01-149-0469
Structural Component Air Bracket
Clip finish f-2.30; made from AND10136-2407 by 1.000 in. lg; extruded
01-149-0470
Structural Component Air Bracket
Clip finish f-2.30; make from AND10136-2407 extruded; opposite -11
01-149-0471
Structural Component Air Bracket
Used on B-52. clip extruded; finish f-2.30; make from AND10136-2407; opposite -14
01-149-0472
Structural Component Air Bracket
Used on B-52. clip extruded; finish f-2.30; make from AND10136-2407 spec material; opp 13
01-149-0473
Structural Component Air Bracket
Used on B-52. clip extruded; finish f-2.30; make from BAC1505-100156 spec material; opp 16
01-149-0474
Structural Component Air Bracket
Used on B-52. clip extruded; finish f-2.30; make from BAC1505-100136 spec material; opp 15
01-149-0475
Structural Component Air Bracket
Clip extruded; finish f-2.30; make from BAC1505-100156 spec material; opp -18
01-149-0476
Structural Component Air Bracket
Clip extruded; finish f-2.30; make from BAC1505-100156 spec material; opp -17
01-149-0477
Structural Component Air Bracket
Clip finish f-2.30; make from AND10136-2407 spec material; opp -8
01-149-0478
Structural Component Air Bracket
Clip finish f-2.30; make from AND10136-2407 spec material; opp -7
01-149-0479
Structural Component Air Bracket
2.500" overall length 1.500" overall width 0.040" material thickness clip dim. are stock material
01-149-0480
Structural Component Air Bracket
2.500" overall length 1.500" overall width 0.040" material thickness clip dim. are stock material
01-149-0481
Structural Component Air Bracket
Clip finish f-2.30; make from AND10136-2407 spec material; opp -10
01-149-0482
Structural Component Air Bracket
2.500" overall length 1.500" overall width 0.125" material thickness clip dim. are stock material
01-149-0483
Aircraft Former
Used on B-52. stiffener-angle
01-149-0484
Aircraft Former
Used on B-52. stiffener-angle
01-149-0485
Aircraft Former
Used on B-52. stiffener-angle
01-149-0486
Aircraft Former
8.400" overall length 4.000" overall width 0.063" material thickness
01-149-0487
Aircraft Former
Used on B-52.
01-149-0488
Aircraft Former
Used on B-52. opposite p/n 25-2308-15
01-149-0489
Aircraft Former
30.900" overall length 2.800" overall width 0.050" material thickness
01-149-0490
Aircraft Former
Used on B-52.
01-149-0491
Aircraft Former
37.000" overall length 5.000" overall width 0.063" material thickness
01-149-0492
Aircraft Former
Used on B-52. opposite p/n 25-2308-23
01-149-0493
Aircraft Former
15.200" overall length 11.300" overall width 0.040" material thickness
01-149-0494
Aircraft Former
Used on B-52. opposite p/n -25-2308-41
01-149-0495
Aircraft Former
11.300" overall length 8.300" overall width 0.040" material thickness
01-149-0496
Aircraft Former
Used on B-52.
01-149-0497
Aircraft Former
6.500" overall length 5.000" overall width 0.063" material thickness
01-149-0498
Aircraft Former
2.000" overall length 1.000" overall width 0.130" material thickness
01-149-0499
Aircraft Former
7.000" overall length 0.080" material thickness
01-149-0500
Aircraft Former
18.000" overall length 5.000" overall width 0.080" material thickness
01-149-0501
Aircraft Former
12.000" overall length 4.000" overall width 0.063" material thickness
01-149-0502
Aircraft Former
Used on B-52.
01-149-0503
Longeron
50.000" overall length 5.000" overall width 0.040" material thickness
01-149-0504
Longeron
Used on B-52. opposite pn 25-2308-27
01-149-0505
Aircraft Skin
Used on F-111.
01-149-1412
Access Aircraft Cover
01-149-1476
Structural Component Aircraf Web
01-149-1477
Access Aircraft Cover
Used on b-52 acft.
01-149-1498
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 302 per mil-s-5059 comp d annealed surf cond 2d; location-pp station 236.25, tail fairiring installation-outboard strut
01-149-1499
Structural Aircraft Plate
3.700" overall length 1.400" overall width 0.032" material thickness used as doubler on firewall installation, aisi 301-1/2 hard
01-149-1500
Structural Aircraft Plate
16.000" overall length 7.200" overall width 0.020" material thickness used as doubler on firewall installation
01-149-1501
Structural Aircraft Plate
12.300" overall length 1.200" overall width 0.025" material thickness used as filler on firewall installation
01-149-1502
Structural Aircraft Plate
6.100" overall length 1.300" overall width 0.071" material thickness location-closure rib assembly; function-filler
01-149-1503
Structural Aircraft Plate
6.100" overall length 1.300" overall width 0.071" material thickness location-closure rib assembly, function-filler;
01-149-1504
Structural Aircraft Plate
27.900" overall length 2.400" overall width 0.020" material thickness location-closure rib assembly, function-angle
01-149-1505
Structural Aircraft Plate
7.700" overall length 3.200" overall width 0.080" material thickness location-closure rib assembly, function-doubler; matl 6al-4v
01-149-1506
Structural Aircraft Plate
22.900" overall length 3.400" overall width 0.020" material thickness location-closure rib assembly, function-angle 18
01-149-1507
Structural Aircraft Plate
48.700" overall length 14.600" overall width 0.063" material thickness location-closure rib assembly, function-web; matl 6al-4v
