01-162-4208
Structural Aircraft Panel
Used on f-5 aircraft.
01-162-4209
Structural Aircraft Panel
Used on f-5 acft. location-fuselage station-337.000 to 359.494; function-dorsal cover
01-162-4210
Structural Aircraft Plate
Used on acft model kc-135r. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.03; 3.100 in. lg, 0.900 in. w, 0.100 in. thk; located nacelle station 224.465; nha 458-58077-4
01-162-4211
Structural Aircraft Plate
Used on acft model kc-135r. c/o corrosion resistant steel 304 per mil-s-5059 firewall, al 2024-T81 bonded web assembly; located nacelle station 204.21; opposite p/n -509; nha 458-58042-508
01-162-4212
Structural Aircraft Plate
Used on acft model kc-135r. al alloy clad sheet 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 11.900 in. lg, 7.400 in. w, 0.063 in. thk; nha 458-58066-8
01-162-4675
Access Aircraft Door
Used on av-8b acft.
01-162-4676
Access Aircraft Door
Used on av-8b acft.
01-162-4677
Access Aircraft Door
Used on av-8b acft.
01-162-5480
Structural Component Air Bracket
11.000" overall length 3.500" overall width 0.032" material thickness
01-162-5481
Structural Component Air Bracket
11.000" overall length 3.500" overall width 0.032" material thickness
01-162-5482
Structural Component Air Bracket
6.500" overall length 1.600" overall width 0.032" material thickness
01-162-5499
Structural Aircraft Plate
5.000" overall length 4.000" overall width 0.064" material thickness 1/16 laminated, cotton fabric base
01-162-5500
Structural Aircraft Plate
2.500" overall length 1.600" overall width 0.050" material thickness
01-162-5501
Structural Component Air Support
2.500" overall length 2.400" overall width 0.090" material thickness
01-162-5503
Structural Component Air Support
8.000" overall length 2.000" overall width 0.080" material thickness
01-162-5504
Structural Component Air Fitting
01-162-5505
Structural Component Air Fitting
01-162-5506
Structural Component Air Support
3.800" overall length 2.200" overall width 0.063" material thickness
01-162-5507
Structural Component Air Support
3.800" overall length 2.200" overall width 0.063" material thickness
01-162-5509
Aircraft Former
5.900" overall length 1.500" overall width 0.050" material thickness
01-162-5510
Aircraft Former
7.000" overall length 3.000" overall width 0.063" material thickness
01-162-5511
Aircraft Former
80.000" overall length 45.000" overall width 0.040" material thickness opp -16
01-162-5512
Aircraft Former
80.000" overall length 45.000" overall width 0.040" material thickness opp -15
01-162-5513
Aircraft Former
7.000" overall length 3.000" overall width 0.063" material thickness
01-162-5514
Aircraft Former
7.000" overall length 3.000" overall width 0.063" material thickness
01-162-5515
Aircraft Former
2.200" overall length 0.870" overall width 0.063" material thickness
01-162-5516
Aircraft Former
10.500" overall length 6.300" overall width 0.080" material thickness
01-162-5517
Aircraft Former
10.500" overall length 6.300" overall width 0.080" material thickness opp 39-9918-21; 0 temper
01-162-5518
Aircraft Former
16.000" overall length 5.500" overall width 0.063" material thickness
01-162-5519
Aircraft Former
16.000" overall length 5.500" overall width 0.063" material thickness
01-162-5520
Longeron
Used on B-52.
01-162-6458
Structural Aircraft Panel
74.000" overall length 26.000" overall width opp -18; alum honeycomb core
01-162-6460
Structural Component Air Bracket
5.500" overall length 4.700" overall width 0.040" material thickness
01-162-6483
Structural Aircraft Panel
Used on acft model kc-135r. used as honeycomb panel assembly on fan duct inner acoustic panel assembly; opposite p/n -510; nha 458-58025-507
01-162-6494
Structural Aircraft Panel
Used on B-52. 6.000" overall length 17.000" overall width opposite p/n 39-99295-8
01-162-6495
Structural Aircraft Panel
Used on B-52. 6.000" overall length 17.000" overall width opposite p/n 39-9915-7
01-162-6496
Structural Aircraft Panel
Used on B-52. 6.000" overall length 11.000" overall width opposite p/n 39-9915-10
01-162-6497
Structural Aircraft Plate
6.000" overall length 11.000" overall width 0.080" material thickness opposite to p/n 39-9915-9; used as web fwd
01-162-6498
Structural Aircraft Plate
2.700" overall length 2.400" overall width 0.080" material thickness used as web; comp 4335
01-162-6499
Structural Aircraft Plate
2.300" overall length 1.000" overall width 0.125" material thickness used as pad; comp 4335
01-162-6503
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-0; matl size 0.050 by 1.540 by 20.000 in. lg; opposite to p/n 25-2377-816; used as splice plate on nose cowl assy
01-162-6504
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-0; matl size 0.050 by 1.540 by 20.000 in. lg; opposite to p/n 25-2377-817; used as splice plate on nose cowl assy
01-162-6505
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-0; matl size 0.050 by 1.540 by 20.000 in. lg; opposite to p/n 25-2377-814; used as splice plate on nose cowl assy
01-162-6506
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-T3; matl size 0.050 by 2.500 by 27.000 in. lg; used as splice plate on nose cowl assy
01-162-6507
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-367, 2024-T3; matl size 0.050 by 2.500 by 26.000 in. lg; opposite to p/n 25-2377-67; used as splice plate on nose cowl assy
01-162-6509
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 25-2377-63; used as splice plate on nose cowl assy
01-162-6510
Structural Aircraft Plate
Used on b-52 acft. matl magnesium alloy; matl size 0.050 by 2.000 by 51.000 in. lg; used as circular splice plate on nose cowl assy
01-162-6511
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-T3; matl size 0.050 by 3.000 by 33.000 in. lg; used as splice plate on nose cowl assy
01-162-6512
Structural Aircraft Plate
3.300" overall length 0.900" overall width 0.310" material thickness comp 4335
01-162-6513
Structural Aircraft Plate
3.100" overall length 1.000" overall width 0.312" material thickness comp 4335
