01-126-0350
Structural Component Air Support
Temper T6
01-126-0351
Structural Component Air Support
Used on acft model a10. al casting 7075-T7351 per qq-a-250/12; packaged as matched set c/o support 1ea p/n 160D321041-21 8.600 in.lg, 4.000 in.w, 1.500 in.thk, and support 1ea p/n 160D321041-23 8.600 in.lg, 4.000 in.w, 2.500 in.thk, used on pitch control cable crank, fuselage station 682.80
01-126-0352
Structural Component Air Support
Used on acft model a10. al casting 7075-T7351 per qq-a-250/12; packaged as matched set c/o support 1ea p/n 160D321041-22 8.600 in.lg, 4.000 in.w, 1.500 in.thk, and support 1ea p/n 160D321041-24 8.600 in.lg, 4.000 in.w, 2.500 in.thk, used on pitch control cable crank, fuselage station 682.80
01-126-0365
Aircraft Skin
Used on acft model c135. al alloy sheet 7075-T6 per qq-a-287; 60.000 in.lg, 34.000 in.w, .051 in.thk; used on aft left hand inboard nacelle strut
01-126-0367
Aircraft Skin
Used on acft model c135. al alloy sheet 7075-T6 per qq-a-287; 96.000 in.lg, 36.000 in.w, .051 in.thk; used on aft right hand inboard nacelle strut
01-126-1804
Structural Component Air Bracket
6.000" overall length 1.500" overall width
01-126-1805
Structural Component Air Bracket
3.000" overall length 1.000" overall width
01-126-1887
Structural Component Air Support
Matl:al alloy, COMP5; 4 mtg holes 0.2495 in dia; distance from c to c holes along length 2.630in; distance from c to c holes along wd. 1/500 in; u/a: support, bearing drag link, nose gear
01-126-1888
Structural Component Air Support
Used on c-5 acft. 7.500" overall length 0.750" overall width 0.251 in. dia hole
01-126-1889
Structural Component Air Support
Used on acft model c135. al clad 2024-0 per qq-a-362, 8.800 in.lg, 3.400 in.w, .072 in.thk, used on front spar, outboard nacelle strut
01-126-1891
Structural Component Air Support
Used on acft model f111. 4.750" overall length 2.500" overall width
01-126-1892
Structural Component Air Support
Used on acft model f111. nylon per mil-p-170918, located fuselage station 359.00
01-126-1894
Structural Component Air Support
C/o 1 support, 1 nutplate
01-126-1901
Aircraft Skin
Used on acft model c135. al alloy 7075-T6 per qq-a-283, 23.000 in.lg, 18.000 in.w, .064 in.thk, used on outboard nacelle strut, aft right hand side
01-126-1902
Aircraft Skin
Used on acft model c135. al alloy 7075-T6 per qq-a-287, 88.000 in.lg, 28.000 in.w, .051 in.thk, used on outboard nacelle strut, forward right hand side
01-126-2888
Access Aircraft Cover
01-126-2890
Access Aircraft Door
01-126-3134
Aircraft Former
01-126-3135
Aircraft Former
01-126-3136
Aircraft Former
01-126-3144
Aircraft Trailing Edge
Honeycomb core (nomex) .125 in. cell x 3 pounds per cubic foot; type 120 prepregnated cloth 7075-T6 x .050 in. al alloy clad sheet; c/o spar assembly 1 ea p/n 160D612512-4, core 1 ea p/n 160D612512-17, laminate build-up 1 ea p/N160D612512-20; used on outboard trailing edge flap stations 4.712 to 83.454
01-126-4254
Access Aircraft Cover
Used on acft model e3a.
01-126-4287
Aircraft Fairing
01-126-4293
Structural Component Air Support
Used on acft model c135. used on right hand bottom cowl engine nacelle
01-126-4294
Aircraft Former
01-126-4295
Aircraft Former
01-126-4296
Aircraft Skin
Used on acft model c135. 0.040 in.thk, 1.600 in.w, 5.500 in.lg, right hand
01-126-4297
Horizontal Stabilizer
01-126-4301
Thermal Special Purpo Insulation
C/o fiberglass insulation, p/n 69-3345-4; cover, p/n 69-3345-6; grommet, p/n 69-3345-14, right hand; end item identification:aircraft, model E3a
01-126-6158
Wing Section Outer Rib
25.910" overall length 1.375" overall width finish per lac 0471
01-126-6872
Access Aircraft Cover
Gun lh access
01-126-6907
Aircraft Former
15.800" overall length
01-126-7686
Structural Component Air Support
Matl:al aly forging per AMS4149
01-126-7687
Structural Component Air Support
01-126-8268
Access Aircraft Door
01-126-8319
Structural Aircraft Plate
33.000" overall length 15.000" overall width 0.025" material thickness
01-126-8336
Structural Component Air Support
Used on acft model c-135. c/o bearing 4 ea p/n ab-6, fitting 4 ea p/n NAS516-1, ring 4 ea p/n NAS50-156, support fitting 1 ea p/n 5-73143-11, left hand, located at ws 615
01-126-8343
Aircraft Spar
128.000" overall length 7.500" overall width 0.072" material thickness
01-126-8344
Aircraft Spar
128.000" overall length 7.500" overall width 0.072" material thickness
01-126-8345
Aircraft Spar
128.000" overall length 4.700" overall width 0.064" material thickness
01-126-8346
Aircraft Spar
128.000" overall length 4.700" overall width 0.064" material thickness
01-126-8347
Aircraft Spar
128.000" overall length 5.500" overall width 0.051" material thickness
01-126-8348
Aircraft Spar
128.000" overall length 5.500" overall width 0.051" material thickness
01-126-8349
Aircraft Spar
01-126-8350
Aircraft Spar
01-126-9457
Structural Aircraft Panel
Used on uh-60a helicopter. aluminum alloy, qq-a-250-18
01-126-9584
Structural Aircraft Plate
01-126-9585
Structural Aircraft Plate
01-126-9586
Fuselage Aircraft Fairing
Used on uh-60a helicopter. c/o component quantity, 27;
01-126-9587
Fuselage Aircraft Fairing
