01-246-6437
Structural Component Air Support
Used on aircraft model av-8.
01-246-6438
Structural Component Air Support
Used on aircraft model av-8.
01-246-6439
Structural Component Air Support
Used on aircraft model av-8.
01-246-6440
Structural Component Air Support
Used on aircraft model av-8. titanium alloy per mil-t-9047, comp 6; 4.500 in. lg; 2.980 in. w
01-246-6441
Structural Component Air Support
Used on aircraft model av-8. titanium alloy per mil-t-9047, comp 6; 4.500 in. lg; 2.980 in. w
01-246-6443
Structural Component Air Support
Used on aircraft model av-8. titanium alloy per mil-t-9046, type 3, comp c; 2.950 in. nom o/a lg; 2.060 in. nom o/a h
01-246-6457
Aircraft Former
Used on aircraft model av-8.
01-246-6460
Aircraft Skin
Used on aircraft model f-18. aluminum alloy per qq-a-250/13, cond T6
01-246-6461
Aircraft Skin
Used on aircraft model f-18. aluminum alloy per qq-a-250/13, cond T6
01-246-6462
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/4, cond o
01-246-6463
Aircraft Spar
Used on acft model av-8.
01-246-6763
Access Aircraft Door
Used on uh-60a and eh-60a.
01-246-6766
Structural Component Air Support
Used on uh-60 black hawk helicopter....
01-246-7164
Structural Aircraft Plate
2.120" overall length 2.100" overall width 0.040" material thickness
01-246-7224
Structural Aircraft Plate
01-246-7225
Structural Component Air Support
Aluminum alloy, qq-a-250/5, alloy 2024-T42
01-246-7226
Structural Component Air Support
01-246-7434
Structural Aircraft Panel
01-246-7537
Structural Aircraft Plate
Aluminum alloy 2024-0 qq-a-250/5, matl 0.063 in. thk by 0.891 in. w by 1.906 in. lg
01-246-7538
Structural Aircraft Plate
Aluminum alloy 2024-0 qq-a-250/5, matl 0.063 in. thk by 1.000 in. w by 2.703 in. lg
01-246-7539
Structural Component Air Support
Aluminum alloy 7075-0 qq-a-250/13, matl 0.040 in. thk by 33.000 in. w by 54.000 in. lg
01-246-7540
Structural Component Air Support
Aluminum alloy 7075-0 qq-a-250/13, matl 0.040 in. thk by 33.000 in. w by 54.000 in. lg
01-246-7541
Structural Component Air Support
Steel corrosion 321 mil-s-6721, matl 0.040 in. thk by 0.391 in. w by 0.844 in. lg
01-246-7545
Airfoil Rib
Used on aircraft model av8b.
01-246-7546
Wing Rib
10.000" overall length 6.000" overall width 0.032" material thickness
01-246-7547
Airfoil Rib
Used on aircraft model av8b.
01-246-7548
Wing Rib
10.000" overall length 6.000" overall width 0.032" material thickness
01-246-7566
Thermal Special Purpo Insulation
Color dark gull grey
01-246-7887
Aircraft Elevator
01-246-7889
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh qq-a-250/13 7075-0, 37.000 in. lg, 9.600 in. w, 0.050 in. thk
01-246-7893
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 19.600 in. lg, 3.500 in. w, 0.063 in. thk
01-246-7897
Structural Component Air Support
Used on f-15 aircraft. size .040X3.84X13.89; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-7898
Structural Component Air Support
Used on f-15 aircraft. size .040X3.55X7.90; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-7899
Structural Component Air Support
Used on f-15 aircraft. size .040X3.55X7.90; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-7900
Structural Component Air Support
Used on f-15 aircraft. size .040X4.18X8.30; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-7901
Structural Component Air Support
Used on f-15 aircraft. size .040X3.67X7.33; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-7902
Structural Component Air Support
Used on f-15 aircraft. size .040X4.18X8.30; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, FS626.900-FS712.310
01-246-7903
Structural Component Air Support
Used on f-15 aircraft. size .040X3.73X11.68; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, fs 626.900-FS712.310
01-246-7904
Structural Component Air Support
Used on f-15 aircraft. size .050X2.95X8.76; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, fs 626.900-FS712.310
01-246-7905
Structural Component Air Support
Used on f-15 aircraft. size .050X2.95X8.76; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus, fs 626.900-FS712.310
01-246-7906
Structural Component Air Support
Used on f-15 aircraft. size .040X3.65X11.66; matl titanium per mil-t-9046, type 3, comp c, anl; used on -1001 keel structure, aft fus fs 626.900-FS712.310
01-246-7908
Aircraft Former
20.000" overall length 1.300" overall width 0.063" material thickness
01-246-8315
Structural Component Air Support
Used on sentry f22 aircraft.
01-246-8328
Structural Aircraft Panel
Used on f22 sentry aircraft.
01-246-8923
Aircraft Door
Make from -021; nha L5342999
01-246-8946
Structural Aircraft Plate
Used on F-15. 29.390" overall length 2.880" overall width 0.032" material thickness web
01-246-8947
Structural Aircraft Plate
Used on C-130.
01-246-8949
Structural Aircraft Plate
Used on 130.
01-246-8950
Structural Aircraft Plate
Used on C-130.
01-246-8951
Structural Aircraft Plate
Used on C-130.
