Airframe Structural Components FSG 15 — FSC 1560

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NSN
NIIN
Name
Details
1560-01-151-8435
01-151-8435
Structural Aircraft Plate
6.500" overall length 6.300" overall width 0.100" material thickness
1560-01-151-8436
01-151-8436
Structural Aircraft Plate
Used on B-52. used as shim solid
1560-01-151-8437
01-151-8437
Structural Aircraft Plate
Used on B-52. used as splice plate
1560-01-151-8438
01-151-8438
Structural Aircraft Plate
Used on B-52. used as shim laminated
1560-01-151-8439
01-151-8439
Structural Aircraft Plate
Used on B-52. used as spacer
1560-01-151-8440
01-151-8440
Structural Aircraft Plate
Used on B-52. used as zee entrusion, aft cowl
1560-01-151-8441
01-151-8441
Structural Aircraft Plate
Used on B-52. used as web, fwd firewall instl
1560-01-151-8442
01-151-8442
Structural Aircraft Plate
Used on B-52. used as web, fwd firewall instl; opposite pn 35-8226-180
1560-01-151-8443
01-151-8443
Structural Aircraft Plate
20.900" overall length 1.600" overall width 0.050" material thickness
1560-01-151-8444
01-151-8444
Structural Component Air Bracket
1560-01-151-8445
01-151-8445
Structural Component Air Bracket
1560-01-151-8446
01-151-8446
Structural Aircraft Plate
30.000" overall length 1.500" overall width 0.063" material thickness ht tr 180, 000-200, 000 psi, finish f-8.05
1560-01-151-8447
01-151-8447
Structural Aircraft Plate
Used on B-52. opp pn 35-10720-137
1560-01-151-8448
01-151-8448
Structural Aircraft Plate
Used on B-52. opp pn 35-10720-82
1560-01-151-8449
01-151-8449
Structural Aircraft Plate
Used on B-52. opposite pn 35-102720-81
1560-01-151-8450
01-151-8450
Structural Aircraft Plate
Used on B-52.
1560-01-151-8451
01-151-8451
Structural Component Air Bracket
1560-01-151-8452
01-151-8452
Structural Component Air Bracket
1560-01-151-8453
01-151-8453
Structural Aircraft Plate
16.000" overall length 3.500" overall width 0.040" material thickness finish f-8.05; opposite pn -112
1560-01-151-8454
01-151-8454
Structural Aircraft Plate
5.000" overall length 3.500" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05
1560-01-151-8455
01-151-8455
Structural Aircraft Plate
42.000" overall length 4.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -120
1560-01-151-8456
01-151-8456
Structural Aircraft Plate
42.000" overall length 4.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -119
1560-01-151-8457
01-151-8457
Structural Aircraft Plate
48.000" overall length 3.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -122
1560-01-151-8458
01-151-8458
Structural Aircraft Plate
8.700" overall length 6.700" overall width 0.080" material thickness
1560-01-151-8460
01-151-8460
Structural Component Air Support
6.400" overall length 3.300" overall width 0.025" material thickness
1560-01-151-8461
01-151-8461
Structural Component Air Support
1560-01-151-8462
01-151-8462
Structural Component Air Support
7.600" overall length 4.500" overall width 0.063" material thickness opp 35-10720-140; used as bracket, support inst
1560-01-151-8463
01-151-8463
Structural Component Air Support
7.600" overall length 4.500" overall width 0.063" material thickness opp 35-10720-139; used as bracket, support instl
1560-01-151-8464
01-151-8464
Structural Component Air Support
Matl st 4340 ams 6359 annealed
1560-01-151-8465
01-151-8465
Structural Component Air Support
1.800" overall length 1.700" overall width 0.040" material thickness steel 17-7ph per mil-s-25043, cond 2d, heat treat 180000-200000 psi; finish f-8.05
1560-01-151-8466
01-151-8466
Structural Component Air Support
3.200" overall length 2.600" overall width 0.050" material thickness bracket-transducer torque bulkhead
1560-01-151-8467
01-151-8467
Structural Component Air Support
3.200" overall length 2.600" overall width 0.050" material thickness bracket-transducer torque bulkhead
1560-01-151-8468
01-151-8468
Structural Component Air Support
2.000" overall length 2.000" overall width 0.700" material thickness
1560-01-151-8469
01-151-8469
Structural Component Air Support
5.300" overall length 3.100" overall width 0.040" material thickness used on temperature regulator, inboard strut
1560-01-151-8470
01-151-8470
Structural Component Air Support
5.300" overall length 3.100" overall width 0.040" material thickness used on temperature regulator, inboard strut
1560-01-151-8471
01-151-8471
Structural Component Air Support
Used on acft model b-52. made from steel bar forging per mil-s-5626 annealed
1560-01-151-8477
01-151-8477
Aircraft Former
3.200" overall length 2.200" overall width 0.040" material thickness
1560-01-151-8478
01-151-8478
Aircraft Former
18.500" overall length 3.300" overall width 0.063" material thickness
1560-01-151-8479
01-151-8479
Aircraft Former
12.600" overall length 3.400" overall width 0.032" material thickness
1560-01-151-8480
01-151-8480
Aircraft Former
Used on b-52 aircraft. used as web
1560-01-151-8481
01-151-8481
Aircraft Former
Used on b-52 aircraft. used as stiffener
1560-01-151-8482
01-151-8482
Aircraft Former
Used on b-52 aircraft. used as stiffener
1560-01-151-8483
01-151-8483
Aircraft Former
Used on b-52 aircraft. used as stiffener
1560-01-151-8484
01-151-8484
Aircraft Former
Used on b-52 aircraft. used as stiffener
1560-01-151-8485
01-151-8485
Aircraft Former
Used on b-52 aircraft. used as stiffener
1560-01-151-8486
01-151-8486
Aircraft Former
Used on b-52 aircraft. used as stiffener
1560-01-151-8487
01-151-8487
Aircraft Former
Used on b-52 aircraft. used as web
1560-01-151-8488
01-151-8488
Aircraft Former
Used on b-52 aircraft. used as web
1560-01-151-8489
01-151-8489
Aircraft Former
Used on b-52 acft.
1560-01-151-8490
01-151-8490
Aircraft Former
Used on b-52 acft.
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