00-125-5660
Structural Component Air Bracket
4.063" overall length 3.500" overall width
00-125-5991
Structural Component Air Bracket
00-125-6016
Aircraft Skin
Aluminum alloy, qq-a-250/4, comp 2024, temper T81, 0.125 in. thk
00-125-6026
Structural Component Air Bracket
56.343" overall length 5.093" overall width
00-125-6060
Structural Component Air Bracket
Used as: rudder bracket assy
00-125-6075
Structural Component Air Bracket
2.688" overall length 2.500" overall width u/a: rudder hinge bracket asy, bracket incl:2 mounting holes 0.218 dia, 2 mounting holes 0.197 dia, 1 opening 0.563 dia, 1 bearing p/n AN200K4 included
00-125-6097
Structural Component Air Bracket
3.250" overall length 0.875" overall width 1.000" material thickness u/a: anti drag ring bracket; bracket incl: 1 hole 0.197 dia, 1 hole 0.128 dia, 4 holes 0.098 dia; make from steel
00-125-6103
Structural Component Air Bracket
4.562" overall length 1.688" overall width 0.625" material thickness u/a: mechanical latch bracket; bracket incl: 2 holes 0.197 dia, 4 holes 0.098, 6 holes threaded 8-32NC2b
00-125-6132
Structural Component Air Bracket
U/a:bracket asy, fuel flowmeter
00-125-6195
Structural Component Air Bracket
U/a: bracket assy, propeller, make from aluminum alloy
00-125-6198
Structural Component Air Bracket
13.812" overall length u/a bracket, cowling; bracket matl:tubing per mil-t-6736, plate per mil-s-18729 cond n
00-125-6264
Structural Component Air Bracket
5.563" overall length 4.000" overall width 1.103" material thickness u/a bracket, astro comp
00-125-6707
Aircraft Door
Used on C-47.
00-125-7123
Aircraft Fairing
Used on aircraft model f-14a.
00-125-7475
Structural Component Air Support
U/a: adapter, anchor cable
00-125-7478
Structural Component Air Bracket
11.500" overall length 1.500" overall width 0.750" material thickness
00-125-7480
Access Aircraft Door
00-125-7481
Aircraft Pylon
U/a: pylon assy, pedal control
00-125-7482
Access Aircraft Cover
00-125-7484
Aircraft Skin
58.000" overall length 56.000" overall width
00-125-8000
Aircraft Skin
Used on aircraft,f-15.
00-125-8001
Aircraft Skin
Used on aircraft,f-15.
00-125-8866
Supplemental Small Arms-fr Armor
Used on oh-58d ahip (army helicopter improvement program), rotary wing aircraft.
00-125-8869
Supplemental Small Arms-fr Armor
00-125-8896
Aircraft Fairing
Used on ah-1s acft.
00-125-8898
Fuselage Section
Aluminum alloy, qq-a-250/5, comp 2024, temper T3
00-125-9385
Aircraft Engine Build- Parts Kit
00-125-9392
Aircraft Engine Build- Parts Kit
00-126-1114
Aircraft Leading Edge
119.750" overall length 0.091" material thickness
00-126-1987
Aircraft Window Panel
00-126-2526
Access Aircraft Cover
Used on oh-58a/c helicopter. 0.190" hole diameter oxide film surface treated
00-126-3330
Aircraft Tip
Used on aircraft model a4.
00-126-4069
Access Aircraft Door
00-126-4070
Access Aircraft Door
00-126-4245
Access Aircraft Door
00-126-4246
Access Aircraft Door
00-126-4369
Supplemental Small Arms-fr Armor
Used on goh-58d ahip (army helicopter improvement program), rotary wing aircraft.
00-126-4388
Supplemental Small Arms-fr Armor
00-126-4421
Aircraft Window Panel
Used on helicopter observation and trainer.
00-126-4426
Aircraft Window Panel
Used on oh-58d helicopter.
00-126-4435
Fuselage Section
Assembly of honeycomb panels forming forward lower sect of fuselage;
00-126-5633
Structural Aircraft Panel
66.210" overall length 27.330" overall width plastic polyuethane foam core fscm 21213
00-126-5636
Structural Aircraft Panel
64.100" overall length 29.650" overall width fiberglass inner
00-126-5637
Structural Aircraft Panel
54.560" overall length 29.650" overall width glass cloth laminate, polyurethane foam covered 54.560 in.lg 29.650 in. w 6 ea 0.420 in. min, 0.450 in. max dia mtg holes
00-126-5638
Structural Aircraft Panel
63.900" overall length 29.650" overall width w/cloth laminate, polyurethane foam cover; manufacturer suggested name - panel assembly-trim, overhead, rh side, troop/courier compt, fs 927 to 990; nha 4E20012
00-126-5639
Structural Aircraft Panel
54.560" overall length 29.150" overall width laminated glass cloth, polyurethane foam covered 54.560 in.lg, 29.150 in.w
00-126-5641
Structural Aircraft Panel
63.150" overall length 36.900" overall width fiberglass inner
00-126-5642
Structural Aircraft Panel
49.500" overall length 36.900" overall width fiberglass inner
00-126-5643
Structural Aircraft Panel
79.000" overall length 37.350" overall width fiberglass, inner
00-126-5644
Structural Aircraft Panel
67.500" overall length 37.350" overall width plastic polyurethane foam core fscm 21213
