01-152-4429
Structural Component Air Support
89.000" overall length 17.500" overall width 0.020" material thickness opp 25-2779-20; used as retainer on tip assembly, fairing
01-152-4430
Structural Component Air Support
89.000" overall length 17.500" overall width 0.020" material thickness opp 25-2779-19; used as retainer on tip assembly, fairing
01-152-4431
Structural Component Air Support
89.500" overall length 18.000" overall width 0.020" material thickness opp 25-2779-22; used as retainer-outboard on tip assembly, fairing
01-152-4432
Structural Component Air Support
89.500" overall length 18.000" overall width 0.020" material thickness opp 25-2779-21; used as retainer-outboard on tip assembly, fairing
01-152-4433
Structural Component Air Support
8.000" overall length 6.000" overall width 0.040" material thickness
01-152-4434
Structural Component Air Support
8.000" overall length 4.000" overall width 0.040" material thickness
01-152-4435
Structural Component Air Support
8.000" overall length 4.000" overall width 0.040" material thickness
01-152-4436
Structural Component Air Support
10.000" overall length 6.000" overall width 0.040" material thickness
01-152-4437
Structural Component Air Support
10.000" overall length 6.000" overall width 0.040" material thickness
01-152-4438
Structural Component Air Support
9.000" overall length 6.000" overall width 0.040" material thickness
01-152-4439
Structural Component Air Support
8.000" overall length 6.000" overall width 0.040" material thickness
01-152-4440
Structural Component Air Support
6.500" overall length 2.500" overall width 0.025" material thickness used on -516, -522, & -545
01-152-4447
Aircraft Former
89.500" overall length 17.500" overall width 0.040" material thickness opp 25-2779-802
01-152-4448
Aircraft Former
89.500" overall length 17.000" overall width 0.040" material thickness opp 25-2779-801
01-152-4449
Aircraft Former
89.500" overall length 18.000" overall width 0.040" material thickness opp 25-2779-804
01-152-4450
Aircraft Former
89.000" overall length 18.000" overall width 0.040" material thickness opp 25-2779-803
01-152-4451
Aircraft Former
Used on b-52 aircraft. opp 35-10704
01-152-4452
Aircraft Former
7.400" overall length 1.400" overall width 0.050" material thickness
01-152-4453
Aircraft Former
Used on b-52 aircraft. opp 35-10704-801
01-152-4454
Aircraft Former
5.000" overall length 1.500" overall width 0.063" material thickness
01-152-4455
Aircraft Former
7.000" overall length 2.000" overall width 0.032" material thickness heat treat 180, 000-200, 000; opp -192
01-152-4456
Aircraft Former
7.000" overall length 2.000" overall width 0.032" material thickness heat treat 180, 000-200, 000; finish f-8.05; opposite -191
01-152-4457
Aircraft Former
6.000" overall length 3.000" overall width 0.032" material thickness heat treat 180, 000-200, 000; finish f-8.05; opp -194
01-152-4458
Aircraft Former
6.000" overall length 3.000" overall width 0.032" material thickness heat treat 180, 000-200, 000; finishf-8.05; opp -193
01-152-4459
Aircraft Former
58.000" overall length 2.000" overall width 0.032" material thickness heat treat 180, 000-200, 000; finishf-8.05; opp -198
01-152-4460
Aircraft Former
58.000" overall length 2.000" overall width 0.063" material thickness heat treat 180, 000-200, 000; finish f-8.05; opp -197
01-152-4461
Aircraft Former
7.000" overall length 6.000" overall width 0.040" material thickness heat treat T4
01-152-4462
Aircraft Former
10.380" overall length 1.000" overall width 0.020" material thickness heat treat 180, 000-200, 000; finish f-8.51; opp -514
01-152-4463
Aircraft Former
10.380" overall length 1.000" overall width 0.020" material thickness heat treat 180000-200000; finish f-8.51; opposite -513
01-152-4464
Aircraft Former
2.500" overall length 0.700" overall width 0.040" material thickness opposite -201; tempered T3; finish f-2.115
01-152-4465
Aircraft Former
2.500" overall length 0.800" overall width 0.025" material thickness used on -516, -522
01-152-4466
Aircraft Former
12.800" overall length 0.100" overall width 0.020" material thickness
01-152-4467
Aircraft Former
10.000" overall length 1.300" overall width 0.020" material thickness finish f-10.10
01-152-4468
Aircraft Former
13.500" overall length 9.800" overall width 0.020" material thickness finish f-10.10
01-152-4469
Aircraft Former
10.000" overall length 1.300" overall width 0.020" material thickness finish f-10.10
01-152-4470
Aircraft Former
1.900" overall length 1.600" overall width 0.025" material thickness used on -516, -522
01-152-4471
Longeron
Used on B-52. opposite pn -2003
01-152-4472
Aircraft Skin
Used on B-52. 89.500" overall length 15.000" overall width opposite to p/n 25-2779-10
01-152-4473
Aircraft Skin
Used on B-52. 89.500" overall length 15.000" overall width opposite to p/n 25-2779-9
01-152-4474
Aircraft Skin
Used on B-52. 72.000" overall length 14.000" overall width opposite p/n 25-2779-24
01-152-4475
Aircraft Skin
Used on B-52. 72.000" overall length 14.000" overall width opposite p/n 25-2779-23
01-152-4476
Aircraft Skin
Used on B-52. 72.000" overall length 14.000" overall width opposite p/n 25-2779-26
01-152-4477
Aircraft Skin
Used on B-52. 72.000" overall length 14.000" overall width opposite p/n 25-2779-25
01-152-5160
Movable Canopy
01-152-5161
Movable Canopy
01-152-5164
Aircraft Former
Used on acft model ef-111.
01-152-5187
Structural Aircraft Plate
24.000" overall length 6.000" overall width 0.040" material thickness
01-152-5188
Structural Aircraft Plate
24.000" overall length 6.000" overall width 0.040" material thickness
01-152-5189
Structural Aircraft Plate
14.900" overall length 8.500" overall width 0.050" material thickness
01-152-5191
Structural Component Air Support
Used on acft model b52. c/o clip 1 ea p/n 29-2498-817, clip 1 ea p/n 29-2498-818, bracket 1 ea p/n 25-2781-803, used on outboard gap cover, left hand
