01-222-5718
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.000 in. lg, 3.000 in. w, 0.045 in. thk
01-222-5719
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.000 in. lg, 3.000 in. w, 0.045 in. thk
01-222-5720
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 3.500 in. lg, 2.000 in. w, 0.045 in. thk
01-222-5721
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 3.500 in. lg, 2.000 in. w, 0.045 in. thk
01-222-5722
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 3.800 in. lg, 2.320 in. w, 0.080 in. thk
01-222-5723
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 7.600 in. lg, 3.400 in. w, 0.050 in. thk
01-222-5724
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 21.000 in. lg, 6.000 in. w, 1.375 in. thk
01-222-5725
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 21.000 in. lg, 6.000 in. w, 1.375 in. thk
01-222-5726
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 23.300 in. lg, 1.750 in. w, 0.063 in. thk
01-222-5727
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 6.500 in. lg, 3.700 in. w, 0.036 in. thk
01-222-5728
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 6.500 in. lg, 3.700 in. w, 0.036 in. thk
01-222-5729
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 6.200 in. lg, 2.600 in. w, 0.100 in. thk
01-222-5731
Aircraft Former
2.550" overall length
01-222-5732
Aircraft Former
49.750" overall length 17.700" overall width 0.063" material thickness
01-222-6000
Access Aircraft Cover
Used on acft model f-16c/d usaf. c/o 17 stiffener, 1 plate, 1 skin, 6 spacer, 151 pin, 151 collar, 10 nut assy, 1 bracket, rivet
01-222-6061
Aircraft Wing Assembly
Wing box assy
01-222-6109
Fluid Aircraft Manifold
01-222-6329
Structural Aircraft Plate
01-222-6330
Structural Aircraft Plate
5.600" overall length 4.700" overall width 0.056" material thickness
01-222-6331
Structural Component Air Support
Used on acft model f-111. approximately 7.000 in. lg o/a
01-222-6332
Structural Component Air Support
Used on f-15 aircraft.
01-222-6333
Structural Component Air Support
Used on f-15 aircraft.
01-222-6334
Structural Component Air Support
Used on f-15 acft.
01-222-6335
Structural Component Air Support
Used on f-15 acft.
01-222-6336
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 12.500 in. lg, 6.000 in. w, 2.000 in. thk
01-222-6337
Structural Component Air Support
Used on f-15 acft. aluminum alloy per qq-a-250/5 condition 0, 6.250 in. lg, 5.600 in. w, 0.063 in. thk
01-222-6338
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition aln, 4.000 in. lg, 2.400 in. w, 0.045 in. thk
01-222-6347
Aircraft Former
01-222-6348
Aircraft Former
01-222-6349
Aircraft Former
01-222-6350
Aircraft Former
01-222-6351
Aircraft Former
01-222-6352
Aircraft Former
29.020" overall length material per 1MT360A01-10040
01-222-6353
Aircraft Former
01-222-6354
Aircraft Former
43.250" overall length material per 1MT360A01-10037
01-222-6355
Aircraft Former
43.250" overall length material per 1MT360A01-10037
01-222-6356
Aircraft Former
10.500" overall length 4.500" overall width 1.000" material thickness
01-222-6357
Aircraft Former
47.100" overall length 16.300" overall width 0.090" material thickness
01-222-6358
Aircraft Former
47.100" overall length 16.300" overall width 0.090" material thickness
01-222-6359
Aircraft Former
51.000" overall length 20.000" overall width 0.080" material thickness
01-222-6360
Aircraft Former
51.000" overall length 20.000" overall width 0.080" material thickness
01-222-6361
Aircraft Former
52.100" overall length 19.300" overall width 0.063" material thickness
01-222-6362
Aircraft Former
52.100" overall length 19.200" overall width 0.063" material thickness
01-222-6363
Aircraft Former
47.000" overall length 16.000" overall width 0.080" material thickness
01-222-6364
Aircraft Former
47.000" overall length 16.000" overall width 0.080" material thickness
01-222-6365
Aircraft Stringer
01-222-6366
Aircraft Stringer
01-222-7517
Access Aircraft Door
Used on doubler aft door assy,nose landing rear 1560-00-894-4186.
01-222-7625
Structural Aircraft Plate
Type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5; matl 0.063 in. thk by 6.500 in. w by 9.297 in. lg
01-222-7626
Structural Aircraft Plate
Type/model designation:GRMK5 steel comp 304 qq-s-766; matl 0.080 in. thk by 0.766 in. w by 3.766 in. lg; 2 mtg holes 0.1865 in. min
