01-235-6038
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 2.234 in. lg
01-235-6866
Structural Component Air Support
2.570" overall length 2.020" overall width 0.040" material thickness anodize surface treated
01-235-7527
Structural Component Air Support
Used on acft model f-111t. aluminum alloy per qq-a-282 condition T6 7075-T6, 2.000 in. lg, 1.500 in. w, 0.500 in. thk ftldgused on actuator, canopy seal valve
01-235-7915
Access Aircraft Door
Used on AH64A.
01-235-7949
Aircraft Fairing
01-235-8408
Aircraft Former
01-235-8409
Aircraft Skin
Used on f-15c/d aircraft.
01-235-9220
Access Aircraft Cover
01-235-9329
Structural Aircraft Plate
Used on F-15. gang channel
01-235-9330
Structural Aircraft Plate
Used on F-15. 6081 T6
01-235-9332
Structural Aircraft Plate
Used on F-15. 73.000" overall length 5.300" overall width 0.220" material thickness opposite -2008; splice
01-235-9333
Structural Aircraft Plate
Used on F-15. 5.500" overall length 5.500" overall width 1.500" material thickness
01-235-9334
Structural Aircraft Plate
Used on F-15. splice
01-235-9335
Structural Aircraft Plate
Used on F-15. splice angle
01-235-9336
Structural Aircraft Plate
Used on F-15. splice angle
01-235-9340
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-T3; angle-conduit sopport, wing
01-235-9349
Aircraft Pylon
01-235-9350
Airfoil Rib
15.000" overall length 6.500" overall width 0.100" material thickness 6al-4v; nha 68A230000
01-235-9351
Aircraft Skin
Used on F-15. 22.000" overall length 22.000" overall width part of -1001 skin, spindle bay; opposite p/n -2006; type 3, comp 3, cond annealed, 6al-6v-2sn
01-235-9352
Aircraft Skin
Used on F-15. 22.000" overall length 22.000" overall width type 3, comp e, cond annealed, 6al-6v-2sn; part of -1002 skin, spindle bay; opposite p/n -2005
01-235-9354
Aircraft Trailing Edge
01-235-9355
Aircraft Trailing Edge
01-235-9356
Aircraft Trailing Edge
01-235-9788
Structural Aircraft Plate
Type/model designation:AV8b steel corrosion resisting 304 qq-s-766 annealed class 304, matl 0.312 in. thk by 4.594 in. w by 5.203 in. lg
01-236-1130
Structural Aircraft Plate
Used on F-15. T6
01-236-1131
Structural Component Air Support
Used on f-15 acft. support-trunnion nose landing gear
01-236-1132
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075 forging; 2 bushings; u/o mechanism-nose landing gear uplock, forward
01-236-1133
Structural Component Air Support
Used on f-15 acft.
01-236-1267
Structural Component Air Support
5.820" overall length 4.250" overall width
01-236-2022
Aircraft Fairing
01-236-2024
Structural Component Air Support
0.064" material thickness
01-236-2025
Structural Component Air Support
0.064" material thickness
01-236-2026
Structural Component Air Support
Used on aircraft model f14a. 7.000" overall length 5.000" overall width 0.040" material thickness
01-236-2027
Structural Component Air Support
Used on f-14a aircraft.
01-236-2028
Structural Component Air Support
Used on f-14a aircraft.
01-236-2029
Structural Component Air Support
Used on f-14a aircraft.
01-236-2087
Fluid Aircraft Manifold
01-236-2233
Aircraft Thrust Reverser
01-236-2234
Aircraft Thrust Reverser
01-236-2769
Structural Component Air Support
01-236-3563
Structural Aircraft Plate
Used on F-15. 0.720" overall length 0.720" overall width 0.020" material thickness also called seal plate
01-236-3564
Structural Aircraft Plate
Used on F-15. 1.300" overall length 1.300" overall width 0.020" material thickness also called seal plate
01-236-3565
Structural Aircraft Plate
Used on F-15. 1.5000" overall length 1.500" overall width 0.020" material thickness also called seal plate
01-236-3567
Structural Aircraft Plate
Used on F-15. 26.000" overall length 7.000" overall width 0.080" material thickness also known as splice strap; clad one side
01-236-3568
Structural Aircraft Plate
Used on F-15. 7.800" overall length 2.660" overall width 0.032" material thickness also known as a doubler
01-236-3569
Structural Aircraft Plate
Used on F-15. 3.100" overall length 0.750" overall width 0.050" material thickness also known as clip
01-236-3570
Structural Component Air Support
1.400" overall length
