00-703-0293
Aircraft Skin
Used on acft model kc-135.
00-703-0298
Structural Component Air Support
Used on aircraft model c135k.
00-703-0314
Aircraft Skin
Used on aircraft,kc-135. 56.000" overall length 14.000" overall width
00-703-0463
Aircraft Skin
00-703-0605
Structural Component Air Bracket
00-703-0606
Structural Component Air Bracket
00-703-0878
Thermal Special Purpo Insulation
T-33
00-703-2307
Structural Aircraft Panel
00-703-2787
Attachment Molded Tank Flange
00-703-2788
Attachment Molded Tank Flange
0.280" hole diameter
00-703-2791
Attachment Molded Tank Flange
0.280" hole diameter
00-703-2801
Attachment Molded Tank Flange
0.230" hole diameter
00-703-2803
Attachment Molded Tank Flange
0.280" hole diameter
00-703-2804
Attachment Molded Tank Flange
0.280" hole diameter
00-703-2806
Attachment Molded Tank Flange
00-703-2808
Attachment Molded Tank Flange
0.280" hole diameter
00-703-2809
Attachment Molded Tank Flange
00-703-2810
Attachment Molded Tank Flange
00-703-2811
Attachment Molded Tank Flange
0.280" hole diameter
00-703-3960
Access Aircraft Cover
Used on f-106 aircraft. 0.500" hole diameter
00-703-4303
Structural Component Air Support
Used on b-52 aircraft. fitting, wing trailing edge flap track ribs lug hinge
00-703-4304
Structural Component Air Support
Used on b-52 aircraft. fitting, wing trailing edge flap track ribs lug hinge
00-703-5922
Access Aircraft Cover
00-703-5956
Structural Component Air Support
00-703-5993
Structural Component Air Bracket
00-703-6785
Access Aircraft Cover
0.189" hole diameter
00-703-7275
Aircraft Fairing
00-703-9721
Access Aircraft Cover
0.306" hole diameter
00-703-9762
Structural Component Air Bracket
Bracket assy, tank pilot valve
00-703-9765
Fluid Aircraft Manifold
Model f-104
00-704-0169
Structural Aircraft Panel
00-704-0683
Filler Opening Cap
00-704-0865
Longeron
Aluminum alloy, 2024-0, qq-a-250/5;
00-704-0972
Thermal Special Purpo Insulation
T-33
00-704-1204
Access Aircraft Door
00-704-1205
Access Aircraft Door
00-704-1675
Aircraft Beam
15.750" overall length 1.460" material thickness
00-704-1676
Aircraft Beam
15.750" overall length 1.460" material thickness
00-704-1686
Structural Component Air Support
00-704-1755
Aircraft Fairing
Manufacturer suggested name - ventral fin installation
00-704-1839
Access Aircraft Door
00-704-2030
Aircraft Channel
00-704-2031
Aircraft Channel
00-704-2032
Structural Aircraft Plate
86.000" overall length 6.000" overall width 0.040" material thickness manufacturer suggested name - glass retainer windshield, aft; nha 4011701
00-704-2034
Aircraft Former
