00-229-1719
Aircraft Door
00-229-1764
Structural Component Air Support
Used on acft model c130a. stl 303 per mil-s-7720, ball 1.500 in.dia, 1.000 in.thk, base 2.500 in.dia, 0.250 in.thk, shank 0.500 in.dia, 0.500 in.lg, used on apq-115 indicator
00-229-2051
Structural Component Air Fitting
0.875" overall width 0.050 " material thickness steel 4130 per mil-s-18729
00-229-3572
Aircraft Skin
Used on aircraft model a7d.
00-229-3802
Aircraft Fairing
00-230-1804
Access Aircraft Door
00-230-3395
Aircraft Skin
Used on aircraft,s-3a.
00-230-3400
Aircraft Skin
Used on aircraft,f-14.
00-230-3402
Aircraft Skin
Used on aircraft,f-14.
00-230-3403
Aircraft Skin
Used on aircraft,f-14.
00-230-3404
Aircraft Skin
Used on aircraft,f-14.
00-230-4911
Aircraft Boom
00-230-4913
Aircraft Bulkhead
00-231-1521
Access Aircraft Door
00-231-1522
Aircraft Skin
Used on aircraft,a-6.
00-231-1524
Access Aircraft Cover
0.196" hole diameter anodize surface treated
00-231-1525
Access Aircraft Cover
00-231-2600
Access Aircraft Cover
Used on 62302329979. 11.500" outside diameter
00-231-2707
Outer Wing Section
00-231-2708
Outer Wing Section
00-231-2710
Aircraft Window Panel
Glass, mil-g-1366, 13.360 in. lg, 12.340 in. w, 0.750 in. thk
00-231-2716
Aircraft Former
Nuclear hardness item
00-231-4674
Wing Section Center Rib
00-231-4678
Structural Component Air Fitting
00-231-4683
Structural Component Air Bracket
Alluminum alloy, qq-a-200/11
00-231-4755
Aircraft Skin
00-231-7661
Aircraft Channel
3.875" overall width
00-231-7897
Exhaust Pipe
Used on hu16 aircraft.
00-231-9167
Structural Aircraft Plate
00-231-9187
Aircraft Pylon
00-231-9189
Aircraft Beam
Matl: aluminum alloy
00-231-9206
Access Aircraft Cover
00-231-9210
Aircraft Channel
00-231-9228
Structural Aircraft Panel
Used on aircraft model kc135. aluminum alloy, qq-a-250/5, alloy alclad 2024, T3
00-231-9229
Structural Aircraft Panel
Used on aircraft model kc135. aluminum alloy, qq-a-250/5, alloy alclad 2024, T3
00-231-9245
Aircraft Former
00-231-9629
Aircraft Pylon
00-232-1746
Structural Component Air Support
00-232-1762
Structural Component Air Support
00-232-1771
Structural Component Air Support
00-232-3484
Structural Aircraft Plate
0.433" overall length temp comdition T4, outer dia; o.433 in. min, 0.435 in. max
00-232-4082
Wing Section Center Rib
00-232-4084
Structural Component Air Support
Used on f-4c acft. kmatl al alloy, 7075-T73; first leg lg 1.370 in.; second leg lg 1.711 in.; 0.3750 in. od; distance from center to center 1.000 in.; 0.190 in. od; 0.2500 in. od; opposite to p/n 53-140055-4; used on pinion support
00-232-4086
Structural Component Air Bracket
00-232-4107
Aircraft Skin
00-232-4257
Structural Component Air Support
Used on acft model f4. matl code 356-T6 per mms-132 sc, left hand, used on hyd swivel, actuator t.e., flap inner wing
00-232-4258
Structural Component Air Support
Used on acft model f4. matl code 356-T6 per mms-132 sc, right hand, used on hyd swivel, actuator, flap t.e. inner wing
00-232-4608
Bell Crank
0.250" bore diameter
00-232-6618
Access Aircraft Cover
Used on u-21 aircraft. 0.250" hole diameter
