01-504-6364
Structural Aircraft Panel
Panel assy, stair tread-crew door c/o 1 guard, -3, stocksize 33X4x.032) , AL6061; 1 panel, -5, 11X33 (make FROM9D0059-4a) ; 9 insert plugs, p/n 9D0057-38400; 1 mat, p/n 17P1A4668-11, stocksize 8X30, deck covering non-skid cloth, DMS2377 type 2; 2 plates, 2X8x.032, AL6061 sheet, p/n -21; 5 insert, p/n 9D0057-38450; 14 insert sleeve, p/n 9D0119-3-2; heat treat 6; nha 17P1A4604
01-504-6365
Structural Aircraft Panel
9.900" overall length 9.500" overall width rudder assy-vertical stablizer anodize per PS13201 TYPE2 class 1; heat treat to cond T62 per PG15534; dim are stock material
01-504-6366
Structural Aircraft Panel
16.360" overall length 8.000" overall width rudder assy-vertical stablizer anodize per PS13201 TYPE2 class 1; heat treat to cond T62 per PG15534; dim are stock material
01-504-6367
Aircraft Former
3.750" overall length 3.550" overall width 0.040" material thickness formers-rudder closure next higher assembly 68A240001; heat treat to 2024-T62 per 15534
01-504-6370
Structural Aircraft Panel
9.500" overall length 3.600" overall width closure, rudder assy-vertical stabilizer anodize per PS13201 TYPE2 class 1; heat treat to condition T62 per PG15534; dim are stock material
01-504-6376
Aircraft Floor
11.050" overall length 4.760" overall width walkway assy make from LS60373 cond T76511
01-504-6377
Aircraft Floor
11.050" overall length 4.760" overall width walkway assy make from LS60373 cond T76511
01-504-6378
Fuselage Parts Kit
01-504-6380
Structural Aircraft Panel
49.000" overall length 8.000" overall width ramp cover assy dim are stock matl
01-504-6381
Structural Aircraft Panel
49.000" overall length 8.000" overall width ramp cover assy dim are stock matl
01-504-6497
Structural Component Air Support
Support - windshield, attach - forward machined from 74A350611-2006
01-504-6500
Structural Component Air Support
Support - windshield, attach - forward machined from 74A350611-2001
01-504-6595
Structural Component Air Bracket
10.500" overall length 3.600" overall width 0.071" material thickness matl 7075-0 alclad
01-504-6713
Aircraft Window Panel
Used on v-22 tilt rotor aircraft. window panel
01-504-6764
Access Aircraft Cover
Used on mh60s knighthawk. (navy) cover assembly
01-504-6768
Structural Component Air Bracket
Used on mh60s knighthawk. (navy) bracket
01-504-6771
Access Aircraft Cover
Used on mh60s knighthawk. (navy) cover assembly
01-504-6772
Structural Component Air Bracket
Used on mh60s knighthawk. (navy) bracket
01-504-6778
Wing Landing Flap
Used on mh60s knighthawk. (navy) flap assembly
01-504-6779
Structural Component Air Bracket
Used on mh60s knighthawk. (navy) bracket assembly
01-504-7130
Structural Aircraft Plate
Used on c130k aircraft. lower cap, bulkhead-cargo fus sta 717.0
01-504-7375
Aircraft Former
4.750" overall length 4.400" overall width 0.040" material thickness formers-rudder closure next higher assembly, 68A240001, u/o f-15a, b, c, d, e; heat treat to 2024-T62 per PS15534; dim are stock material
01-504-7376
Aircraft Former
4.600" overall length 4.190" overall width 0.040" material thickness formers-rudder closure next higher assembly, 68A240001, u/o f-15a, b, c, d, e; heat treat to 2024-T62per PS15534; dim are stock material
01-504-7377
Wing Landing Flap
Inbd flap/inbd trlg edge panel eff. from 17A071-184; c/o 3 spar assy; 10 rib assy; 2 skin assy; 1 channel assy; 2 support assy; 2 plugs; 10 angles; 2 rub strips; polyglass/satin cloth, composition matl. carbon fiber epoxy resin impregrated; dms 2224, type 1 class w, grade 5; misc. hardware; nha 17P6-5601-503
01-504-7378
Aircraft Floor
42.800" overall length 5.900" overall width walkway make from LS60373 cond T76511
01-504-7381
Aircraft Former
62.000" overall length 5.000" overall width 0.020" material thickness former assy, aft eng. mount nha 17P7W3103-9; ams 5529 CRES17-ph cold finish sheet; dimensions stocksize
01-504-7382
Aircraft Former
62.000" overall length 5.000" overall width 0.020" material thickness former assy, aft. eng. mount nha 17P7W3103-9; CRES17-ph cold fin.sheet; dim.stocksize
01-504-7752
Structural Component Air Fitting
Used on f/a-22 raptor. fitting assembly this dash number was removed from the drawing
01-504-7753
Structural Aircraft Panel
Used on f/a-22 raptor. 15.000" overall length 8.000" overall width cover, blank-dlt antenna
01-504-7760
Structural Aircraft Panel
Panel assy, stair tread - crew door c/o 1 guard, stock size .032X4X33; 1 panel (make from 9D0059-4a) ; 1 mat, deck covering non-skin cloth, 4 plugs, 14 insert plugs; heat treat T6
01-504-7783
Aircraft Hinge
Used on f/a18e/f. 3.090" overall length hinge assy, upper-vertical stabilizer dia of hinge holes are 0.376 in (after installation of bushings) ; 2 unthreaded mounting holes dia are 0.530 in,
01-504-7892
Structural Component Air Bracket
01-504-8128
Aircraft Window Panel
01-504-8205
Structural Component Air Bracket
01-504-8231
Access Aircraft Door
Door, access-video tape cartridge
01-504-8340
Structural Aircraft Panel
01-504-8458
Aircraft Fairing
Used on sh-2g seasprite. fairing assy, weapons pylon, nose
01-504-8459
Aircraft Fairing
Used on sh-2g seasprite. fairing assy, weapons pylon
01-504-8482
Aircraft Scoop
01-504-8555
Structural Component Air Support
01-504-8888
Canopy Transparency
Used on v-22 tilt rotor aircraft. transparency, canopy as differentiated by the source control drawing.
01-504-8913
Structural Component Air Support
Used on mv-22 osprey tilt rotor aircraft. (navy) pan assy, fuel-air contractor supported item for navicp phil consummable
01-504-8918
Access Aircraft Door
Used on mv-22 tilt rotor aircraft. (navy) door assy, air, aircr fuel
01-504-8920
Structural Component Air Support
Used on mv-22 osprey tilt rotor aircraft. (navy) pan assy, fuel-air contractor supported item for navicp phil consummable
01-504-8921
Access Aircraft Door
Used on mv-22 tilt rotor aircraft. (navy) door assy, fuel, aircr fuel
01-504-8922
Fuselage Section
Used on mv-22 osprey tilt rotor aircraft. (navy) vent manifold assy contractor supported item for navicp phil consummable; sponson fwd fuel cell installation
01-504-9207
Structural Component Air Support
Used on l-1011 tristar.
01-504-9208
Structural Component Air Support
Used on l-1011 tristar.
01-504-9209
Structural Component Air Support
Used on l-1011 tristar.
01-504-9210
Structural Component Air Support
Used on l-1011 tristar.
