01-474-2756
Aircraft Fairing
Used on westland gwhl-64 helicopter. fairing assembly, tail rotor drive shaft
01-474-2757
Aircraft Fairing
Used on westland gwhl-64 helicopter. fairing assembly, tail rotor drive shaft
01-474-2762
Structural Component Air Support
Used on westland gwhl-64 helicopter. support assembly, transmission access, rh
01-474-2763
Structural Component Air Support
Used on westland gwhl-64 helicopter. support assembly, transmission access, lh
01-474-2767
Aircraft Fairing
Used on westland gwhl-64 helicopter. fairing
01-474-3720
Structural Component Air Support
Used on trainer tio harrier. guard
01-474-3721
Structural Aircraft Plate
Used on harrier gr7. plate, striker
01-474-3743
Structural Aircraft Plate
Used on f/a-18 (hornet).
01-474-4388
Aircraft Latch Assembly
Used on sh-2g(a) seasprite helicopter. 4.050" overall length 0.930" overall width latch assembly - hook width is measured at mounting bushing; latch handle has 15 deg. plus or minus 2 deg. free travel when latched; small latch pinned to handle hooks over pin on side of main hook to hold handle; main hook width is 0.250-0.260 in.
01-474-4412
Aircraft Fairing
Used on sh-2g(a) seasprite helicopter. 24.654" overall length nose gear box two temperature sensors embedded within fiberglass structure of forward fairing for temp. monitoring; socket head cap screws are secured with lockwire; components normally shipped looseunless specifically defined by purchase order; fairing construction thickness 0.100 in. except in areas of temp. sensors, electrical lead wire, flanges, hardware attachment or as specified; assembly consists of fairing assembly, forward, left hand p/n K870302-103; fairing assembly, aft upper, left hand p/n K870302-105;
01-474-4413
Aircraft Fairing
Used on sh-2g(a) seasprite helicopter. 24.654" overall length nose gear box two temperature sensors embedded within fiberglass structure of forward fairing for temp. monitoring; socket head cap screws are secured with lockwire; components normally shipped looseunless specifically defined by purchase order; fairing construction thickness 0.100 in. except in areas of temp. sensors, electrical lead wire, flanges, hardware attachment or as specified; assembly consists of fairing assembly, forward, right hand p/n K870 302-104; fairing assembly, aft upper, right hand p/n K870302-106; fairing assembly, aft lower, right hand p/n K870302-108; station location sta 120.75; opposite of p/n K870302-101
01-474-4414
Structural Aircraft Panel
Used on westland gwhl-64 helicopter. panel, transmission access
01-474-4596
Aircraft Pylon
Used on aircraft item.
01-474-4597
Aircraft Pylon
Used on aircraft item.
01-474-4611
Aircraft Windshield Panel
01-474-5197
Aircraft Skin
Used on f/a-18 (hornet).
01-474-5575
Bleed Air Duct Assembly
01-474-5647
Aircraft Stiffener
Used on trainer,tio harrier gr7.
01-474-5648
Aircraft Skin
Used on trainer t10 harrier. 6.200" overall length 3.500" overall width matl 7075-T6 alclad
01-474-5653
Aircraft Skin
6.200" overall length 3.500" overall width matl 7075-T6 alclad
01-474-5754
Fuselage Aircraft Fairing
Used on oh-58d army helicopter improvement program (ahip) rotary.
01-474-6053
Structural Component Air Support
01-474-6149
Aircraft Pylon
01-474-6471
Structural Component Air Bracket
Used on trainer, gr7/tio harrier.
01-474-6610
Structural Aircraft Plate
0.197" material thickness part name assigned by controlling agency; auxiliary lox armor, base, axi
01-474-6897
Structural Component Aircr Patch
Plug patch, patch-repair cmrbit o/a dia 5.000 by 3.000 by 0.250 inch dia, consists of skin patch 5.000 inch dia
01-474-6898
Structural Component Aircr Patch
01-474-6899
Structural Component Aircr Patch
01-474-6900
Structural Component Aircr Patch
Plug patch, patch-repair cmrbit o/a dia 5.000 by 3.000 by 0.500 inch dia, consists of skin patch 5.000 inch dia
01-474-6901
Structural Component Aircr Patch
Plug patch, patch-repair cmrbit o/a dia 7.000 by 5.000 by 1.250 inch dia, consists of skin patch 7.000 inch dia
01-474-6902
Structural Component Aircr Patch
Plug patch, patch-repair cmrbit o/a dia 5.000 by 3.000 by 1.250 inch dia, consists of skin patch 5.000 inch dia
01-474-6903
Structural Component Aircr Patch
Plug patch, patch-repair cmrbit o/a dia 7.000 by 5.000 by 0.250 inch dia, consists of skin patch 7.000 inch dia
01-474-6904
Structural Component Aircr Patch
Plug patch, patch-repair cmrbit o/a dia 7.000 by 5.000 by 0.500 inch dia, consists of skin patch 7.000 inch dia
01-474-6905
Structural Component Aircr Patch
01-474-6979
Aircraft Skin
78.000" overall length 7.500" overall width matl: alclad sh, alloy 2024-0, heat treat al aly per ST0111LA0009 to temper T62; opposite -013; dimensions listed are stock size
01-474-6998
Access Aircraft Cover
01-474-7001
Access Aircraft Cover
Used on F/A18E.
01-474-7004
Access Aircraft Cover
Used on F/A18E.
01-474-7017
Structural Aircraft Panel
Cover assy, dorsal aircraft access
01-474-7018
Aircraft Skin
Used on f/a18-e/f. 19.750" overall length 14.187" overall width cover, access, aircraft (navy) ; cover, wing access - lex (drawing name) includes skin assembly 1; support 1; bulb seal 1; nut 8; bolt 8
01-474-7021
Aircraft Pylon Section
Used on predominant application to f-18 e/f. cover, access, aircraft bru dummy cover assy
01-474-7023
Aircraft Pylon Section
Used on predominant application to f-18 e/f. cover, aircraft, mate bru cover
01-474-7024
Access Aircraft Cover
Used on F/A18E.
01-474-7025
Access Aircraft Cover
Used on F/A18E.
01-474-7026
Access Aircraft Cover
Used on f18 e/f fighter aircraft. 3.980" outside diameter cover, center line pivot-external fuel tank
01-474-7030
Access Aircraft Cover
01-474-7031
Access Aircraft Cover
01-474-7033
Access Aircraft Cover
Used on f/a-18e/f aircraft. 0.255" hole diameter item appears (side view) like a toboggan sled, with uneven thickness throughout (due to layers of plies (from 14 ply at 0.109" thichk to 36 plies at 0.281" thick
01-474-7034
Access Aircraft Cover
Used on f/a-18e/f aircraft. 0.255" hole diameter item appears (side view) like a toboggan sled, with uneven thickness throughout (due to layers of plies (from 14 ply at 0.109" thichk to 36 plies at 0.281" thick
01-474-7035
Structural Aircraft Panel
