01-505-0870
Structural Component Air Support
Clevis support, latch fwd & aft pylon opposite A02S8079-9
01-505-0872
Structural Component Air Support
Clevis support, latch fwd & aft pylon opposite A02S8079-13
01-505-0876
Structural Aircraft Plate
01-505-0877
Structural Component Air Support
Clevis support, latch fwd & aft pylon
01-505-0878
Structural Component Air Support
Clevis support, latch fwd & aft pylon
01-505-0886
Structural Aircraft Plate
01-505-0926
Structural Aircraft Panel
Inlet cowl outer repair skin mat'l is bare sheet
01-505-0928
Structural Component Air Bracket
2.800" overall length 1.600" overall width 0.040" material thickness bracke-u-bolt nha 204-70045; u/o e-3a; finish per-8.07+srf 12.206
01-505-0934
Aircraft Windshield Panel
Windshield controled interchangeable assembly, -501, -502, -507, -508; -507 is opp
01-505-0938
Aircraft Windshield Panel
Windshield controled interchangeable assembly, -501, -502, -507, -508; -508 opp
01-505-1046
Structural Component Air Fitting
Used on f/a-22 raptor. fitting assembly per drawing 5HF42714-117 is removed
01-505-1049
Structural Component Air Bracket
Used on f-22a raptor. 5.000" overall length 1.000" overall width 0.080" material thickness bracket, assembly of dim. are stock material; m/f: 2024-T81 alum sht; c/o: -135 bracket, LK204F3 nut,
01-505-1145
Structural Component Air Fitting
12.700" overall length 5.000" overall width 3.200 " material thickness cam support make from 5-88728-1; opp make from 7075-01 heat treat to T73; dim are stock matl; the -1 is opp
01-505-1150
Structural Component Air Fitting
Finnish F2.5
01-505-1154
Structural Component Air Fitting
Finnish F2.5
01-505-1186
Structural Aircraft Plate
01-505-1211
Aircraft Bulkhead
01-505-1243
Structural Component Air Bracket
01-505-1270
Structural Component Air Bracket
01-505-1282
Structural Component Air Bracket
01-505-1284
Aircraft Windshield Panel
Windshield assy, pane number 3, pilots
01-505-1289
Aircraft Windshield Panel
Windshield assy, pane number 3, pilots
01-505-1295
Structural Component Air Bracket
01-505-1457
Aircraft Door
Heat treat zero; c/o 1 door (p/n 17P6N1026-8) , stock size .100X8.0X21.0; 4 angle's
01-505-1458
Structural Aircraft Panel
Panel instl-struc.outbd te, flap asame as -504 excep ecn shown; NHA17N6P0639-535; effectivity 17A067-184; c/o 1 doubler, stocksize .125 x 4 X5; 14 shim, stocksize .065x 1.25 x 12, 1 shim .065 x 1.5 x 9, 1 te assy; misc. hardware
01-505-1459
Structural Aircraft Plate
62.000" overall length 2.000" overall width 0.032" material thickness fence NHA17P2A3940; heat treat 0; sheetalclad; dimensions are stocksize
01-505-1460
Structural Aircraft Plate
62.000" overall length 2.000" overall width 0.032" material thickness fence nha 17P2A3940; heat treat 0; sheet alclad; dimensions are stocksize
01-505-1461
Structural Aircraft Plate
62.000" overall length 2.000" overall width 0.032" material thickness fence nha 17P2A3940; heat treat 0; sheet alclad; dimensions are stocksize
01-505-1589
Aircraft Window Panel
Window assy, pane number 4, pilots
01-505-1595
Aircraft Window Panel
Window assy, pane number 4, pilots
01-505-1800
Structural Component Air Fitting
Used on NIMROD. 1.388" overall length lee hi-bar screen in fitting, special passivate surface treated
01-505-1825
Aircraft Pylon
Used on apache attack helicopter.
01-505-1833
Structural Component Air Support
Used on chinook helicopter. bonded assembly
01-505-1907
Radome
Used on f/a-22 raptor.
01-505-1911
Aircraft Rudder
Used on f-22 raptor. rudder, aircraft
01-505-1912
Aircraft Fairing
Used on f/a-22 raptor. 102.000" overall length c/o 1 (-103 seal, 102.000 in., matl. rubber; 1 (-105 seal, 106.000 in., matl. rubber) , 1 fairing, outbd (5HW02261-123, made of glass/phenolic honeycomb core, 3/16 5.5 pcf) ;
01-505-1913
Aircraft Fairing
Used on f/a-22 raptor. 73.440" overall length fairing inboard-vertical stabilizer, assembly of
01-505-1914
Aircraft Fairing
Used on f-22 raptor. fairing, outboard-vertical stabilizer, assembly of xconsists of 1 each 5HW02161-104
01-505-1915
Aircraft Rudder
Used on f-22 raptor. rudder, aircraft
01-505-1916
Aircraft Fairing
Used on f/a-22 raptor. fairing
01-505-1928
Aircraft Channel
36.000" overall length heat treat T0, u/o -1, -3, -133, -137, -145
01-505-1929
Aircraft Fairing
30.000" overall length 5.000" overall width 0.063" material thickness fairing dimensions are stocksize; heat treat 0
01-505-1931
Structural Aircraft Plate
62.000" overall length 1.900" overall width 0.032" material thickness fence, fwd outbrd maingear door alclad sheet; heat treat 3; dimensions are stocksize; effectivity from 17A007-020; nha 17P2A9930
01-505-2019
Fuselage Parts Kit
Used on a-37 acft. kit modifies; plyon tank, tip tank, fuel cell no.7, fuel cell no.6, fuel cell no.5, fuel cell no.4, fuel cell no.3, fuel cell no.2, fuel cell no.1
01-505-2045
Aircraft Skin
Outer skin
01-505-2049
Aircraft Skin
Outer skin
01-505-2053
Structural Aircraft Panel
01-505-2057
Structural Component Air Bracket
01-505-2064
Structural Component Air Bracket
01-505-2077
Vertical Stabilizer
