01-232-3777
Structural Component Air Bracket
Used on sentry f22 aircraft. bracket assembly
01-232-3974
Airframe Modification Kit
01-232-4004
Aircraft Stringer
0.540" overall length 0.063" material thickness
01-232-4162
Structural Component Air Support
01-232-4163
Structural Component Air Support
Used on acft model f-111.
01-232-4338
Structural Component Air Support
Used on f-14a aircraft. anodize surface treated
01-232-4339
Structural Component Air Support
Used on f-14a aircraft. 3.850" overall length anodize surface treated
01-232-4340
Structural Component Air Support
Used on f-14a aircraft. 0.050" material thickness
01-232-5200
Aircraft Floor
Used on A-37.
01-232-5848
Structural Aircraft Plate
Used on acft model kc-135. aisi 321 or 347 cres sheet per mil-s-672 annealed; opposite p/n -14; finish F8.07; 2.5 in. lg, 1.1 in. wd, 0.040 in. thk; nha 65-10506
01-232-5849
Structural Aircraft Plate
Used on acft model kc-135. aisi 321 or 347 cres sheet per mil-s-672 annealed; finish F8.07; nha 65-10506; opposite p/n -13; 2.5 in. lg, 1.1 in. wd, 0.040 in. thk
01-232-5850
Structural Aircraft Plate
Used on acft model kc-135. aisi 321 or 347 cres sheet per mil-s-672 annealed; opposite p/n -12; 10.5 in. lg, 1.1 in. wd, 0.040 in. thk; nha 65-10506; finish F8.07
01-232-5851
Structural Aircraft Plate
Used on acft model kc-135. aisi 321 or 347 cres sheet per mil-s-672 annealed; opposite p/n -11; finish F8.07; 10.5 in. lg, 1.1 in. wd, 0.040 in. thk; nha 65-10506
01-232-6382
Thermal Special Purpo Insulation
Consist of 1 inner facesheet, 1 outer facesheet, 1 retainer, 1 blanket, 1 id plate, 26 grommet; located on yn 216.5 to yn 265.25; used on nac insulation assy
01-232-6383
Thermal Special Purpo Insulation
Consist of 12 grommet, 1 inner facesheet, 1 outer facesheet, 1 retainer, 1 blanket, 1 id plate; located on yn 216.5 to yn 265.25; used on nac insulation blanket assy
01-232-6813
Exhaust Muffler
7.380" overall length color forest green plastic polyamide surface treated
01-232-7066
Flap Wing Landing Rib
9.797" overall length 4.703" overall width 1.250" material thickness
01-232-7357
Structural Aircraft Plate
Used on acft model e-3a. opposite p/n -23; 2024-T3 clad sh per qq-a-250/5; 61.0 in. lg, 30.5 in. wd, 0.063 in. thk; finish srf-2.30
01-232-7358
Structural Aircraft Plate
Used on F-15.
01-232-7359
Structural Component Air Support
Used on f-15 acft. cap, inboard-former; fuselage station 651.060
01-232-7360
Structural Component Air Support
Used on f-15 acft. tee, splice-upper ml; fuselage station 672.680
01-232-7381
Longeron
Used on F-15. upper inboard
01-232-7382
Longeron
Used on F-15. keel-upper center, forward
01-232-7383
Aircraft Skin
01-232-7384
Aircraft Skin
Used on acft model kc-135. opposite p/n -17; clad 7075-0 sh per qq-a-287, 0 temper; heat treat T6; 90.0 in. lg, 22.0 in. wd, 0.051 in. thk; nha 5-71748
01-232-7385
Aircraft Skin
Used on acft model kc-135. opposite p/n -72; 7075-0 clad sh per qq-a-287, 0 temper; heat treat T6; 55.0 in. lg, 45.0 in. wd, 0.071 in. thk; nha 5-71748
01-232-7386
Aircraft Skin
Used on acft model kc-135. opposite p/n -71; 7075-0 sh clad per qq-a-287, 0 temper; heat treat T6; 55.0 in. lg, 45.0 in. wd, 0.071 in. thk; nha 5-71748
01-232-7776
Aircraft Floor
Used on ch-47, rotary wing aircraft.
01-232-8215
Structural Component Air Support
Used on f-15 acft. cap, inboard-former; fuselage station 651.060
01-232-8850
Aircraft Leading Edge
Used on f-18 acft.
01-232-8851
Aircraft Leading Edge
Used on f-18 acft.
01-232-8852
Wing Landing Flap
Used on aircraft model f-18.
01-232-8885
Refueling Aircraft Probe
Used on aircraft model av-8.
01-232-8994
Aircraft Fairing
Used on aircraft model f-18.
01-232-9003
Aircraft Floor
01-232-9007
Airfoil Rib
Used on acft model a-6.
01-232-9318
Access Aircraft Door
Used on acft model a-10a.
01-232-9325
Structural Aircraft Plate
01-232-9326
Structural Aircraft Plate
Used on F-15.
01-232-9327
Structural Aircraft Plate
Used on F-15.
01-232-9328
Structural Aircraft Plate
Used on F-15.
01-232-9329
Structural Aircraft Plate
Used on F-15.
01-232-9330
Structural Aircraft Plate
Used on F-15.
01-232-9339
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-headliner, fus sta 769.50 to 827.00, bl 28.50 to 66.25; c/o: -113a panel assembly (1) , nutplate (3) ; nha 4E32080
01-232-9340
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-headliner, fus sta 769.50 to 827.00, bl 3.25 to 29.50; c/o: -105a panel (1) , grill (1) ; nha 4E32080
01-232-9341
Structural Aircraft Panel
01-232-9349
Aircraft Former
01-232-9350
Aircraft Former
01-232-9351
Aircraft Former
01-232-9352
Aircraft Former
