01-276-6402
Structural Aircraft Panel
Used on acft model b-1b. located at sta YF290.000 to YF422.000
01-276-6418
Aircraft Former
Used on C-141.
01-276-6431
Airfoil Rib
Used on C-141. 7175-T74; nha 3W33002, 3W33074, 3W33075
01-276-6432
Airfoil Rib
Used on C-141.
01-276-7217
Structural Component Air Support
01-276-7218
Structural Component Air Support
Used on f-16c/d aircraft.
01-276-7219
Structural Component Air Support
Used on f-16a aircraft.
01-276-7220
Structural Component Air Support
01-276-7221
Structural Component Air Support
01-276-7227
Stiffener Aircraft Rib
01-276-7239
Structural Component Air Support
13.120" overall length 8.000" overall width
01-276-7240
Structural Component Air Support
13.120" overall length 8.000" overall width
01-276-7593
Structural Aircraft Panel
01-276-7631
Thermal Special Purpo Insulation
Arc shaped
01-276-7632
Thermal Special Purpo Insulation
Arc shaped; one end notched 1.390 in. lg by 24.0 deg w
01-276-7770
Structural Aircraft Panel
Used on f-4 aircraft. core, honeycomb; part of 1560009321674 honeycomb assy
01-276-8259
Access Aircraft Door
Used on acft model b-1b.
01-276-8262
Access Aircraft Door
Used on acft model f-15. located FS415.000 to FS780.000; used on lwr ml fairing assembly
01-276-8263
Access Aircraft Door
Used on acft model f-15. located FS415.000 to fs 780.000; used on lower ml fairing assembly
01-276-8286
Structural Aircraft Plate
Used on C-141.
01-276-8287
Structural Aircraft Plate
Used on C-141.
01-276-8288
Aircraft Fairing
C/o 3 stiffener, 4 shims, 1 strap, 2filler, 4 former, 3 skin, 1 angle; nha isp/N68A250002
01-276-8289
Aircraft Fairing
Used on F-15. 3c/o 5 supports, 1 nut assy, 1 plate, 1 filler, 1 channel, 4 stringers, 8 clips, 1 aft panel, 2 shims, 2 sills, 9 spacers, 2 airings, 1 web, 1 panel, 1 cover, 1 pad, 1 block, 11 ribs, 52 bushings, 1 nutplates, 25 gang channels
01-276-8290
Structural Component Air Support
C/o 1 fitting, 2 bushing; nha L1800075
01-276-8291
Structural Component Air Support
C/o 1 fitting, 2 bushing; nha L1800075
01-276-8292
Structural Component Air Support
C/o 1 fitting, 2 bushing; nha L1800075
01-276-8293
Structural Component Air Support
C/o 1 fitting, 2 bushing; nha L1800075
01-276-8294
Structural Component Air Support
01-276-8295
Structural Component Air Support
01-276-8296
Structural Component Air Support
Used on f-15 acft. al alloy 2024-0; includes 10 rivets 1 nutplate; support-pressure control valve, wing
01-276-8299
Structural Aircraft Panel
C/o 1 panel assy, 5 exterior surface covering, 22 seal, 53 hi-lk, 53 collar
01-276-8300
Structural Aircraft Panel
C/o 1 panel duct vane, 1 terminal block, 3 plate, 4 strap cable tie, 7 clamp, 9 splice, 9 sleeving, 2 sealing plug, safety wire, polysulfide sealant type b, chafe guard; opp -001
01-276-8301
Structural Aircraft Panel
C/o 1 panel duct vane, 1 terminal block, 3 plate, 4 strap cable tie, 7 clamp, 9 splice, 9 sleeving, 2 sealing plug, misc hardware, safety wire, polysulfide sealant, chafe guard; opp-002
01-276-8303
Retractable Aircra Step Assembly
C/o 1 core, 2 facesheet, 4 doubler, r channel, 1 retainer, 1 walkway matting, misc hardware; nha L3011701
01-276-8304
Retractable Aircra Step Assembly
C/o 1 core, 2 facesheet, 4 doubler, 4 channel, 1 retainer, 1 walkway matting, misc hardware; nha L3011701
01-276-8305
Retractable Aircra Step Assembly
C/o 4 doubler, 2 channel, 1 core, 2 facesheet, 2 channel, 1 retainer, 1 walkway matting, misc hardware; nha L3011700
01-276-8306
Wing Aircraft Spoiler
C/o 1 spoiler, 1 cam, 2 track, 4 retainer, misc hardware; nha L3054450
01-276-8312
Aircraft Skin
Used on acft model f-15. 7075-T76 al clad per qq-a-250/25, cond T6; nha 68A250277; located FS626.900 to FS761.830; 53.00 in lg, 15.50 in wd, 0.100 in thk; opposite -2012
01-276-8313
Aircraft Skin
Used on acft model f-15. 7075-T76 al clad per qq-a-250/25, cond T6; 53.00 in lg, 15.50 in wd, 0.100 in thk; located FS626.900 to fs 761.830; nha 68A250277; opposite -2011
01-276-9220
Structural Component Air Support
Fiber glass laminate, GM4001F42 grumman aerospace corp, separators; includes 6 angles, 14 cores, 2 frames, 1 channel, 4 skins, 3 closures, 5 fillers
01-276-9295
Access Aircraft Cover
Used on acft model b-1b. identical to L2500004-031 except allow 0.125 excess material around periphery of part; used on horizontal stabilizer components spares
01-276-9296
Access Aircraft Cover
Used on acft model b-1b. identical to L2500003-021 except allow 0.125 excess material around periphery of part; used on horizontal stabilizer components spares
01-276-9297
Access Aircraft Door
Used on acft model b-1b. nha L6000501; used on forward segment weapons bay door assembly
01-276-9298
Access Aircraft Door
Used on acft model b-1b. identical to L2500049-031 except add 0.125 excess material around perimeter of part
01-276-9299
Access Aircraft Door
Used on b-1b aircraft. mnuclear hardness critical item; consist of 3 honeycomb core, 1 skin, 3 closeout, 1 half hinge; nha L2501047; located at YVS262.63 to YVS300.87; used on tail warning system, horizontal stabilizer fairing door assembly
01-276-9343
Structural Aircraft Plate
17.020" overall length 9.950" overall width 9.350" material thickness T6
01-276-9344
Structural Aircraft Plate
13.250" overall length 9.300" overall width 4.300" material thickness T6
01-276-9345
Structural Aircraft Plate
17.020" overall length 4.450" overall width 4.350" material thickness T651
01-276-9346
Structural Aircraft Plate
17.020" overall length 4.450" overall width 4.350" material thickness T651
01-276-9348
Structural Aircraft Plate
Used on AC-130. T6
