01-234-9146
Aircraft Spar
01-234-9147
Aircraft Spar
01-234-9544
Structural Component Air Support
01-234-9556
Metal Molding
01-235-0051
Structural Component Air Support
01-235-0059
Airfoil Rib
Used on C-130. T4 clad
01-235-0687
Aircraft Door
01-235-0688
Aircraft Door
01-235-0832
Structural Aircraft Plate
Type/model designation:AV8b steel corrosion resisitng 304 qq-s-766 annealed class 304, matl 0.312 in. thk by 4.594 in. w by 5.203 in. lg
01-235-0833
Structural Component Air Support
Type/model designation:AV8b aluminum alloy 7075-0 qq-a-250/13, matl 0.500 in. thk by 6.000 in. w by 8.203 in. lg
01-235-0840
Aircraft Former
01-235-0844
Aircraft Skin
Used on C-141.
01-235-1016
Structural Component Air Support
Used on acft model kc-135. cement per bac 5010 type 49; finish srf-2.115; nha 65-18891
01-235-1017
Structural Component Air Support
Used on acft model b-52. 2024-T4 per qq-a-268, T4 temper; opposite -1929; nha 35-2462
01-235-1026
Aircraft Former
22.000" overall length 3.100" overall width 0.125" material thickness
01-235-1027
Aircraft Former
22.000" overall length 3.100" overall width 0.125" material thickness
01-235-1028
Aircraft Former
22.000" overall length 4.500" overall width 0.125" material thickness
01-235-1029
Aircraft Former
22.000" overall length 3.100" overall width 0.125" material thickness
01-235-1030
Aircraft Former
22.000" overall length 4.300" overall width 0.125" material thickness
01-235-1031
Aircraft Former
22.000" overall length 3.100" overall width 0.125" material thickness
01-235-1032
Aircraft Former
21.000" overall length 3.200" overall width 0.063" material thickness
01-235-1033
Aircraft Former
21.000" overall length 3.200" overall width 0.063" material thickness
01-235-1034
Aircraft Former
21.000" overall length 3.200" overall width 0.063" material thickness
01-235-1035
Aircraft Former
21.000" overall length 3.200" overall width 0.063" material thickness
01-235-1036
Aircraft Former
23.000" overall length 3.200" overall width 0.063" material thickness
01-235-1037
Aircraft Former
30.000" overall length 3.200" overall width 0.063" material thickness nha 65-18891
01-235-1038
Aircraft Former
21.000" overall length 3.300" overall width 0.063" material thickness
01-235-1039
Aircraft Former
21.000" overall length 3.300" overall width 0.063" material thickness
01-235-1040
Aircraft Former
21.000" overall length 3.300" overall width 0.063" material thickness
01-235-1041
Aircraft Former
21.000" overall length 3.200" overall width 0.063" material thickness
01-235-1042
Aircraft Former
21.000" overall length 3.200" overall width 0.063" material thickness
01-235-1068
Attachment Molded Tank Flange
Used on acft model b-52. consist of 1 flange, 2 plug; nha 5-61161, 9-45307, 5-63962, and 29-9576; used on static drain flange assy
01-235-1269
Structural Component Air Support
4.000" overall length 3.000" overall width 0.080" material thickness
01-235-1709
Structural Component Air Support
1.620" overall width
01-235-2305
Structural Aircraft Plate
01-235-2306
Structural Aircraft Plate
Used on C-130. T6 clad
01-235-2307
Structural Aircraft Plate
Used on C-130. T6 clad
01-235-2308
Structural Aircraft Plate
Used on C-130.
01-235-2309
Structural Aircraft Plate
Used on F-15. T81 alclad
01-235-2315
Structural Component Air Support
Used on c-130 acft. tee; p/o bulkhead, ramp forward
01-235-2317
Structural Component Air Support
Used on f-15 acft. engine mount, aft, outboard
01-235-2318
Structural Component Air Support
Used on f-15 acft. engine mount, aft, outboard
01-235-2319
Structural Component Air Support
Used on f-15 acft. p/o rib-wing section le; aluminum alloy 2024-0
01-235-2320
Structural Component Air Support
Used on f-15 acft. u/w inboard canopy lock
01-235-2333
Aircraft Skin
Used on acft model f-111-t. aluminum alloy 2024-T84 per qq-a-355-T84, 60.000 in. lg, 45.000 in. w, 0.160 in. thk
