01-035-9782
Aircraft Fairing
01-035-9783
Structural Component Aircraf Web
41.000" overall length 13.500" overall width 0.025" material thickness
01-035-9784
Structural Aircraft Panel
01-035-9785
Structural Aircraft Panel
01-035-9786
Structural Component Air Fitting
01-035-9787
Structural Component Air Fitting
01-035-9788
Access Aircraft Door
Used on e-3a acft.
01-035-9789
Structural Component Air Bracket
01-035-9790
Structural Component Air Fitting
01-035-9791
Structural Aircraft Plate
01-036-0251
Structural Component Air Bracket
01-036-0287
Structural Component Air Support
01-036-0290
Aircraft Rudder
01-036-1335
Structural Aircraft Panel
Used on ta-7c aircraft.
01-036-1337
Longeron
Used on ta-7c aircraft.
01-036-2121
Outer Wing Section
01-036-2876
Aircraft Stiffener
01-036-2877
Aircraft Stiffener
01-036-2878
Aircraft Stiffener
01-036-2879
Aircraft Stiffener
01-036-2880
Aircraft Stiffener
01-036-3185
Structural Component Air Bracket
01-036-3186
Aircraft Channel
45.000" overall length 4.000" overall width 0.050" material thickness dim. are stock material
01-036-3207
Structural Component Air Support
01-036-3230
Structural Component Air Bracket
39.000" overall length 12.000" overall width 4.250" material thickness
01-036-3231
Aircraft Frame
01-036-3232
Structural Aircraft Panel
01-036-3272
Aircraft Fairing
01-036-3273
Structural Component Air Support
Aluminum alloy, qq-a-250/5, 2024, temper 0
01-036-3277
Aircraft Skin
Used on C-141. aluminum 7079, T6, bare; variation of thickness not to exceed 0.012 in.
01-036-4162
Aircraft Stiffener
01-036-4326
Aircraft Door
01-036-4328
Structural Aircraft Panel
01-036-4329
Aircraft Door
01-036-4330
Aircraft Fairing
01-036-4347
Structural Aircraft Panel
Used on ah-1p acft.
01-036-4348
Structural Aircraft Plate
Aluminum alloy qq-a-250/5 2024 temper T3, serrated, 1.750 in. lg, 1.750 in. w, 0.063 in. o/a thk, 4 holes 0.0937 in. dia located 0.250 in. from each corner, 2 slots 0.218 in. w, 0.640 in. lg
01-036-4349
Structural Aircraft Plate
Aluminum alloy qq-a-250/5 2024 temper T3, 1.500 in. ln. w, 0.063 in. o/a thk, 2 holes 0.208 in. min
01-036-4369
Cowling
Aluminum alloy qq-a-250/5 2024 temper T3
01-036-4781
Airframe Modification Kit
Used on uh-1d,h,eh-1h.
01-036-4782
Airframe Modification Kit
Used on uh-1b,c,d,h,m,eh-1h.
01-036-4845
Structural Aircraft Plate
4.250" overall length 0.400" material thickness
01-036-4846
Structural Aircraft Plate
4.250" overall length 0.650" material thickness
01-036-4966
Aircraft Fairing
Used on ah-1 series acft.
01-036-4970
Aircraft Skin
Used on C-141. 328.000" overall length 62.000" overall width matl temp-T6, variation in thicknnot to exceed 0.012 in.
01-036-5024
Fluid Aircraft Manifold
45.980" overall length 3.000" overall width
01-036-5318
Structural Aircraft Panel
Used on ta-7c aircraft.
01-036-5319
Structural Component Air Support
Used on aircraft model f-14a.
01-036-5988
Structural Component Air Support
Titanium mil-t-9046 class 7, o/a lg 64.000 in., 2.000 in. w, 0.020 in. thk, forward firewall assy appl
01-036-5989
Structural Component Air Support
Titanium mil-t-9046 class 7, o/a lg 27.000 in., 1.800 in. w, 0.020 in. thk, right hand retainer design, forward firewall assy appl
