01-234-4945
Aircraft Skin
66.000" overall length 7.000" overall width
01-234-4946
Aircraft Skin
82.000" overall length 7.000" overall width
01-234-5283
Structural Component Air Support
2.810" overall length 1.920" overall width
01-234-5284
Structural Component Air Support
14.450" overall length
01-234-5285
Movable Canopy
Used on f-4 aircraft. consists of three sections
01-234-5286
Aircraft Floor
01-234-5290
Thermal Special Purpo Insulation
01-234-5851
Stiffener Aircraft Rib
8.600" overall length 5.800" overall width 0.040" material thickness
01-234-6699
Fuselage Aircraft Fairing
Used on uh-60a helicopter. fiberglass, ss 9578-009, c/o component quantity, 32;
01-234-6704
Aircraft Floor
Used on ch-47d aircraft.
01-234-7306
Aircraft Skin
Aluminum alloy per qq-a-250/13, cond-o
01-234-7442
Exhaust Pipe
Used on acft model kc-135. used on engine thrust reverser tail pipe; nha 65-10500
01-234-7712
Aircraft Floor
Includes 1 rug p/n 906437-5; 1 panel p/n 906437-7
01-234-7713
Aircraft Leading Edge
01-234-8547
Aircraft Door
01-234-8548
Aircraft Door
01-234-8582
Structural Aircraft Plate
Used on c-5b aircraft. matl fiberglass per stm 22-502 impregnated with epoxy resin per mil-r-9300 warp 45 deg to each other; nha 4J12004
01-234-8583
Structural Aircraft Plate
Used on C-5. c/o: -105b angle (1) , -601b retainer (1) , shim (1) ; opposite -104a; part of -101a seal instl-pressure, forward ramp
01-234-8584
Structural Aircraft Plate
Used on acft model f-16. material per fms-3022-T81, 29.000 in. lg, 8.000 in. w, 0.125 in. thk
01-234-8585
Structural Aircraft Plate
Used on F-15.
01-234-8586
Structural Component Air Support
C/o 2 supports; nha 4A10006-101a
01-234-8598
Structural Aircraft Panel
Used on c-5b aircraft. access panel assembly-owbr sta 79.171; c/o: -103a panel (1) , -105a stiffener (2) , -107a doubler (1) , stiffener (3) , dome nut (38) ; nha 4W73004-101a
01-234-8618
Aircraft Former
01-234-8625
Aircraft Leading Edge
Nha 16B4825-5
01-234-8626
Aircraft Leading Edge
Superseded p/n 16B4821-12, nic-ow, ecn 14U45, nha 16B4825-6
01-234-8652
Aircraft Wing Assembly
Wing box assy
01-234-9123
Aircraft Former
21.000" overall length 3.300" overall width 0.063" material thickness
01-234-9124
Aircraft Former
23.000" overall length 3.300" overall width 0.063" material thickness
01-234-9125
Aircraft Former
30.000" overall length 3.300" overall width 0.063" material thickness
01-234-9126
Aircraft Former
21.000" overall length 3.300" overall width 0.063" material thickness
01-234-9127
Aircraft Former
22.000" overall length 4.100" overall width 0.125" material thickness
01-234-9128
Aircraft Former
22.000" overall length 4.100" overall width 0.125" material thickness
01-234-9129
Aircraft Former
21.000" overall length 3.300" overall width 0.063" material thickness
