Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-154-3369
Structural Component Air Bracket
39.000" overall length 8.600" overall width
01-154-3373
Aircraft Fairing
01-154-3384
Structural Aircraft Panel
Used on A-10.
01-154-3385
Structural Aircraft Panel
Used on A-10.
01-154-3386
Structural Aircraft Plate
1.500" overall length 0.700" overall width 0.300" material thickness used as filler tapered
01-154-3387
Structural Aircraft Plate
Used on B-52. 0.040" material thickness used as frame attachment; 17-7ph; annealed; ht tr 180, 000-200, 000 psi
01-154-3388
Structural Aircraft Plate
10.300" overall length 5.100" overall width 0.071" material thickness opp pn 35-68682-9
01-154-3389
Structural Aircraft Plate
16.100" overall length 5.100" overall width 0.063" material thickness opp pn 35-8286-11
01-154-3390
Structural Aircraft Plate
16.100" overall length 5.100" overall width 0.063" material thickness opp pn 35-8386-13
01-154-3391
Structural Aircraft Plate
6.200" overall length 3.000" overall width 0.040" material thickness
01-154-3392
Structural Aircraft Plate
6.200" overall length 2.500" overall width 0.040" material thickness
01-154-3393
Structural Aircraft Plate
3.000" overall length 0.032" material thickness
01-154-3394
Structural Aircraft Plate
3.000" overall length 0.032" material thickness
01-154-3395
Structural Aircraft Plate
19.300" overall length 1.600" overall width 0.040" material thickness
01-154-3396
Structural Aircraft Plate
6.200" overall length 5.800" overall width 0.032" material thickness
01-154-3397
Structural Aircraft Plate
5.000" overall length 1.500" overall width 0.080" material thickness
01-154-3398
Structural Aircraft Plate
6.700" overall length 3.000" overall width 0.032" material thickness
01-154-3399
Structural Aircraft Plate
6.700" overall length 3.000" overall width 0.032" material thickness
01-154-3400
Structural Aircraft Plate
6.000" overall length 3.500" overall width 0.063" material thickness
01-154-3401
Structural Aircraft Plate
6.000" overall length 3.500" overall width 0.063" material thickness
01-154-3402
Structural Aircraft Plate
6.700" overall length 2.700" overall width 0.032" material thickness
01-154-3403
Structural Aircraft Plate
6.000" overall length 3.300" overall width 0.063" material thickness
01-154-3404
Structural Aircraft Plate
6.000" overall length 3.300" overall width 0.063" material thickness
01-154-3405
Structural Aircraft Plate
7.000" overall length 3.000" overall width 0.063" material thickness
01-154-3406
Structural Aircraft Plate
6.700" overall length 2.700" overall width 0.032" material thickness
01-154-3407
Structural Aircraft Plate
6.700" overall length 2.700" overall width 0.032" material thickness
01-154-3408
Structural Aircraft Plate
6.700" overall length 2.700" overall width 0.063" material thickness
01-154-3409
Structural Aircraft Plate
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-362, T3 temper; finish f-2.130; 15.200 in. lg, 6.700 in. w, 0.045 in. thk; opposite p/n -4; located stab. buttock lines 235.73 to 245.73; nha 65-15688-1
01-154-3411
Structural Aircraft Plate
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-362, T3 temper; finish f-2.130; 13.400 in. lg, 7.900 in. w, 0.071 in. thk; opposite p/n -4; nha 65-15942-1
01-154-3412
Structural Aircraft Plate
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-362; T3 temper; finish f-2.130; 13.400 in. lg, 7.900 in. w, 0.071 in. thk; opposite p/n -3; nha 65-15942-2
01-154-3413
Structural Aircraft Plate
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-362, T3 temper; finish f-2.130; 9.700 in. lg, 8.300 in. w, 0.045 in. thk; opposite p/n -4
01-154-3414
Structural Aircraft Plate
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-362, T3 temper; finish f-2.130; 9.700 in. lg, 8.300 in. w, 0.045 in. thk; opposite p/n -3
01-154-3415
Structural Aircraft Plate
6.200" overall length 5.800" overall width 0.032" material thickness
01-154-3416
Structural Aircraft Plate
15.000" overall length 1.400" overall width 0.050" material thickness
01-154-3417
Aircraft Fairing
75.500" overall length 16.000" overall width 0.050" material thickness opposite -4
01-154-3418
Aircraft Fairing
75.500" overall length 16.000" overall width 0.050" material thickness opposite -3
01-154-3419
Structural Component Air Support
60.000" overall length 2.600" overall width 0.040" material thickness opposite to p/n 39-10757-7; annealed
01-154-3420
Structural Component Air Support
18.000" overall length 2.500" overall width 0.080" material thickness
01-154-3421
Aircraft Fairing
5.000" overall length 2.500" overall width 0.430" material thickness opp 39-7648-803
01-154-3422
Aircraft Fairing
2.900" overall length 2.500" overall width 0.080" material thickness opp 39-7648-506
01-154-3423
Aircraft Fairing
2.900" overall length 2.500" overall width 0.080" material thickness opp 39-7648-505
01-154-3424
Aircraft Fairing
11.300" overall length 2.500" overall width 0.080" material thickness opp 39-7648-802
01-154-3425
Aircraft Fairing
11.300" overall length 2.500" overall width 0.080" material thickness opp 39-7648-801
01-154-3426
Structural Component Air Support
Used on acft model c/kc-135. made from 9-66825; 4 attaching holes in. base 0.250 in. dia
01-154-3432
Movable Canopy
01-154-3434
Movable Canopy
01-154-3436
Aircraft Former
Used on B-52. extrusion; stock size AND10135-1005 by 4.000 in.
01-154-3437
Aircraft Former
9.800" overall length 4.500" overall width 0.040" material thickness
01-154-3438
Aircraft Former
Used on B-52. opp p/n 35-8642-801
01-154-3439
Aircraft Former
4.400" overall length 2.600" overall width 0.080" material thickness
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