01-148-5627
Structural Component Air Support
Used on acft model b-52. angle
01-148-5628
Structural Component Air Support
Used on acft model b-52. angle
01-148-5629
Structural Component Air Support
01-148-5630
Structural Component Air Support
01-148-5631
Structural Component Air Support
12.000" overall length 4.500" overall width 1.375" material thickness
01-148-5632
Structural Component Air Support
12.000" overall length 4.500" overall width 1.375" material thickness
01-148-5633
Structural Component Air Support
25.000" overall length 5.500" overall width 2.500" material thickness
01-148-5634
Structural Component Air Support
25.000" overall length 5.500" overall width 2.500" material thickness
01-148-5635
Structural Component Air Support
14.000" overall length 5.750" overall width 1.375" material thickness
01-148-5636
Structural Component Air Support
17.400" overall length 4.770" overall width 2.220" material thickness
01-148-5637
Structural Component Air Support
Used on acft model b52. c/o 21 component parts
01-148-5638
Structural Component Air Support
11.000" overall length 4.750" overall width 2.250" material thickness
01-148-5639
Structural Component Air Support
01-148-5640
Structural Component Air Support
01-148-5641
Structural Component Air Support
01-148-5649
Aircraft Former
2.100" overall length 1.100" overall width 0.040" material thickness finish f-10.10; clad
01-148-5650
Aircraft Former
1.100" overall length 1.000" overall width 0.040" material thickness finish f-10.10
01-148-5651
Aircraft Former
1.800" overall length 1.100" overall width 0.080" material thickness finish f-2.115
01-148-5655
Aircraft Former
01-148-5656
Aircraft Former
25.000" overall length 8.000" overall width 0.040" material thickness finish f-3.30 except apply primer mil-p-23377 per bac 5736
01-148-5657
Aircraft Former
5.100" overall length 1.200" overall width 0.020" material thickness
01-148-5660
Aircraft Former
Used on B-52. extruded; function-tee
01-148-5661
Aircraft Former
17.500" overall length
01-148-5662
Aircraft Former
18.000" overall length
01-148-5663
Aircraft Former
18.000" overall length
01-148-5665
Aircraft Former
26.000" overall length
01-148-5666
Aircraft Former
26.000" overall length
01-148-5667
Aircraft Former
17.500" overall length 1.600" overall width 0.050" material thickness
01-148-5669
Longeron
31.600" overall length 5.700" overall width 0.080" material thickness
01-148-5670
Longeron
35.900" overall length 5.500" overall width 0.040" material thickness
01-148-5673
Airfoil Rib
27.500" overall length 22.000" overall width 0.080" material thickness pfd altn
01-148-5674
Airfoil Rib
27.500" overall length 22.000" overall width 0.080" material thickness pfd altn
01-148-5676
Airfoil Rib
Used on A-10. 27.500" overall length 22.000" overall width 0.080" material thickness
01-148-5677
Aircraft Skin
Used on B-52. 60.000" overall length 29.000" overall width 6A1-4v annealed, bms 7-39; finish f 10.10
01-148-5678
Aircraft Skin
Used on B-52. 95.000" overall length 22.000" overall width 6A1-4v annealed, bms 7-39; finish f 10.10
01-148-5679
Aircraft Skin
Used on B-52. 95.000" overall length 22.000" overall width 6A1-4v annealed, bms 7-38; finish f 10.10; opposite p/n -7
01-148-5680
Aircraft Skin
Used on B-52. 30.000" overall length 12.000" overall width finish f 2.130
01-148-5681
Aircraft Skin
Used on B-52. 51.500" overall length 25.000" overall width
01-148-5682
Aircraft Skin
Used on B-52. finish 2.130
01-148-5683
Aircraft Skin
Used on b-52 bomber airplane....
01-148-5684
Aircraft Skin
Used on b-52 bomber airplane....
01-148-5686
Aircraft Skin
Used on b-52 bomber airplane.... material; cres sheet, aisi 302, comp d, annealed, surf cond 2d
01-148-5844
Fluid Aircraft Manifold
01-148-6328
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 fairing installation-outboard strut
01-148-6330
Structural Aircraft Plate
40.500" overall length 7.500" overall width 0.080" material thickness
01-148-6331
Structural Aircraft Plate
9.000" overall length 4.700" overall width 0.050" material thickness
01-148-6332
Structural Aircraft Plate
8.400" overall length 3.000" overall width 0.050" material thickness
01-148-6333
Structural Aircraft Plate
8.400" overall length 3.000" overall width 0.050" material thickness
01-148-6334
Structural Component Air Support
10.000" overall length T6 temp; finish f-2.30; opp -814
01-148-6335
Structural Component Air Support
10.000" overall length T6 temper; finish f-2.30; opp-813
