01-273-2367
Structural Component Air Support
01-273-2467
Structural Component Air Support
01-273-2495
Landing Gear Aircraft Fairing
01-273-2496
Landing Gear Aircraft Fairing
01-273-2838
Thermal Insulation Pipe Covering
01-273-2858
Aircraft Skin
Used on acft,model av8.
01-273-2859
Aircraft Skin
Used on acft,model av8.
01-273-3075
Aircraft Stiffener
8.100" overall length 0.650" overall width 0.040" material thickness
01-273-3082
Aircraft Former
11.000" overall length 3.000" overall width 0.071" material thickness ht tr T6; nha 3P21601 & 3P21602
01-273-3083
Aircraft Skin
Used on acft model b-52. 46.0 in lg, 26.0 in wd, 0.025 in thk; opposite -815
01-273-3145
Radome
Located sta 116.74 to sta 149.38; phase vi ecm radome assembly kit; acft model b-52
01-273-3146
Radome
Located sta 116.74 to sta 149.38; used on phase vi ecm radome assembly kit; acft model b-52
01-273-4299
Access Aircraft Cover
Used on f-16c/d. engine rh lower access
01-273-4300
Access Aircraft Cover
Engine, lh lwr access FS389.80 TO446.10
01-273-4303
Access Aircraft Door
Used on acft model kc-135. c/o of 1 door, 1 doubler, 1 retainer, 10 anchor block, 10 shim plate, 10 latch nut, 1 press relief door, 10 screws, 1 door retaining stud, 10 indicator; used on pressure relief access door assembly
01-273-4304
Access Aircraft Door
Used on acft model kc-135. c/o of 1 door, 1 doubler, 1 retainer, 10 anchor block, 10 shim plate, 10 latch nut, 1 press relief door, 8 screw, 1 door retaining stud, 1 indicator; used on pressure relief access door assembly
01-273-4315
Structural Aircraft Plate
Used on acft model kc-135. 7075-0 sheet per qq-a-250/12; heat treat T6; finish f-2.133
01-273-4317
Structural Aircraft Plate
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish SRF2.30; 7.50 in lg, 3.00 in wd, 0.071 in thk; nha 65-2516
01-273-4319
Structural Component Air Support
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish srf-2.30; 77.9 in lg, 5.50 in wd, 0.160 in thk; nha 65-2516
01-273-4321
Structural Component Air Support
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish srf-2.30; 77.9 in lg, 5.50 in wd, 0.160 in thk; nha 65-2516; opposite -31
01-273-4322
Structural Component Air Support
Used on acft model kc-135. steel sheet annealed 4130 per an-qq-s-685 or 8630 an-s-12; heat treat 150, 000-170, 000 psi; finish f-1.20; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516
01-273-4323
Structural Component Air Support
Used on acft model kc-135. steel sheet annealed 4130 per an-qq-s-685 or 8630 an-s-12; heat treat 150, 000-170, 000 psi; finish f-1.20; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516
01-273-4324
Structural Component Air Support
Used on acft model kc-135. steel sheet annealed 4130 per an-qq-s-685 or 8630 an-s-12; finish f-1.20; heat treat 150, 000-170, 000 psi; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516
01-273-4325
Structural Component Air Support
Used on kc-135 aircraft. size .112X19X21; part of bulkhead instl-fwd engine mount, inboard nac STA136
01-273-4326
Structural Component Air Support
Used on kc-135 aircraft. matl 7075-0 extrusion per qq-a-277; part of closure rib installation-inbd nacelle strut
01-273-4327
Structural Component Air Support
Used on kc-135 aircraft. matl 7075-0 extrusion per qq-a-277; part of closure rib installation-inbd nacelle strut
01-273-4328
Structural Component Air Support
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish srf-2.30; 77.9 in lg, 5.50 in wd, 0.160 in thk; opposite -30; nha 65-2516
01-273-4329
Aircraft Strut
01-273-4330
Structural Component Air Support
01-273-4331
Structural Component Air Support
01-273-4333
Structural Component Air Support
Used on kc-135 aircraft. matl 7075-0 extrusion per qq-a-277; part of closure rib installation-inbd nacelle strut
01-273-4335
Structural Component Air Support
Used on acft model kc-135. clad 2024-0 sht per qq-a-250/5, 0 temper; heat treat T4; finish F2.130; 20.0 in lg, 9.0 in wd, 0.040 in thk; nha 5-86024; located sta 1640-1676
01-273-4347
Aircraft Former
38.200" overall length 2.000" overall width 0.032" material thickness opposite -3006; finish f-8.05; nha 65-2516
01-273-4348
Aircraft Former
38.200" overall length 2.000" overall width 0.032" material thickness finish f-8.05; opposite -3005; nha 65-2516
01-273-4349
Aircraft Former
46.800" overall length 2.000" overall width 0.052" material thickness opposite -3018; nha 65-2516
01-273-4350
Aircraft Former
46.800" overall length 2.000" overall width 0.052" material thickness finish f-8.05; opposite -3017; nha 65-2516
01-273-4351
Aircraft Former
38.200" overall length 2.000" overall width 0.032" material thickness finish f-8.05; opposite -3134; nha 65-2516
01-273-4352
Aircraft Former
38.200" overall length 2.000" overall width 0.032" material thickness finish f-8.05; opposite -3133; nha 65-2516
01-273-4663
Structural Aircraft Plate
Used on acft model f-14a. 0.040" material thickness
01-273-4664
Structural Component Air Support
01-273-4669
Aircraft Skin
Used on acft model f-14a. aluminum alloy, mil-a-8920, alloy 2219-T81; 0.125 in. thk
01-273-4892
Aircraft Thrust Reverser
01-273-6343
Access Aircraft Door
Used on a-7 aircraft.
01-273-6382
Aircraft Fairing
0.980" overall width
01-273-6383
Structural Component Air Support
01-273-6513
Structural Aircraft Plate
Used on acft kc-135. 7075-T6 sh per qq-a-283, T6 temp; finish srf 2.30; 36.90 in lg, 14.6 in wd, 0.063 in thk; nha 65-2494
01-273-6514
Structural Aircraft Plate
11.000" overall length 9.000" overall width 0.060" material thickness
01-273-6517
Structural Component Air Support
01-273-6528
Aircraft Former
