Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-152-1397
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.040" material thickness
01-152-1398
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.040" material thickness
01-152-1399
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.020" material thickness
01-152-1400
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.020" material thickness
01-152-1401
Aircraft Tip
Used on B-52. c/o panel assy, lh side p/n 25-2382-503, panel assy, rh side p/n 25-2382-505
01-152-1402
Aircraft Tip
Used on B-52. c/o panel assy, lh side p/n 25-2382-504, panel assy, rh side p/n 25-2382-506
01-152-1405
Structural Aircraft Panel
Used on B-52. c/o core 25-2382-19, inner skin 25-2382-801, outer skin 25-2382-23, doubler 25-2382-25, stiffener 25-2382-27, retainer 25-2382-29
01-152-1407
Structural Aircraft Panel
Used on B-52. opposite p/n 25-2779-6
01-152-1408
Aircraft Tip
Used on B-52. opp pn 25-2779-502
01-152-1409
Structural Aircraft Panel
Used on B-52. opposite p/n 25-2779-504
01-152-1410
Structural Aircraft Panel
Used on B-52. opposite p/n 25-2779-503
01-152-1411
Structural Aircraft Plate
8.000" overall length 1.700" overall width 0.125" material thickness matl: clad; T3 temper
01-152-1412
Structural Component Air Bracket
1.300" overall length clip manufacturer suggested name: clip; make from BAC1505-100156; T4 temper
01-152-1413
Structural Aircraft Plate
1.300" overall length manufacturer suggested name:clip; matl; make from bac 1505-100156, T4 temper
01-152-1414
Aircraft Frame
8.000" overall length 2.000" overall width 0.050" material thickness matl: clad sht; 0 temper; ht T4; opp -832
01-152-1415
Aircraft Frame
8.000" overall length 2.000" overall width 0.050" material thickness matl: cl sht; 0 temper; opp -831
01-152-1416
Aircraft Stringer
7.500" overall length 2.000" overall width 0.050" material thickness matl: clad sht; 0 temper; opp -838
01-152-1417
Aircraft Stringer
01-152-1418
Aircraft Stringer
Opposite p/n 35-10704-511
01-152-1419
Aircraft Stringer
39.000" overall length 2.8000" overall width 0.040" material thickness
01-152-1420
Aircraft Stringer
Opposite p/n 35-10704-513
01-152-1421
Aircraft Stringer
39.000" overall length 2.800" overall width 0.040" material thickness
01-152-1422
Aircraft Stringer
Opposite p/n 35-10704-515
01-152-1423
Aircraft Stringer
39.000" overall length 2.800" overall width 0.040" material thickness
01-152-1424
Aircraft Stringer
Opposite p/n 35-10704-517
01-152-1425
Aircraft Stringer
39.000" overall length 2.800" overall width 0.040" material thickness
01-152-1426
Aircraft Former
11.200" overall length 7.200" overall width 0.040" material thickness
01-152-1427
Aircraft Former
11.200" overall length 7.200" overall width 0.040" material thickness opposite 35-10727-25
01-152-1428
Aircraft Former
2.800" overall length 1.900" overall width 0.050" material thickness
01-152-1429
Aircraft Former
2.800" overall length 1.900" overall width 0.050" material thickness opp 35-10727-27
01-152-1430
Structural Component Air Support
3.830" overall length 1.070" overall width 4340 per mil-s-5000; opp -2
01-152-1431
Structural Component Air Support
3.830" overall length 1.070" overall width 4340 per mil-S5000
01-152-1432
Aircraft Former
Used on b-52 acft. c/o 11 shear angles
01-152-1433
Aircraft Former
Used on b-52 acft.
01-152-1434
Structural Aircraft Plate
54.800" overall length 0.600" overall width 0.032" material thickness
01-152-1435
Cowling
Used on B-52.
01-152-1436
Cowling
Used on B-52.
01-152-1437
Structural Aircraft Plate
1.200" overall length
01-152-1438
Structural Aircraft Plate
1.200" overall length
01-152-1439
Aircraft Former
01-152-1440
Structural Aircraft Plate
2.000" overall length 7021
01-152-1441
Aircraft Fairing
18.500" overall length 2.000" overall width 0.080" material thickness
01-152-1442
Aircraft Fairing
01-152-1443
Aircraft Fairing
6.000" overall length 2.000" overall width 0.080" material thickness
01-152-1444
Structural Aircraft Plate
0.700" overall length 0.500" overall width 0.080" material thickness used as filler
01-152-1445
Structural Aircraft Plate
0.700" overall length 0.600" overall width 0.040" material thickness used as filler
01-152-1446
Aircraft Former
8.200" overall length 2.000" overall width 0.063" material thickness
01-152-1447
Structural Aircraft Plate
14.000" overall length 1.500" overall width 0.040" material thickness used as filler
01-152-1448
Structural Aircraft Plate
1.500" overall length 1.400" overall width 0.080" material thickness
01-152-1449
Aircraft Former
Used on B-52.
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