01-247-4270
Structural Component Air Support
Used on acft model a-10a. aluminum alloy clad sh per qq-a-250/13 7075-0, 2.500 in. lg, 2.500 in. w, 0.050 in. thk
01-247-4271
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage; fuselage station 626.900 to 712.310
01-247-4272
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage; fuselage station 626.900 to 712.310
01-247-4274
Structural Component Air Support
Used on f-15 acft. fitting, engine-forward mount; fuselage station 657.060 to 672.680
01-247-4275
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage; fuselage station 626.900 to 712.310
01-247-4276
Structural Component Air Support
Used on f-15 acft. p/o keel structure, aft fuselage; fuselage station 626.900 to 712.310
01-247-4277
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; doubler u/o access opening, upper aft fuselage
01-247-4279
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9047 type 3 comp c annealed; supports stabilator actuator
01-247-4280
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9047 type 3 comp c annealed; supports stabilator actuator
01-247-4281
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9047 type 3 comp c annealed; supports stabilator actuator
01-247-4282
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9047 type 3 comp c annealed; supports stabilator actuator
01-247-4310
Wing Landing Flap
C/o: stringers, closeouts, intercostals, ribs, trailing edges, doors, gussets, splices, spars, skin, doublers, & hardware
01-247-4311
Aircraft Former
Used on F-16. 5.630" overall length 0.96 high one end b 0.85 high other end; nha 16B6556-43; stiffener, engine access door
01-247-4312
Aircraft Former
Replaces -33; 8.73 lg, taper length is 3.00; nha 16B6556-43; stiffener, engine access door
01-247-4313
Aircraft Former
Used on F-16. replaces -75 except 0.88 high; nha 16B6556-51; stiffener, engine access door
01-247-4314
Aircraft Former
Used on F-16. replaces -155; same except for 1.6 in. longer; nha 16B6556-51; stiffener, engine access door
01-247-4321
Aircraft Former
45.200" overall length 14.300" overall width 0.050" material thickness
01-247-4323
Aircraft Former
32.000" overall length 0.062" material thickness
01-247-4325
Aircraft Former
29.000" overall length 6.000" overall width 0.025" material thickness
01-247-4326
Aircraft Former
29.000" overall length 6.000" overall width 0.025" material thickness
01-247-4328
Aircraft Former
28.000" overall length 3.000" overall width 0.032" material thickness
01-247-4330
Aircraft Former
28.000" overall length 3.000" overall width 0.032" material thickness
01-247-4331
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4332
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4333
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4334
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4335
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4336
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4337
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4338
Aircraft Former
24.000" overall length 4.000" overall width 0.050" material thickness
01-247-4339
Aircraft Former
12.700" overall length 12.500" overall width 0.032" material thickness
01-247-4340
Aircraft Former
25.700" overall length 7.400" overall width 0.063" material thickness
01-247-4341
Aircraft Former
7.700" overall length 7.400" overall width 0.063" material thickness
01-247-4342
Aircraft Former
25.100" overall length 7.400" overall width 0.063" material thickness
01-247-4343
Aircraft Former
25.400" overall length 7.400" overall width 0.063" material thickness
01-247-4344
Aircraft Former
30.800" overall length 16.600" overall width 0.032" material thickness
01-247-4345
Aircraft Former
5.000" overall length 4.000" overall width 0.050" material thickness
01-247-4346
Aircraft Former
19.000" overall length 0.050" material thickness
01-247-4347
Aircraft Former
Used on F-15. p/o inboard, empennage support beam closure
01-247-4348
Aircraft Former
Used on F-15.
01-247-4354
Longeron
66.600" overall length
01-247-4356
Airfoil Rib
Used on F-15.
01-247-4357
Airfoil Rib
Used on F-15.
01-247-4358
Airfoil Rib
Used on F-15. cond 0 alclad
01-247-4359
Airfoil Rib
Used on F-15.
01-247-4360
Airfoil Rib
Used on F-15. cond 0 alclad
01-247-4361
Airfoil Rib
Used on F-15. cond 0 alclad
01-247-4365
Aircraft Skin
54.000" overall length 42.000" overall width p/o skin installation
01-247-4368
Aircraft Skin
18.000" overall length 17.000" overall width p/o skin installation
