00-955-6363
Structural Component Air Support
Used on acft model f-4. aluminum alloy casting per qq-a-596 composition 8
00-955-6374
Access Aircraft Door
00-956-0521
Aircraft Skin
00-956-0522
Aircraft Skin
00-956-0524
Structural Component Air Fitting
00-956-0752
Aircraft Door
Used on F-104.
00-956-0753
Aircraft Leading Edge
0.050" material thickness
00-956-0816
Aircraft Leading Edge
0.050" material thickness
00-956-0817
Structural Component Air Support
00-956-3604
Structural Aircraft Panel
C/o 1 panel, 5 support, hardware
00-956-3725
Aircraft Fairing
00-956-3726
Aircraft Skin
00-956-3727
Aircraft Skin
40.000" overall length 36.000" overall width
00-956-3729
Aircraft Skin
40.000" overall length 12.000" overall width
00-956-4021
Wing Panel Outer Rib
00-956-4022
Wing Panel Outer Rib
00-956-4064
Structural Component Air Support
Used on acft model f-4. aluminum alloy 7075-T73, 8.300 in.lg, 8.300 in. w, 1.250 in. thk
00-956-4065
Structural Component Air Support
Used on acft model f-4. aluminum alloy 7075-T73, 6.450 in. lg, 6.450 in. w, 1.250 in. thk
00-956-5412
Structural Component Air Support
00-956-5606
Structural Component Air Support
Matl:250 microinch machine fin
00-956-6420
Fuel Aircraft Tank
External fuel, 50 gal capacity
00-956-9929
Structural Component Air Support
Used on aircraft model ch-47. aluminum alloy
00-957-1664
Wing Landing Flap
00-957-1680
Wing Landing Flap
00-957-1681
Wing Landing Flap
Used on aircraft model no. c-141.
00-957-1683
Wing Landing Flap
Used on aircraft model no. c-141.
00-957-6496
Metal Molding
00-957-7290
Aircraft Step
8.942" overall length 4.000" overall width
00-957-7339
Access Aircraft Door
00-957-7340
Structural Component Air Fitting
00-957-8218
Structural Aircraft Panel
00-957-8258
Aircraft Door
00-958-0960
Structural Component Air Support
00-958-0962
Structural Component Air Support
00-958-4445
Structural Component Air Support
00-958-4446
Structural Component Air Support
00-958-4447
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, AMS4260, 2.570 in.lg, 1.620 in. w, 2 holes 0.375 in. dia, 4 holes 0.245 in. dia
00-958-4448
Bell Crank
0.375" bore diameter first arm end radius: 0.310 in. ; second arm end radius: 0.310 in. ; first arm thickness: 0.620 in. ; second arm thickness: 0.620 in. ; first arm slot depth: 0.690 in. ; first arm slot width: 0.130 in. ; second arm horizontal slot width: 0.130 in. raised face pivot hole, clevis both ends
00-958-4490
Structural Component Air Support
00-958-4881
Aircraft Latch Assembly
Rotary latch assembly
00-959-2302
Structural Aircraft Plate
00-959-5666
Access Aircraft Door
00-959-5678
Access Aircraft Door
00-959-5693
Aircraft Skin
Used on aircraft model t-2b.
00-959-5702
Structural Component Air Fitting
00-959-5703
Structural Component Air Fitting
00-959-5717
Structural Component Air Fitting
00-959-5747
Structural Component Air Fitting
Used on p-3 aircraft.
