7075 qq-a-250/24 cond T76, matl 0.125 in. thk by 0.500 in. w by 1.750 in. lg
01-235-6036
Structural Aircraft Plate
Type/model designation:AV8b aluminum alloy 7075 qq-a-250/24 cond T76, matl 0.125 in. thk by 0.500 in. w by 1.672 in. lg
01-235-6037
Structural Aircraft Plate
Type/model designation:AV8b aluminum alloy 7075 qq-a-250/24 cond T76, matl 0.125 in. thk by 0.500 in. w by 1.750 in. lg
