01-238-0579
Structural Component Air Support
33.250" overall length 0.620" overall width 0.060" material thickness
01-238-0580
Structural Component Air Support
39.250" overall length 0.620" overall width 0.125" material thickness
01-238-0581
Structural Component Air Support
01-238-0841
Structural Component Air Support
Used on aircraft model f/a18a and tf/a18a.
01-238-0847
Structural Aircraft Panel
Used on acft model c-5a. cp titanium annealed per STM07-306 type 1 comp b; 5.0 in. lg, 5.0 in. wd, 0.040 in. thk
01-238-0848
Structural Aircraft Panel
Consists of one panel; one rug; one batt; one strap
01-238-0859
Aircraft Skin
Aluminum alloy, qq-a-250/13, alloy 7075, core
01-238-2451
Access Aircraft Door
Used on sh-60b helicopter.
01-238-2553
Structural Aircraft Plate
Used on F-15. 8.100" overall length 7.000" overall width 0.063" material thickness opposite -2280
01-238-2555
Structural Aircraft Plate
Used on C-141. made from JW11095-131
01-238-2556
Structural Aircraft Plate
Used on C-141. made from JW11095-133
01-238-2557
Structural Aircraft Plate
Used on C-141. made from JW11095-133
01-238-2561
Structural Aircraft Plate
Used on C-141. made from JW11095-135
01-238-2562
Structural Aircraft Plate
Used on C-141. made from JW11095-136
01-238-2563
Structural Aircraft Plate
Used on C-141. made from JW11093-138
01-238-2564
Structural Aircraft Plate
Used on C-141. made from JW11095-122
01-238-2565
Structural Aircraft Plate
Used on C-141. made from JW11095-123
01-238-2566
Structural Aircraft Plate
Used on C-141. material per JW11095-124
01-238-2567
Structural Aircraft Plate
Used on C-141. material per JW11095-125
01-238-2568
Structural Aircraft Plate
Used on C-141. material per JW11095-125
01-238-2569
Structural Aircraft Plate
Used on C-141. material per JW11097-106
01-238-2570
Structural Aircraft Plate
Used on C-141. material per JW11097-106
01-238-2571
Structural Aircraft Plate
Used on C-141. material per JW11096-112
01-238-2572
Structural Aircraft Plate
Used on C-141. material per JW11095-133
01-238-2573
Structural Aircraft Plate
Used on C-141. material per JW11096-111
01-238-2580
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0; angle p/o bracket-aileron actuator pressure reducer
01-238-2581
Structural Component Air Support
Used on acft model a-10. strap-canopy structure
01-238-2582
Structural Component Air Support
Used on acft model a-10. strap-canopy structure
01-238-2589
Structural Aircraft Panel
LS5796 by 57.0 in; heat treat T6511; finish aa-19-24 type iii aluminized; nha 3W19029
01-238-2605
Aircraft Boom
Used on helicopter model h-1.
01-238-2614
Aircraft Former
4.700" overall length 3.000" overall width 0.040" material thickness
01-238-2615
Aircraft Former
01-238-2620
Aircraft Former
284.000" overall length LS30718-1 by 284.0 in; finish f-1-1; nha 3F30000
01-238-2623
Exhaust Pipe
Used on aircraft model a-4. cognizant service: usn
01-238-3154
Structural Aircraft Plate
01-238-3156
Structural Component Air Support
Used on f-14 aircraft.
01-238-3157
Structural Component Air Support
01-238-3158
Structural Component Air Support
12.120" overall length
01-238-3159
Structural Component Air Support
9.870" overall length 0.045" material thickness
01-238-3160
Structural Component Air Support
Aluminum alloy, qq-a-250/4, alloy 2024, T62, 0.050 in. thk
01-238-3161
Structural Component Air Support
01-238-3443
Structural Aircraft Plate
Used on C-141. 14.000" overall length 1.000" overall width 0.375" material thickness bare aa-19-24 type 111; T7351 finish; nha 3W19031
01-238-3452
Structural Aircraft Plate
Used on C-141. 4.000" overall length 2.000" overall width 0.032" material thickness
01-238-3457
Structural Aircraft Plate
Used on C-141. make from 3W11060-404
01-238-3460
Structural Aircraft Plate
Used on C-141. material per JW11096-108
01-238-3461
Structural Aircraft Plate
Used on C-141. material per JW11095-119
01-238-3462
Structural Aircraft Plate
Used on C-141.
01-238-3463
Structural Aircraft Plate
Used on C-141.
01-238-3464
Structural Aircraft Plate
Used on C-141.
