00-611-9346
Access Aircraft Cover
00-611-9347
Aircraft Truss Assembly
00-611-9348
Fuselage Section
00-611-9352
Structural Aircraft Panel
Used on C-130. impregnated paper, honeycomb core with laminated fiber glass facing
00-611-9353
Structural Aircraft Panel
Used on C-130. impregnated paper, honeycomb core with laminated fiber glass facing
00-611-9354
Structural Aircraft Panel
28.120" overall length 19.649" overall width
00-611-9367
Aircraft Trailing Edge
C/o skin 1 ea p/n 370626-2r, skin 1 ea p/n 370626-3r, strip 1 ea p/n 370626-4, rib 2 ea p/n 370634-1r, rib 1 ea p/n 370633-1l, rib 4 ea p/n 370633-1r
00-611-9368
Aircraft Trailing Edge
C/o skin 1 ea p/n 370626-2l, skin 1 ea p/n 370626-3l, strip 1 ea p/n 370626-4, rib 2 ea p/n 370634-1l, rib 4 ea p/n 370633-1l, rib 1 ea p/n 370633-1
00-611-9373
Thermal Special Purpo Insulation
00-611-9386
Thermal Insulation Pipe Covering
00-611-9387
Thermal Insulation Pipe Covering
00-611-9388
Thermal Insulation Pipe Covering
00-612-1870
Access Aircraft Cover
00-612-2568
Access Aircraft Cover
0.250" hole diameter
00-612-2595
Structural Component Air Support
Used on acft model f106. made from rough forging cres type A286, ams 5735
00-612-2597
Access Aircraft Cover
0.228" hole diameter
00-612-3513
Structural Component Air Bracket
1.880" overall length 1.000" overall width 1.060" material thickness
00-612-4115
Access Aircraft Cover
Used on c-130 aircraft.
00-612-4116
Access Aircraft Cover
Used on c-130 aircraft. 0.313" hole diameter
00-612-4120
Structural Aircraft Panel
Used on C-130. 59.650" overall length 15.850" overall width honeycomb material
00-612-4130
Aircraft Door
Used on C-130.
00-612-4137
Thermal Insulation Pipe Covering
00-612-4597
Aircraft Door
00-612-4598
Aircraft Door
00-612-4893
Access Aircraft Door
Spring loaded self-closing
00-612-4943
Aircraft Door
00-612-4944
Aircraft Door
00-612-4965
Remote Control Lever
1.000" bore diameter clevis link end, securing hole (s) shaft end
00-612-5469
Access Aircraft Cover
00-612-5544
Access Aircraft Cover
Used on t-2 aircraft. 0.189" hole diameter
00-612-7068
Trim Aileron Tab
Aluminum alloy, qq-a-250/5, composition 2024, temper T3;
00-612-7224
Aircraft Channel
00-612-8047
Aircraft Leading Edge
00-612-8048
Aircraft Leading Edge
00-612-8050
Aircraft Door
Used on C-130.
00-612-8062
Structural Aircraft Panel
Used on C-130. impregnated honeycomb core with laminated fiber glass facing
00-612-8064
Structural Aircraft Panel
Used on C-130. impregnated paper, honeycomb core with laminated fiber glass facing
00-612-8065
Structural Aircraft Panel
Used on C-130. impregnated paper, honeycomb core with laminated fiber glass facing
00-612-8066
Structural Aircraft Panel
Used on C-130. impregnated paper, honeycomb core with laminated fiber glass facing
00-612-8067
Structural Aircraft Panel
Used on C-130. impregnated paper, honeycomb core with laminated fiber flass facing
00-612-8068
Access Aircraft Cover
0.331" hole diameter
00-612-8080
Structural Component Air Support
00-612-8096
Structural Component Air Support
Aluminum alloy, qq-a-225/6, 2.200 in. lg, 1.400 in. w, 1.020 in. h, 4 holes 0.221 in. dia, 2 holes 0.189 in. dia
00-612-8958
Access Aircraft Cover
00-612-8998
Aircraft Fairing
0.032" material thickness
00-612-9237
Aircraft Truss Assembly
00-612-9238
Aircraft Truss Assembly
00-612-9239
Aircraft Truss Assembly
