00-208-3701
Structural Component Air Support
16.100" overall length 1.000" overall width
00-208-3707
Structural Aircraft Panel
6.960" overall width
00-208-5296
Aircraft Skin
00-208-9443
Access Aircraft Cover
00-208-9516
Fluid Aircraft Manifold
92.850" overall length 23.000" overall width
00-208-9562
Fluid Aircraft Manifold
29.960" overall length
00-208-9613
Fluid Aircraft Manifold
00-208-9636
Structural Aircraft Plate
Used on f-4 airplane.
00-208-9649
Structural Aircraft Plate
00-208-9807
Structural Aircraft Plate
5.200" overall length 1.800" overall width 0.051" material thickness
00-208-9811
Aircraft Former
00-208-9817
Aircraft Former
00-208-9946
Access Aircraft Cover
00-209-0000
Access Aircraft Door
00-209-0052
Aircraft Floor
35.120" overall length 35.080" overall width
00-209-0053
Stiffener Aircraft Rib
25.260" overall length 1.500" overall width
00-209-3060
Aircraft Leading Edge
41.290 in. canted h, skin forms parabolic shape
00-209-8362
Fuel Aircraft Tank
00-210-6876
Fluid Aircraft Manifold
00-210-6877
Fluid Aircraft Manifold
00-210-7504
Structural Aircraft Plate
Aluminum alloy, qq-a-225/6, 2.000 in. lg, 1.562 in. w, 0.250 in. thk, 5 ea 0.219 in. dia through holes
00-210-7505
Structural Aircraft Plate
Galuminum alloy, qq-a-250/5, 2.938 in. lg, 2.000 in. w, tapered thk, 0.125 in. greater, 0.015 in. lesser thk, 3 edge slots 0.250 in. w 0.625 in. c to c, 1.312 in. deep outside slots, 1.125 in. deep center slot
00-210-7551
Aircraft Floor
Used on aircraft model c5a.
00-210-7582
Structural Component Air Bracket
4.312" overall length 1.671" overall width c/o 1 mold casting, 2 bushing
00-210-7718
Structural Component Air Support
4.250" overall length
00-210-8130
Structural Aircraft Plate
Used on kc-135 straolifter tanker airplane.
00-210-9019
Structural Component Air Support
00-210-9549
Structural Component Air Fitting
U/a tab hinge fitting
00-210-9554
Structural Component Air Bracket
00-210-9559
Structural Component Air Support
4.410" overall length 0.125" material thickness
00-210-9770
Cowling
Used on acft model t-28.
00-210-9778
Structural Component Air Bracket
Bracket, shield, radiation
00-210-9779
Structural Component Air Bracket
U/a: engine control bracket; matl; magnesium alloy; four 0.257in dia mtg holes, spaced on 3.000in by 1.671in mounting centers
00-210-9781
Structural Component Air Support
00-210-9782
Structural Component Air Bracket
U/a: oil dilution solenoid mounting bracket; matl:steel
00-210-9810
Fuel Aircraft Tank
Left hand assembly, located in wing outer panel
00-210-9816
Access Aircraft Door
00-210-9944
Aircraft Speed Brake
00-210-9952
Structural Aircraft Plate
2.250" overall length 1.531" overall width doubler, fuselage panel; slanted slot opening
00-211-0011
Structural Component Air Support
00-211-0184
Center Wing Section
C/o wing assembly, appl to f-86 acft
00-211-0246
Fuel Aircraft Tank
00-211-0247
Fuel Aircraft Tank
00-211-0251
Fuel Aircraft Tank
56.063" overall length
00-211-0252
Fuel Aircraft Tank
51.625" overall length 28.875" overall width conforms to mil-t-5578
00-211-0605
Access Aircraft Cover
Used on f-84 aircraft. cover, assembly, terminal; matl fiber glass
00-212-1228
Structural Component Air Support
T6 temper
00-212-1232
Structural Aircraft Panel
00-212-1762
Aircraft Beam
U/a:closure beam
00-212-1772
Structural Aircraft Plate
Used on f-4 airplane.
