01-162-6516
Structural Aircraft Plate
3.300" overall length 0.900" overall width 0.310" material thickness opp pn 35-8389-33; comp 4335
01-162-6518
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-0; matl size 0.050 by 3.000 by 32.000 in. lg; opposite to p/n 25-2377-64; used as splice plate on nose cowl assy
01-162-6520
Structural Component Air Support
Used on f-16 aircraft. to replace -5; c/o-fitting, bushing, coating-3, adhesive, general sealant; material of fitting-aluminum alloy per qq-a-367, finish-A100
01-162-6521
Structural Component Air Support
2.000" overall length
01-162-6522
Structural Component Air Support
Used on acft model b-1b. 0.500 in.thk, 0.625 in.w, 2.583 in.lg, 3 holes 0.404 in.dia
01-162-6523
Structural Component Air Support
3.800" overall length 2.200" overall width 0.063" material thickness
01-162-6524
Structural Component Air Support
3.800" overall length 2.200" overall width 0.063" material thickness
01-162-6525
Structural Component Air Support
3.800" overall length 2.200" overall width 0.065" material thickness
01-162-6526
Structural Component Air Support
3.800" overall length 2.200" overall width 0.063" material thickness
01-162-6527
Structural Component Air Support
2.300" overall length 1.500" overall width 0.072" material thickness
01-162-6528
Structural Component Air Support
2.700" overall length 1.500" overall width 0.072" material thickness
01-162-6529
Structural Component Air Support
17.700" overall length 3.500" overall width 0.072" material thickness
01-162-6530
Structural Component Air Bracket
17.700" overall length 3.500" overall width 0.072" material thickness
01-162-6531
Structural Component Air Support
14.200" overall length 2.600" overall width 0.063" material thickness
01-162-6532
Structural Component Air Support
1.800" overall length 1.600" overall width 0.063" material thickness
01-162-6559
Aircraft Former
6.500" overall length 4.000" overall width 0.063" material thickness
01-162-6560
Aircraft Former
6.500" overall length 4.000" overall width 0.063" material thickness
01-162-6561
Aircraft Former
3.600" overall length 1.300" overall width 0.063" material thickness
01-162-6571
Aircraft Pylon
Supperceded -847 ow; c/o hardware, door assy, beam, panel, panel assy, trailing edge, trailing edge assy, fairing l.e, frame, sway brace, support assy, equipment instl, hardness instl, tape instl, rib assy, closure, channel; nha 16S500-205; eff on 67 1691, 1694, 1696, 1730, 1734, 1739, 1783
01-162-6572
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width oppos -20
01-162-6573
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width oppos -19
01-162-6714
Fluid Aircraft Manifold
4.155" overall length 2.560" overall width
01-162-6715
Fluid Aircraft Manifold
24.620" overall length 15.000" overall width
01-162-7317
Access Aircraft Door
Used on acft model b-1b.
01-162-7401
Structural Aircraft Panel
C/o 1 honeycomb panel, 1 angle, 1 bonded skin assy, 1 shim, 1 clip, 1 fireseal, 1 airscoop, 1 fitting, 1 junction box seal, , 2 hooks, 1 fitting assy; opposite -507; nha 458-58024
01-162-7406
Structural Aircraft Panel
Used on acft model kc-135r. fused as panel assy on inbd trailing edge fairing instl; c/o 6 doublers, 1 core (dense) , 3 core (light) , 1 inner skin, 1 outer skin, 4 zee members, assembly hardware; opposite p/n -6; nha 65C20606-4
01-162-7408
Structural Aircraft Panel
Used on acft model kc-135r. used as panel assy on outbd trailing edge fairing instl; c/o 6 doublers, 3 core (light) , 1 core (dense) , 1 inner skin, 1 outer skin, 4 zee members; opposite p/n -6; nha 65C20617-3
01-162-7409
Structural Aircraft Panel
Used on acft model kc-135r. used as panel assy on outbd trailing edge fairing instl; c/o 6 doublers, 3 core (light) , 1 core (dense) , 1 inner skin, 1 outer skin, 4 zee members; opposite p/n -5; nha 65C20617-4
01-162-7412
Structural Aircraft Panel
88.000" overall length 48.000" overall width
01-162-7413
Structural Aircraft Panel
88.000" overall length 48.000" overall width
01-162-7414
Structural Aircraft Panel
65.000" overall length 28.000" overall width
01-162-7415
Structural Aircraft Panel
65.000" overall length 28.000" overall width opp -33
01-162-7416
Structural Aircraft Panel
66.000" overall length 30.000" overall width opp -36
01-162-7417
Structural Aircraft Panel
66.000" overall length 30.000" overall width opp -35; alum honeycomb core
01-162-7418
Structural Aircraft Panel
74.000" overall length 26.000" overall width opp -6
01-162-7419
Structural Aircraft Panel
74.000" overall length 26.000" overall width opp -5
01-162-7420
Structural Aircraft Panel
Used on acft model kc-135r. used as panel assy on outer trailing edge fairing instl; c/o 1 outer skin, 5 doublers, 1 core (dense) , 4 core (light) , 1 inner skin, 4 zee members; opposite p/n -7; nha 65C20617-4
01-162-7463
Structural Aircraft Plate
Used on acft model kc-135r.
01-162-7473
Structural Aircraft Plate
Used on acft model b52.
01-162-7478
Structural Component Air Support
0.800" overall length 1.100" overall width 0.250" material thickness matl st, aisi 416, class 6, type a; heat treat 16, 000 to 20, 000 psi; clevis on one end; 0.193 dia countersunk 45 deg at one end; 0.187 dia hole; used as link, hinge latch
01-162-7479
Structural Component Air Support
3.400" overall length 6.000" overall width 0.063" material thickness
01-162-7480
Structural Component Air Support
Used on acft model kc-135r.
01-162-7483
Structural Component Air Support
Used on acft model kc-135. inconel 625 sheet per AMS5599, annealed; finish f-25.01; 3.300 in. lg, 2.100 in. w, 0.063 in. thk; c/o 1 support, 3 nutplates; nha 35-35373
01-162-7484
Structural Component Air Support
Used on acft model kc-135.
01-162-7485
Structural Component Air Support
Used on acft model kc-135.
01-162-7487
Structural Component Air Support
Used on acft model kc-135.
01-162-7488
Structural Component Air Support
Used on acft model kc-135.
01-162-7489
Structural Component Air Support
Used on acft model kc-135.
01-162-7490
Structural Component Air Support
Used on acft model kc-135.
01-162-7491
Structural Component Air Support
Used on acft model kc-135.
