Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-154-3440
Aircraft Former
4.400" overall length 2.600" overall width 0.080" material thickness
01-154-3441
Aircraft Former
4.400" overall length 2.600" overall width 0.080" material thickness
01-154-3442
Aircraft Former
4.400" overall length 2.600" overall width 0.080" material thickness
01-154-3443
Aircraft Former
4.400" overall length 2.600" overall width 0.080" material thickness
01-154-3444
Aircraft Former
4.400" overall length 2.600" overall width 0.080" material thickness
01-154-3445
Aircraft Former
Used on B-52. bac 1490-39 by 8.000
01-154-3446
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi; opposite pn 39-14686-19
01-154-3447
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3448
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi; opposite pn 39-14686-21
01-154-3451
Aircraft Former
Used on B-52. 0.040 17-7ph, heat treated 180, 000-200, 000 psi; opp 39-14686-25
01-154-3452
Aircraft Former
4.500" overall length 1.700" overall width 0.080" material thickness
01-154-3453
Aircraft Former
4.300" overall length 2.300" overall width 0.080" material thickness
01-154-3454
Aircraft Former
2.000" overall length 1.000" overall width 0.040" material thickness
01-154-3455
Aircraft Former
14.000" overall length 1.500" overall width 0.020" material thickness
01-154-3456
Aircraft Former
Used on B-52. 0.040 17-7ph; annealed; heat treated 180, 000 to 200, 000 psi; opposite pn 39-14686-9
01-154-3457
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3458
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi; opposite pn 39-14686-11
01-154-3459
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3460
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi; opposite pn 39-14686-13
01-154-3461
Aircraft Former
Used on B-52. 0.063 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3463
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi; opposite pn 39-14686-27
01-154-3464
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3465
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3466
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi, opposite pn 39-14686-29
01-154-3467
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-3468
Aircraft Former
Used on B-52. 0.040 17-7ph, annealed, ht tr 180000 -200, 000 psi; opp 39-14686-31
01-154-3469
Aircraft Former
12.400" overall length 6.200" overall width 0.025" material thickness function-stiffener
01-154-3470
Aircraft Former
7.900" overall length 0.900" overall width 0.025" material thickness function-stiffenr
01-154-3471
Aircraft Former
7.900" overall length 0.900" overall width 0.025" material thickness function-stiffener
01-154-3472
Aircraft Former
6.700" overall length 0.900" overall width 0.025" material thickness function-stiffener
01-154-3473
Aircraft Former
6.900" overall length 1.000" overall width 0.025" material thickness function-stiffener
01-154-3474
Aircraft Former
12.400" overall length 0.800" overall width 0.025" material thickness function stiffener
01-154-3475
Aircraft Former
Channel
01-154-3477
Airfoil Rib
01-154-3478
Airfoil Rib
01-154-3479
Airfoil Rib
6.700" overall length 3.200" overall width 0.050" material thickness used on owcs 60.10
01-154-3482
Aircraft Skin
Used on B-52. make from p/n 35-8221-93
01-154-3483
Aircraft Skin
Used on B-52. make from p/n 35-8221-93
01-154-3484
Aircraft Skin
Used on B-52. make from p/n 35-8221-812
01-154-3485
Aircraft Skin
Used on B-52. make from p/n 35-8221-812
01-154-3498
Aircraft Window Panel
01-154-3499
Aircraft Window Panel
01-154-3636
Airframe Modification Kit
Used on ah-1 series helicopters.
01-154-4084
Structural Aircraft Plate
Used on B-52.
01-154-4091
Aircraft Former
58.000" overall length 3.200" overall width 0.040" material thickness opposite pn -2025; heat treated 180, 000-200, 000 psi
01-154-4092
Aircraft Former
58.000" overall length 5.500" overall width 0.050" material thickness opp -2027; ht tr 180-200, 000 psi
01-154-4097
Aircraft Skin
Used on B-52.
01-154-4780
Fuel Aircraft Tank
Used on acft model f-18.
01-154-4868
Vertical Stabilizer
53.480" overall length ventral fin assembly
01-154-4872
Access Aircraft Cover
Used on b-52 acft. 7.000 in lg, 6.000 in wd, 0.032 in thk
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