01-150-2504
Structural Component Air Fitting
5.500" overall length
01-150-2505
Structural Component Air Fitting
5.500" overall length
01-150-2506
Structural Component Air Fitting
5.500" overall length
01-150-2507
Structural Component Air Fitting
5.500" overall length
01-150-2508
Structural Component Air Support
C/o 1 channel, 1 angle, 1 clip assy, 1 guard strip, 3 rivets
01-150-2509
Structural Component Air Support
C/o 1 channel, 2 clip assy, 1 guard strip
01-150-2510
Structural Component Air Support
C/o 1 channel, 2 clip assy, 1 guard assembly
01-150-2511
Structural Component Air Support
6.700" overall length 1.500" overall width 1.000" material thickness
01-150-2512
Structural Component Air Support
C/o 1 channel, 2 support assy
01-150-2516
Aircraft Floor
Used on B-52.
01-150-2517
Aircraft Former
22.500" overall length 4.500" overall width 0.080" material thickness 8630
01-150-2518
Aircraft Former
Used on B-52. opposite p/n 25-2308-29
01-150-2519
Aircraft Former
Used on B-52. 6.100" overall length 2.100" overall width 0.050" material thickness opposite p/n 35-8992-132
01-150-2520
Aircraft Former
Used on B-52. 8.300" overall length 2.500" overall width 0.050" material thickness opposite p/n 35-8992-133
01-150-2521
Aircraft Former
Used on B-52.
01-150-2522
Aircraft Former
Used on B-5. 9.500" overall length 1.600" overall width 0.080" material thickness
01-150-2523
Aircraft Former
Used on B-52. 45.000" overall length 33.000" overall width 0.025" material thickness
01-150-2524
Aircraft Former
Used on B-52. 10.500" overall length 1.700" overall width 0.025" material thickness
01-150-2525
Aircraft Former
Used on B-52. 3.000" overall length 2.700" overall width 0.040" material thickness opposite p/n 35-8229-98
01-150-2526
Aircraft Former
Used on B-52. 21.000" overall length 11.000" overall width 0.025" material thickness opposite p/n 35-8229-98
01-150-2527
Aircraft Former
2.300" overall length 0.900" overall width 0.100" material thickness
01-150-2529
Aircraft Former
16.550" overall length 1.400" overall width 0.016" material thickness zee shaped; 1.230 in. h.
01-150-2530
Aircraft Former
17.000" overall length
01-150-2531
Aircraft Former
64.000" overall length alter bac 1515-514 extrusion
01-150-2532
Aircraft Former
Used on B-52. opposite p/n 25-2321-811
01-150-2533
Aircraft Former
Used on B-52.
01-150-2534
Aircraft Former
Used on B-52.
01-150-2535
Aircraft Former
36.000" overall length 4.500" overall width 0.040" material thickness finish f-2.115; heat treated to T4; stiffener
01-150-2536
Aircraft Former
36.000" overall length 4.500" overall width 0.040" material thickness finish f-2.115; heat treated to T4; stiffener
01-150-2537
Aircraft Former
44.200" overall length 2.500" overall width 0.025" material thickness stiffener; opposite -254; finish f-2.115
01-150-2538
Aircraft Former
44.200" overall length 2.500" overall width 0.025" material thickness stiffener; opposite -253; finish f-2.115
01-150-2539
Aircraft Former
11.000" overall length 10.300" overall width 0.025" material thickness angle frame; opposite -50; finish f-2.115; heat treated to T6
01-150-2540
Aircraft Former
9.500" overall length 4.000" overall width 0.320" material thickness commercially pure; finish f-10.10; opposite p/n -194
01-150-2541
Aircraft Former
9.500" overall length 4.000" overall width 0.320" material thickness commercially pure; finish f-10.10; opposite p/n -193
01-150-2542
Aircraft Former
2.600" overall length 0.800" overall width 0.063" material thickness finish f-2.115
01-150-2543
Aircraft Former
5.300" overall length 3.200" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -204
01-150-2544
Aircraft Former
5.300" overall length 3.200" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -203
01-150-2545
Aircraft Former
4.000" overall length 3.600" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -206
01-150-2546
Aircraft Former
4.000" overall length 3.600" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -205
01-150-2547
Aircraft Former
5.800" overall length 2.900" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -208
01-150-2548
Aircraft Former
5.800" overall length 2.900" overall width 0.032" material thickness commercially pure; finish f-10.10; opposite p/n -207
01-150-2549
Longeron
84.000" overall length 2.500" overall width 0.063" material thickness
01-150-2550
Longeron
Used on B-52. opposite pn 25-2321-853
01-150-2551
Longeron
84.000" overall length 2.500" overall width 0.063" material thickness
01-150-2552
Longeron
Used on B-52. opposite pn 25-2321-855
01-150-2553
Longeron
42.000" overall length 3.500" overall width 0.040" material thickness opposite pn -256; inboard; finish f-10.10
01-150-2554
Longeron
42.000" overall length 3.500" overall width 0.040" material thickness opposite pn -255; finish f-10.10; inboard
01-150-2555
Aircraft Skin
Used on B-52. 19.000" overall length 11.000" overall width
01-150-2556
Aircraft Skin
Used on B-52. 85.000" overall length 15.000" overall width 1/2 hard surface condition 2b
01-150-2557
Aircraft Skin
Used on B-52. 85.000" overall length 15.000" overall width 1/2 hard surface condition 2b
