Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-152-2171
Aircraft Skin
Used on B-52. 12.400" overall length 1.400" overall width
01-152-2172
Aircraft Skin
Used on B-52. 12.000" overall length 1.400" overall width
01-152-2173
Aircraft Skin
Used on B-52. 11.400" overall length 1.400" overall width
01-152-2174
Aircraft Skin
Used on B-52. 10.800" overall length 1.400" overall width
01-152-2175
Aircraft Skin
Used on B-52. 22.000" overall length 7.000" overall width finiish f 2.30., ht tr to T4
01-152-2314
Thermal Special Purpo Insulation
01-152-3896
Structural Component Air Bracket
01-152-3897
Structural Component Air Support
01-152-3899
Aircraft Pylon
Used on f-16 egypt wing weapon pylon. egypt only; nha-16S500-883; eff on-97 0001 9999; location-bl 71.00
01-152-4334
Structural Component Air Bracket
Used on sentry f22 aircraft. bracket ay
01-152-4344
Structural Component Air Support
Used on f-4 aircraft. used on structural assembly 10-14 degree engine air duct
01-152-4370
Structural Aircraft Panel
Used on B-52. 72.000" overall length 14.000" overall width al honeycomb perforated, foil
01-152-4371
Aircraft Stringer
Opposite p/n 35-10704-519
01-152-4372
Aircraft Stringer
39.000" overall length 2.800" overall width 0.040" material thickness
01-152-4373
Aircraft Stringer
Opposite p/n 35-10704-523
01-152-4374
Aircraft Stringer
39.000" overall length 2.800" overall width 0.040" material thickness
01-152-4375
Aircraft Stringer
Opposite p/n 35-10704-515
01-152-4377
Structural Aircraft Panel
Used on B-52. item is opposite p/n 25-2372-80 7
01-152-4378
Structural Aircraft Panel
Used on B-52. 72.000" overall length 14.000" overall width al honeycomb, foil; opposite p/n 25-2779-18
01-152-4379
Structural Aircraft Panel
Used on B-52. 72.000" overall length 14.000" overall width al honeycomb, foil; opposite p/n 25-1779-17
01-152-4380
Structural Aircraft Panel
Used on B-52.
01-152-4381
Structural Aircraft Panel
Used on B-52. c/o door assy 1 ea, bearing angle 2 ea, retainer spring 1 ea, spring torsion 1 ea, shim 1 ea
01-152-4382
Aircraft Former
21.300" overall length 4.400" overall width 0.050" material thickness
01-152-4383
Structural Aircraft Plate
4.100" overall length 1.100" overall width 0.063" material thickness
01-152-4384
Aircraft Former
64.000" overall length opposite 35-8231-810
01-152-4385
Aircraft Former
64.000" overall length opposite 35-8231-809
01-152-4386
Aircraft Former
64.000" overall length opposite 35-8231-812
01-152-4387
Aircraft Former
64.000" overall length opposite 35-8231-811
01-152-4388
Structural Aircraft Plate
4.100" overall length 1.100" overall width 0.063" material thickness
01-152-4391
Aircraft Former
Used on acft model b-52. opposite -2007
01-152-4392
Aircraft Former
Used on acft model b-52. frame assembly opposite -2010
01-152-4409
Structural Aircraft Plate
89.000" overall length 17.500" overall width 0.020" material thickness opp pn 25-2779-12
01-152-4410
Structural Aircraft Plate
89.000" overall length 17.500" overall width 0.020" material thickness opp pn 27-2779-11
01-152-4411
Structural Aircraft Plate
89.500" overall length 18.000" overall width 0.020" material thickness opp pn 25-1779-14
01-152-4412
Structural Aircraft Plate
89.500" overall length 18.000" overall width 0.020" material thickness opp pn 25-2779-13
01-152-4413
Structural Aircraft Plate
17.500" overall length 3.750" overall width 0.080" material thickness
01-152-4414
Structural Aircraft Plate
15.500" overall length 3.350" overall width 0.080" material thickness
01-152-4415
Structural Aircraft Plate
15.500" overall length 3.350" overall width 0.080" material thickness
01-152-4416
Structural Aircraft Plate
17.500" overall length 3.650" overall width 0.080" material thickness
01-152-4417
Structural Aircraft Plate
17.500" overall length 3.650" overall width 0.080" material thickness
01-152-4418
Structural Aircraft Plate
12.000" overall length 12.000" overall width 0.050" material thickness
01-152-4419
Structural Aircraft Plate
2.000" overall length 1.500" overall width 0.020" material thickness finish f-8.05; opposite pn -180
01-152-4420
Structural Aircraft Plate
4.100" overall length 3.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -182
01-152-4421
Structural Aircraft Plate
4.100" overall length 3.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; oppossite pn -181
01-152-4422
Structural Aircraft Plate
9.000" overall length 2.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05
01-152-4424
Structural Aircraft Plate
6.200" overall length 2.000" overall width 0.040" material thickness
01-152-4425
Structural Aircraft Plate
6.000" overall length 2.000" overall width 0.040" material thickness
01-152-4426
Structural Aircraft Plate
8.000" overall length 4.200" overall width 0.020" material thickness doubler, fininsh f-10.10
01-152-4427
Structural Aircraft Plate
8.000" overall length 4.200" overall width 0.020" material thickness doulber; finish f-10.10
01-152-4428
Structural Component Air Support
5.600" overall length 1.500" overall width 0.040" material thickness used as intercostal aft, on panel-engine wrap cowl, lower
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