01-149-6413
Structural Aircraft Plate
10.100" overall length 4.000" overall width 0.050" material thickness opposite -10; used as longeron splice
01-149-6414
Structural Aircraft Plate
12.300" overall length 0.600" overall width 0.063" material thickness used as doubler on firewall installation, aisi 301, 1/3 hard
01-149-6415
Structural Aircraft Plate
6.300" overall length 6.000" overall width 0.025" material thickness used as filler on firewall installation
01-149-6416
Structural Aircraft Plate
16.000" overall length 1.600" overall width 0.045" material thickness used as doubler on firewall installation
01-149-6417
Structural Aircraft Plate
7.100" overall length 5.300" overall width 0.045" material thickness used as doubler on firewall installation
01-149-6418
Structural Aircraft Plate
7.700" overall length 3.200" overall width 0.063" material thickness location-closure rib assembly, function-doubler; aisi-301
01-149-6419
Structural Aircraft Plate
15.300" overall length 13.000" overall width 0.040" material thickness used as web on firewall installation
01-149-6420
Structural Aircraft Plate
Used as doubler on firewall installation, forward nacelle; opposite p/n 25-2308-93
01-149-6421
Structural Aircraft Plate
2.300" overall length 2.300" overall width 0.045" material thickness used as doubler on firewall installation, aisi 301, 1/4 hard
01-149-6422
Structural Aircraft Plate
7.100" overall length 1.800" overall width 0.080" material thickness used as filler on firewall installation
01-149-6423
Aircraft Fairing
Used on F-16. c/o of 50 component parts
01-149-6424
Structural Component Air Support
Used on c-5 acft.
01-149-6425
Structural Component Air Support
23.6000" overall length 2.000" overall width 0.040" material thickness class 6
01-149-6426
Structural Component Air Fitting
01-149-6427
Structural Component Air Fitting
01-149-6428
Structural Component Air Support
Used on b-52 acft.
01-149-6429
Structural Component Air Support
Used on b-52 acft.
01-149-6430
Structural Component Air Support
01-149-6431
Structural Component Air Support
3.500" overall length 2.300" overall width 0.050" material thickness soft steel sheet 17-7ph BMS7-12
01-149-6438
Aircraft Former
Used on B-52. function stiffener assembly
01-149-6439
Aircraft Former
35.000" overall length 2.400" overall width 0.080" material thickness 8630 sheet
01-149-6442
Aircraft Former
Used on B-52.
01-149-6443
Aircraft Former
19.700" overall length 1.500" overall width 0.063" material thickness
01-149-6449
Aircraft Former
11.700" overall length 2.100" overall width 0.050" material thickness
01-149-6450
Aircraft Former
9.000" overall length 3.700" overall width 0.050" material thickness
01-149-6455
Aircraft Former
12.700" overall length 2.400" overall width 0.050" material thickness
01-149-6456
Aircraft Former
20.100" overall length 1.900" overall width 0.063" material thickness
01-149-6457
Aircraft Former
Used on B-52.
01-149-6458
Aircraft Former
Used on B-52. function-zee door attachment
01-149-6459
Aircraft Former
Used on B-52. function-zee door attachment
01-149-6460
Aircraft Former
Used on B-52. 4335; forge per mil-f-7190 grade a
01-149-6461
Aircraft Former
Used on B-52.
01-149-6462
Aircraft Former
Used on B-52.
01-149-6463
Aircraft Former
Used on B-52.
01-149-6464
Aircraft Former
Used on B-52.
01-149-6465
Aircraft Former
11.100" overall length 1.500" overall width 0.050" material thickness
01-149-6468
Aircraft Skin
Used on acft model b-52. commercially pure titanium sheet per mil-t-9046, class 7; finish f-10.10; 50.000 in. lg, 11.000 in. w, 0.025 in. thk; opposite p/n -12
01-149-6469
Aircraft Skin
Used on acft model b-52. commercially pure titanium sheet per mil-t-9046, class 7; finish f-10.10; 50.000 in. lg, 11.000 in. w, 0.025 in. thk; opposite p/n -11
01-149-6511
Aircraft Former
10.700" overall length 1.500" overall width 0.040" material thickness
01-149-6512
Aircraft Former
10.700" overall length 1.500" overall width 0.040" material thickness
01-149-6582
Structural Aircraft Plate
Used on acft model c/kc-135. al clad sheet 7075-0 per qq-a-287, 0 temper; heat treated to condition T6; finish f-2.115; 54.000 in. lg, 12.000 in. w, 0.050 in. thk; opposite p/n -182
01-149-6583
Structural Aircraft Plate
Used as shield on pilot seat bulkhead
01-149-6584
Aircraft Fairing
31.000" overall length 18.000" overall width 0.125" material thickness opposite -502
01-149-6585
Structural Component Air Support
6.900" overall length 5.500" overall width 6.400" material thickness bms-7-28 forge
01-149-6586
Structural Component Air Support
6.900" overall length 5.500" overall width 6.400" material thickness bms-7-28 forge
01-149-6587
Structural Component Air Support
3.000" overall length 2.400" overall width 0.040" material thickness soft steel sheet 17-7ph BMS7-12
01-149-6588
Structural Component Air Support
01-149-6589
Structural Component Air Support
01-149-6590
Structural Component Air Support
Support/p/n 26-2-62-2, nut plate-self locking p/n MK2000-1032
01-149-6591
Structural Component Air Support
Support; p/n 26-2062-4, nut plate-self locking p/n MK2000-1032
