01-246-1629
Movable Canopy
NHA16K2500-1; includes cover, frame, latch, hinge, linkage, seal, fairing, handle
01-246-1653
Aircraft Door
Used on C-5.
01-246-1881
Structural Component Air Support
0.310" material thickness
01-246-1882
Structural Aircraft Panel
Aluminum alloy, qq-a-200/11, alloy 7075, T6511 or qq-a-225/9, alloy 7075, T651; plastic, epoxy
01-246-2076
Structural Component Air Support
01-246-2077
Structural Component Air Support
01-246-2187
Structural Aircraft Plate
Aluminum alloy 2024-0 sheet qq-a-250/4, matl 0.063 in. thk by 8.500 in. w by 36.000 in. lg
01-246-2188
Structural Aircraft Plate
Aluminum alloy 2024-T81 sheet qq-a-250/5, matl 0.063 in. thk by 2.594 in. w by 16.000 in. lg
01-246-2189
Structural Aircraft Plate
Aluminum alloy 2024-0 qq-a-250/4 sheet, matl 0.090 in. thk by 4.500 in. w by 13.000 in. lg
01-246-2190
Structural Aircraft Plate
Aluminum alloy 2024-0 sheet qq-a-250/4, matl 0.063 in. thk by 8.500 in. by 36.000 in. lg
01-246-2191
Structural Aircraft Plate
Aluminum alloy 2024-T81 sheet qq-a-250/5, matl 0.063 in. thk by 2.594 in. w by 16.000 in. lg
01-246-2192
Structural Aircraft Plate
Aluminum alloy 2024-0 qq-a-250/4 sheet, matl 0.090 in. thk by 4.500 in. w by 13.000 in. lg
01-246-2200
Wing Rib
9.000" overall length 3.250" overall width 3.000" material thickness
01-246-2201
Wing Rib
10.094" overall length 5.141" overall width 0.032" material thickness
01-246-2202
Aircraft Skin
18.000" overall length 10.703" overall width
01-246-2203
Aircraft Skin
18.000" overall length 10.703" overall width
01-246-2271
Structural Aircraft Panel
Used on ah-64 airframe, rotary wing aircraft.
01-246-2307
Aircraft Spar
01-246-3169
Structural Aircraft Panel
01-246-3292
Structural Component Air Support
Width 2.00 in., bend 55 degree angle, 1 hole in straight side 1/4 in., 2 holes in curve 5/32 in.
01-246-3305
Wing Rib
9.797" overall length 3.250" overall width 0.032" material thickness
01-246-3306
Wing Rib
9.797" overall length 3.250" overall width 0.032" material thickness
01-246-3307
Aircraft Skin
8.797" overall length 6.344" overall width
01-246-4029
Structural Component Air Support
Used on f-4 aircraft. steel, l.h. angle
01-246-4033
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; bracket p/o shear beam inboard, fuselage station 626.900 to 712.310
01-246-4034
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; bracket p/o shear beam inboard, fuselage station 626.900 to 712.310
01-246-4463
Structural Component Air Support
01-246-5209
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/4, matl 0.190 in. thk by 1.594 in. w by 7.750 in. lg
01-246-5210
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/5, matl 0.190 in. thk by 1.125 in. w by 7.750 in. lg
01-246-5211
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/4, matl 0.190 in. thk by 1.594 in. w by 7.750 in. lg
01-246-5228
Aircraft Skin
13.000" overall length 3.594" overall width
01-246-5229
Aircraft Skin
17.500" overall length 13.000" overall width
01-246-5231
Aircraft Skin
17.500" overall length 13.000" overall width
01-246-5584
Structural Aircraft Plate
Used on F-15. 17.750" overall length 1.960" overall width 0.040" material thickness strap
01-246-5591
Structural Component Air Support
Used on f-15 aircraft. nha 68A331029
01-246-5604
Aircraft Former
15.630" overall length 3.000" overall width 0.063" material thickness channel; 6al-4v
01-246-5607
Aircraft Skin
Used on F-15. 19.300" overall length 18.410" overall width type 3, comp c annealed; 6al-4v
01-246-5608
Aircraft Skin
Used on F-15. 19.300" overall length 18.410" overall width type 3, comp c annealed; 6al-4v
01-246-5610
Aircraft Skin
Used on F-15. 122.000" overall length 6.000" overall width
01-246-6036
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/5, matl 0.032 in. thk by 5.500 in. w by 9.641 in. lg
01-246-6038
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/5, matl 0.032 in. thk by 5.500 in. w by 9.641 in. lg
01-246-6040
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-250/5, matl 0.032 in. thk by 2.922 in. w by 7.109 in. lg
01-246-6427
Fuselage Aircraft Fairing
Used on aircraft model f-18. kevlar 49/epoxy laminate per mfg spec mms 525, type 2;
01-246-6429
Fuselage Aircraft Fairing
Used on aircraft model f-18. kevlar 49/epoxy laminate per mfg spec mms 525, type 2;
01-246-6430
Fuselage Aircraft Fairing
Used on aircraft model f-18. kevlar 49/epoxy laminate per mfg spec mms 525, type 2;
01-246-6431
Wing Aircraft Fairing
Used on aircraft model av-8. cognizant service:navy;
01-246-6433
Structural Component Air Support
Used on aircraft model av-8.
01-246-6434
Structural Component Air Support
Used on aircraft model av-8.
01-246-6435
Structural Component Air Support
Used on aircraft model av-8.
01-246-6436
Structural Component Air Support
Used on aircraft model av-8.
