01-098-9598
Aircraft Leading Edge
Used on F-15. retrofit
01-098-9604
Aircraft Skin
Used on c-135 airplane.. mfg ref sin panel-bonded
01-098-9607
Structural Aircraft Panel
01-099-1175
Aircraft Skin
Used on F-15. retrofit
01-099-1802
Aircraft Skin
Used on f-111 aircraft. 16.000" overall length 12.000" overall width
01-099-2358
Bell Crank
Used on uh60 blackhawk.
01-099-3240
Aircraft Pylon
Used on model no. f-5e/f-5f.
01-099-4294
Structural Aircraft Plate
Used on acft b52. parachute door, adjusting. 2.250 in. lg, 4.500 in. w, 0.600 in. thk. sheet steel 4130 an qq-s-685 norm. heat treat 160, 000 to 180, 000 psi, finish f-1.20 type i, except .0002-.0003 thick
01-099-4295
Structural Aircraft Plate
Used on acft b52. parachute door, adjusting. 2.250 in. lg, 4.500 in. w, 0.600 in. thk. sheet steel 4130 an qq-s-685 norm. heat treat 160, 000 to 180, 000 psi, finish f-1.20 type i, except .0002-.0003 thick
01-099-6399
Aircraft Door
01-099-6722
Structural Aircraft Panel
C/o 4 doubler, 1 inner skin, 1 outer skin
01-099-6723
Structural Aircraft Panel
C/o 4 doubler, 1 inner skin, 1 outer skin
01-099-6790
Longeron
37.000" overall length 10.000" overall width 0.071" material thickness
01-099-8086
Vertical Stabilizer
53.480" overall length ventral fin assembly
01-099-8595
Aircraft Leading Edge
Used on aircraft model a-7e.
01-099-8597
Aircraft Pylon
Used on aircraft model a-7e.
01-099-8598
Aircraft Pylon
Used on aircraft model a-7e.
01-099-9727
Aircraft Fairing
33.000" overall length 12.000" overall width 0.063" material thickness 0 temper; heat treat T6; finish f-2.115
01-099-9730
Aircraft Fairing
01-099-9731
Aircraft Channel
01-099-9733
Aircraft Channel
01-099-9735
Aircraft Channel
01-099-9736
Aircraft Channel
01-099-9737
Aircraft Channel
01-099-9738
Aircraft Channel
01-099-9739
Aircraft Channel
Engine nacelle; heat treat T4
01-099-9761
Structural Aircraft Plate
01-099-9762
Aircraft Fairing
34.000" overall length 7.000" overall width 0.032" material thickness mat 6al-6v-2sn
01-099-9763
Aircraft Fairing
3.000" overall length 2.000" overall width 0.110" material thickness cond -T62
01-099-9771
Cowling
Used on C-135. 14.500" overall length 3.350" overall width 0.050" material thickness
01-099-9772
Cowling
Used on C-135. 14.500" overall length 3.350" overall width 0.050" material thickness
01-099-9773
Cowling
Used on C-135. 14.500" overall length 3.800" overall width 0.050" material thickness
01-100-1688
Aircraft Skin
Used on H-60A. oil cooler inst sta 387.30 - 411.285 main rotor pylon
01-100-1701
Structural Component Air Fitting
Used on H-60A. 2.875" overall length 2.000" overall width pivot assembly, tail rotor blade
01-100-1742
Structural Component Air Support
01-100-1939
Supplemental Small Arms-fr Armor
01-100-1940
Supplemental Small Arms-fr Armor
01-100-2270
Aircraft Channel
11.000" overall length 2.500" overall width 0.050" material thickness engine nacelle; heat treat T4
01-100-2271
Aircraft Channel
11.000" overall length 2.500" overall width 0.050" material thickness engine nacelle; heat treat T4
01-100-2272
Aircraft Channel
8.000" overall length 7.400" overall width 0.050" material thickness engine nacelle; heat treat T4
01-100-2273
Aircraft Channel
13.000" overall length 7.400" overall width 0.050" material thickness engine nacelle; heat treat T4
01-100-2274
Aircraft Intercostal
23.500" overall length 3.300" overall width 0.050" material thickness heat treat T4
01-100-2277
Aircraft Channel
9.000" overall length 2.800" overall width 0.050" material thickness engine nacelle; heat treat T4
01-100-2286
Structural Component Air Fitting
Matl:al heat forged; temper T411
