01-236-8392
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 cond c annealed; p/o sidewall closure, engine fairing
01-236-8393
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 cond c annealed; p/o sidewall closure, engine fairing
01-236-8394
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure; engine fairing
01-236-8396
Structural Component Air Support
Opposite -105; nha 3W00037
01-236-8420
Aircraft Skin
Used on F-15.
01-236-9408
Structural Aircraft Plate
Used on KC-135. 78.300" overall length 0.093" material thickness nha 8627733-10
01-236-9409
Structural Aircraft Plate
Used on acft model kc-135. 2024-0 clad sh spec per qq-a-250/5, 0 temper; heat treat T4; finish f-2.115; 7.6 in. lg, 5.0 in. wd, 0.032 in. thk; nha 5-88190; opposite -21
01-236-9410
Structural Aircraft Plate
Used on F-15. web
01-236-9411
Structural Aircraft Plate
Used on F-15. web
01-236-9412
Structural Aircraft Plate
Used on F-15. web
01-236-9413
Structural Aircraft Plate
Used on F-15.
01-236-9414
Structural Aircraft Plate
Used on F-15.
01-236-9415
Structural Aircraft Plate
Used on F-15.
01-236-9416
Structural Aircraft Plate
Used on F-15.
01-236-9417
Structural Aircraft Plate
Used on F-15.
01-236-9418
Structural Aircraft Plate
Used on F-15.
01-236-9419
Structural Aircraft Plate
Used on F-15.
01-236-9420
Aircraft Fairing
17.000" overall length 7.000" overall width 0.040" material thickness
01-236-9421
Aircraft Fairing
17.000" overall length 7.000" overall width 0.040" material thickness
01-236-9423
Structural Component Air Support
Used on acft model a-7d.
01-236-9424
Structural Component Air Support
Used on acft model kc-135. consist of 1 fitting, 1 lub fitting, 1 bearing; opposite -2; nha 5-83876; located on sta 960
01-236-9425
Structural Component Air Support
Used on acft model e-3a.
01-236-9426
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-9427
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-9428
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-9429
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/osidewall closure, engine
01-236-9430
Structural Component Air Support
Used on f-15 acft. p/o former empennage support beam, fuselage station 721.830
01-236-9431
Structural Component Air Support
Used on f-15 acft. p/o former empennage support beam, fuselage station 721.830
01-236-9432
Structural Component Air Support
Used on f-15 acft. p/o former empennage support beam, fuselage station 721.830
01-236-9433
Structural Component Air Support
Used on f-15 acft. p/o former empennage support beam, fuselage station 721.830
01-236-9434
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-236-9435
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-236-9436
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-236-9439
Structural Aircraft Panel
Used on acft model kc-135. 7075-0 clad sh per qq-a-287, 0 temper; heat treat T6; finish f-2.115; 21.0 in lg, 11.2 in wd, 0.040 in thk; opp -8; nha 5-73119; located on bl 779.18
01-236-9440
Structural Aircraft Panel
P/o former empennage support beam
01-236-9455
Aircraft Former
Opposite p/n -12
01-236-9456
Aircraft Former
01-237-0015
Remote Control Lever
01-237-0041
Aircraft Floor
Used on ch-47d aircraft.
01-237-0295
Structural Aircraft Plate
Used on F-15. 15.110" overall length 8.030" overall width 0.045" material thickness
01-237-0298
Structural Aircraft Plate
Used on F-15.
01-237-0299
Structural Aircraft Plate
Used on F-15.
01-237-0301
Structural Component Air Support
Used on f-15 aircraft. matl 6al-4v per mil-t-9046, type 3, comp c anl; size .045X1.46X2.20; opposite -2288; used -1031 shear beam-inboard fs 626.900-fs 712.310
01-237-0302
Structural Component Air Support
Used on f-15 aircraft. matl 6al-4v per mil-t-9046, type 3, comp c anl; size .045X1.46X2.20; opposite -2287; used on -1032 shear beam-inboard fs 626.900-fs 712.310
01-237-0303
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-237-0304
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-237-0306
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-237-0307
Structural Component Air Support
Used on f-15 acft. p/o shear beam-inboard, fuselage station 626.900 to 712.310
01-237-0349
Aircraft Skin
Used on F-15.
