01-155-5660
Aircraft Former
7.700" overall length 1.300" overall width 0.050" material thickness
01-155-5661
Aircraft Former
7.100" overall length 1.300" overall width 0.020" material thickness function-angle
01-155-5662
Aircraft Former
10.200" overall length 2.800" overall width 0.040" material thickness function-angle
01-155-5663
Aircraft Former
4.200" overall length 2.400" overall width 0.040" material thickness function-angle
01-155-5664
Aircraft Former
4.200" overall length 2.400" overall width 0.040" material thickness function-angle
01-155-5667
Aircraft Former
10.200" overall length 2.800" overall width 0.050" material thickness function-frame
01-155-5668
Aircraft Former
10.200" overall length 2.800" overall width 0.050" material thickness function frame
01-155-5669
Aircraft Former
Used on B-52. 11.000" overall length 5.000" overall width 0.050" material thickness c/o web, p/n 3P61516-101; plate; pin, 17; collar, 17; miscellaneous hardwares
01-155-5670
Aircraft Skin
32.000" overall length 28.000" overall width eff 5c 0001 9999, ecn 2C152, nha 16B1931-809
01-155-5671
Aircraft Skin
23.000" overall length 13.000" overall width eff 5c 0001 9999, ecn 2C152, nha 16B1931-809
01-155-5672
Aircraft Stringer
17.000" overall length 3.000" overall width 0.032" material thickness used as stringer
01-155-5673
Aircraft Stringer
13.800" overall length 3.000" overall width 0.032" material thickness used as stringer
01-155-5728
Fuel Aircraft Tank
Aluminum alloy per qq-a-250/11 comp 6061-T6; 190.489 in. o/a lg
01-155-6036
Bell Crank
0.7488" bore diameter
01-155-6037
Access Aircraft Door
01-155-6038
Access Aircraft Door
01-155-6283
Access Aircraft Cover
0.221" hole diameter
01-155-6284
Access Aircraft Door
01-155-6307
Structural Component Aircraf Web
23.100" overall length 17.600" overall width 0.040" material thickness
01-155-6308
Structural Component Air Bracket
3.000" overall length 1.400" overall width
01-155-6317
Structural Component Aircraf Web
01-155-6318
Structural Component Aircraf Web
01-155-6319
Structural Component Aircraf Web
Opposite 39-9916-507
01-155-6320
Structural Component Air Bracket
01-155-6321
Aircraft Frame
Opposite 35-8227-857
01-155-6347
Structural Aircraft Panel
Used on B-52. 11.000" overall length 6.200" overall width do not use cadmium plated tools on this item
01-155-6348
Structural Aircraft Plate
Used on B-52. make from sht 7.0 in. x 3.3 in. X0.032 in.
01-155-6349
Structural Aircraft Plate
3.800" overall length 2.800" overall width 0.071" material thickness
01-155-6350
Structural Aircraft Plate
6.000" overall length 3.200" overall width 0.050" material thickness used as doubler
01-155-6351
Structural Aircraft Plate
4.300" overall length 3.200" overall width 0.050" material thickness used as doubler
01-155-6352
Structural Aircraft Plate
2.500" overall length 1.600" overall width 0.050" material thickness used as filler
01-155-6353
Structural Aircraft Plate
5.600" overall length 4.600" overall width 0.071" material thickness used as doubler
01-155-6354
Structural Aircraft Plate
5.200" overall length 3.200" overall width 0.050" material thickness
01-155-6355
Structural Aircraft Plate
2.000" overall length 1.400" overall width 0.040" material thickness
01-155-6356
Structural Aircraft Plate
2.100" overall length 1.400" overall width 0.040" material thickness
01-155-6359
Structural Aircraft Plate
1.500" overall length 1.300" overall width 0.040" material thickness
01-155-6362
Structural Aircraft Plate
2.100" overall length 1.200" overall width 0.040" material thickness
01-155-6364
Structural Aircraft Plate
Used on B-52. 23.400" overall length 1.900" overall width 0.020" material thickness do not use cadmium plated tools on this item
01-155-6365
Structural Aircraft Plate
23.500" overall length 1.900" overall width 0.020" material thickness do not use cadmium plated tools on this item
01-155-6366
Structural Aircraft Plate
23.600" overall length 2.000" overall width 0.020" material thickness do not use cadmium plated tools on this item
01-155-6367
Structural Aircraft Plate
23.500" overall length 2.100" overall width 0.020" material thickness do not use cadmium plated tools on this item
01-155-6368
Structural Aircraft Plate
23.500" overall length 2.100" overall width 0.020" material thickness
01-155-6369
Structural Aircraft Plate
23.600" overall length 2.300" overall width 0.020" material thickness
01-155-6370
Structural Aircraft Plate
5.600" overall length 1.200" overall width 0.020" material thickness
01-155-6371
Structural Aircraft Plate
23.600" overall length 2.300" overall width 0.020" material thickness
01-155-6372
Structural Aircraft Plate
2.500" overall length 1.400" overall width 0.100" material thickness
01-155-6373
Structural Aircraft Plate
12.300" overall length 3.300" overall width 0.020" material thickness used as splice doubler
01-155-6389
Aircraft Former
4.200" overall length 2.700" overall width 0.040" material thickness do not use cadmium plated tools on this item; use of titanium, mil-t-9046 class 7 optional for firewall webs only
01-155-6390
Aircraft Former
4.200" overall length 2.700" overall width 0.040" material thickness do not use cadmium plated tools on this item, use of titanium, mil-t-9046 class 7 optional for firewall webs only
01-155-6391
Aircraft Former
6.000" overall length 2.000" overall width 0.032" material thickness do not use cadmium plated tools on this item
