01-534-4453
Aircraft Skin
01-534-4454
Aircraft Skin
01-534-4456
Aircraft Skin
01-534-4458
Aircraft Skin
01-534-4732
Aircraft Door
Used on model e-8a. door assy - ram air plenum nha 525-11408
01-534-4997
Structural Component Air Support
01-534-4999
Structural Component Air Support
01-534-5000
Structural Component Air Support
01-534-5027
Structural Aircraft Plate
Used on model 34 energy absorber on ground support aircraft arresting gear equipment. wear plate
01-534-5303
Trim Elevator Tab
Trim tab elevator
01-534-5319
Structural Component Air Fitting
Used on U-2.
01-534-5322
Aircraft Elevator
Elevator
01-534-5330
Aircraft Elevator
Elevator tab assy
01-534-5335
Aircraft Elevator
Elevator tab assy
01-534-5338
Aircraft Door
Used on u-2 aircraft. door, tail landing gear
01-534-5346
Aircraft Door
Door, tlg composite
01-534-5352
Aircraft Door
Used on f-22 aircraft. tail landing gear door
01-534-5357
Aircraft Door
Used on u-2 dragon lady.
01-534-5366
Structural Aircraft Panel
Hatch assy
01-534-5371
Aircraft Windshield Assembly
Consists of panel
01-534-5372
Aircraft Door
Door
01-534-5375
Structural Aircraft Panel
Hatch assy
01-534-5376
Aircraft Door
Door
01-534-5377
Aircraft Windshield Panel
Single windshield
01-534-5391
Structural Aircraft Panel
Hatch
01-534-5800
Structural Component Air Bracket
Used on chinook helicopter ch47. al aly 2024T0 clad sht per qq-a-250/5 ht tr T42; .032 inc
01-534-5860
Airfoil Rib
Used on A-10A. 6.000" overall length 4.400" overall width 0.040" material thickness nha 160D512000; heat treat 0; dim. are stocksize
01-534-5937
Fuel Aircraft Tank Assembly
Used on fuel system tcn1-up. next higher assembly 213-6960 lines gp-fuel
01-534-6037
Structural Aircraft Panel
01-534-6206
Structural Component Air Fitting
Used on kc-135 stratotanker. 3.000" overall length 2.320" overall width 0.100 " material thickness tee fitting matl al aly 7075-T6 extr, qq-a-277 T6 temper; bac 1506-1442; nha 8-8254; dim are stock matl
01-534-6213
Structural Component Air Fitting
Used on kc-135 stratotanker. 2.700" overall length 2.360" overall width 0.100 " material thickness tee fitting matl al aly 7075 extr, qq-a-277 T6 temper; bac 1506-1442; dim are stock matl
01-534-6266
Structural Component Air Fitting
Used on C-135. 2.930" overall length 2.360" overall width 0.100 " material thickness tee fitting finish 2.30; heat treat T6 temp extr; process specification BAC5423
01-534-6271
Structural Component Air Fitting
Used on C-135. 2.620" overall length 2.360" overall width 0.100 " material thickness tee fitting finish 2.30; heat treat T6 temp extr; process specification BAC5423
01-534-6706
Aircraft Stiffener
Used on helicopter ab212.
01-534-6815
Structural Component Air Support
Used on f/a-22 raptor. 2.348" overall length seal blade dim are stock matl; matl mil-t-9047, 6al-4v titanium bar
01-534-6816
Structural Component Air Support
Used on f/a-22 raptor. matl mil-t-9047, 6al-4v titanium bar
01-534-6817
Structural Component Air Support
Used on f/a-22 raptor. matl mil-t-9047, 6al-4v titanium bar
01-534-6938
Airframe Aircraft Rail
Used on jet engine. 20.960" overall length 0.962" overall width 0.120" material thickness navy-rail, mntg angle material thickness 11 ga hrpo steel; typical hole DIAMETER0.281 inch
01-534-7199
Aircraft Skin
01-534-7201
Structural Aircraft Panel
01-534-7202
Radome
Used on p-3c orion aircraft. radome assembly
01-534-7203
Radome
Used on p-3c orion aircraft. radome assembly
01-534-7218
Aircraft Channel
01-534-7303
Aircraft Skin
01-534-7305
Aircraft Skin
01-534-7328
Structural Component Air Fitting
Used on F/A-22. fitting, support - ram air duct this p/n replaced p/n 5HP46730-115
01-534-7508
Aircraft Bulkhead
8.100" overall length 6.700" overall width 0.016" material thickness details - eng pylon bulkhead & former - instl of
01-534-7563
Structural Component Air Support
Used on c130j hercules fixed wing aircraft.
01-534-7817
Structural Aircraft Plate
8.200" overall length 4.800" overall width 0.040" material thickness gusset - inboard aileron rib no. 7 opposite -2004, heat treat T4
01-534-7925
Structural Aircraft Plate
Used on C-130. angle plate assy nha 02032389; c/o 1 (angle plate -01) , nutplates, rivets
