00-909-8485
Structural Aircraft Panel
26.487" overall length 10.661" overall width
00-909-8486
Structural Aircraft Panel
23.739" overall length 11.770" overall width
00-909-8487
Structural Aircraft Panel
23.379" overall length 11.770" overall width
00-909-8488
Structural Aircraft Panel
35.563" overall length 11.610" overall width
00-909-8489
Structural Aircraft Panel
35.563" overall length 11.610" overall width
00-909-8718
Aircraft Fairing
00-909-8921
Thermal Special Purpo Insulation
00-909-8922
Thermal Special Purpo Insulation
00-909-8952
Thermal Special Purpo Insulation
00-909-9024
Bell Crank
0.766" bore diameter
00-909-9055
Airfoil Rib
6.006" overall length 2.070" overall width
00-909-9249
Aircraft Fairing
18.610" overall length
00-909-9250
Structural Aircraft Panel
22.100" overall length 13.750" overall width
00-909-9251
Structural Aircraft Panel
22.100" overall length 13.750" overall width
00-909-9264
Access Aircraft Door
Used on c-141 aircraft.
00-909-9265
Structural Aircraft Panel
00-909-9266
Structural Aircraft Panel
00-909-9267
Structural Aircraft Panel
00-909-9268
Structural Aircraft Panel
00-909-9269
Structural Aircraft Panel
00-909-9270
Structural Aircraft Panel
00-909-9774
Lubricating Oil Aircraft Tank
00-909-9927
Access Aircraft Door
00-910-0345
Structural Component Air Fitting
00-910-1944
Structural Aircraft Panel
00-910-1945
Thermal Insulation Pipe Covering
Acft c-141
00-910-1947
Structural Aircraft Panel
00-910-1962
Structural Component Air Support
Steel 4130 per mil-s-6758, condition F4; 2.550 in. lg, 1.110 in. w, 0.730 in. thk; base 0.120 in. thk; 2 0.156 in. dia mounting holes in base; 2 inline 0.313 in. dia holes perpendicular to mounting holes; used on forward entrance door uplock
00-910-2688
Aircraft Former
Used on helicopter,ch-47. 19.600" overall length 6.600" overall width 0.025" material thickness
00-910-3873
Aircraft Door
Used on ch-47 helicopter,cargo-tr.
00-910-5537
Aircraft Leading Edge
00-910-5543
Aircraft Leading Edge
00-910-6229
Wing Landing Flap
00-910-6230
Wing Landing Flap
00-910-6231
Aircraft Skin
Titanium alloy, AMS4910
00-910-6232
Aircraft Skin
40.000" overall length 28.000" overall width
00-910-6928
Structural Aircraft Plate
0.019" material thickness
00-910-7259
Aircraft Floor
00-910-7260
Structural Aircraft Panel
With fabric, polyester, single ply facing no. 120, triple ply body no. 181, type 4, grade b, class 2
00-910-7655
Aircraft Spar
Used on acft model f-4.
00-910-7656
Horizontal Stabilizer Spar
Titanium alloy, AMS4911, condition 6al-4v annealed;
00-910-7939
Aircraft Pylon
00-910-7940
Aircraft Pylon
00-910-8601
Structural Aircraft Panel
00-910-8602
Structural Aircraft Panel
00-910-8871
Aircraft Fairing
00-910-9087
Fuel Tank Parts Kit
Used on f-4 aircraft.
00-910-9092
Structural Component Air Support
Aluminum alloy, qq-a-596, 9.000 in. lg, 5.550 in. w, 3.750 in. h, 0.503 in. min, 0.511 in. max dia hole thru 8 places
00-910-9095
Aircraft Bulkhead
4.230" overall length 25.070 in. o.d.
