00-911-6683
Aircraft Skin
00-911-6684
Aircraft Skin
00-911-7328
Fluid Aircraft Manifold
00-911-7332
Access Aircraft Door
00-911-7856
Structural Aircraft Panel
00-911-8602
Access Aircraft Door
Used on uh-1, rotary wing aircraft.
00-911-8603
Fuselage Aircraft Fairing
Used on aircraft model uh1. aluminum alloy, qq-a-250/5;
00-911-8645
Aircraft Engine Build- Parts Kit
00-911-8780
Structural Aircraft Panel
00-911-9984
Structural Aircraft Panel
Aluminum alloy honeycomb, mil-c-7438, stock size 27.000 in. lg, 27.000in. w, 0.500 in. thk
00-912-0201
Aircraft Skin
Aluminum alloy, 0.04 in. thk
00-912-0277
Structural Aircraft Panel
00-912-0546
Airfoil Rib
Used on aircraft model a6.
00-912-0547
Airfoil Rib
Used on a6 acft.
00-912-0548
Wing Panel Outer Rib
00-912-0550
Wing Panel Outer Rib
00-912-0551
Wing Panel Outer Rib
00-912-0554
Wing Panel Outer Rib
00-912-1308
Airfoil Rib
Used on aircraft,model f-4c.
00-912-1309
Airfoil Rib
Used on aircraft,model f-4c.
00-912-1392
Structural Component Air Support
Used on acft model c-135. used on flap track, rear spar wing station 444
00-912-1393
Structural Component Air Support
Used on acft model c-135. used on flap track, rear spar wing station 444
00-912-1394
Structural Component Air Support
Used on acft model c-135. used on flap track, rear spar wing station 546.30 to 700.50
00-912-1395
Structural Component Air Support
Used on acft model c-135. used on flap track, rear spar wing station 546.30 to 700.50
00-912-1396
Structural Component Air Support
Used on acft model c-135. used on flap track, rear spar wing station 546.30 to 700.50
00-912-1806
Wing Landing Flap
00-912-1812
Wing Landing Flap
00-912-2076
Structural Component Air Support
Aluminum alloy, qq-a-367
00-912-5734
Aircraft Leading Edge
00-912-8029
Structural Component Air Support
00-912-8042
Structural Component Air Bracket
00-913-4057
Eye Rotating Shaft Bracket
Used on uh-1 series helicopters. 5.770" overall length bolt hole:qty-4, shape-round, size-0.264/0.270 in. dia; hole size, 2.750 in.; distance from bore ctrline to base bottom, 2.120/2.150 in.; c to c distance betwen bolt holes, 4.560 in.; hole location, horizontal line of ctr base; attchment type for which drilled, pin
00-914-8468
Aircraft Skin
Used on f-4 phantom airplane.... matt stock size 59.000 in. lg, 23.100 in. w, 0.190 in. thk, heat treat per T6
00-914-8469
Aircraft Skin
Used on f-4 phantom airplane....
00-914-8478
Airfoil Rib
Material type T6
00-914-9156
Radome
28.000" overall length 21.900" overall width
00-915-0890
Aircraft Trailing Edge
00-915-0891
Aircraft Trailing Edge
00-915-0892
Aircraft Trailing Edge
00-915-0893
Wing Landing Flap
0.125" material thickness 6AL4v
00-915-0896
Structural Aircraft Panel
Honeycomb core al, mil-c-7438
00-915-0919
Structural Aircraft Panel
00-915-0920
Structural Aircraft Panel
00-915-2652
Structural Aircraft Panel
Used on f-5 aircraft.
00-915-2667
Structural Aircraft Panel
C/o 1 inner skin, 1 outer skin, 1 core
00-915-2668
Structural Aircraft Panel
00-915-3329
Structural Aircraft Panel
00-915-3332
Structural Aircraft Panel
