01-450-4871
Window Aircraft Frame
01-450-4965
Structural Component Air Support
3.600" overall length 4.480" overall width 3.490" material thickness manufacturer suggested name-support, actuator; c/o; -003 support & LD1307-0040-0815 bushing; n/a:L3056419; u/o acft 1 & subq; opposite -002; matl:al aly bar, aly 7075-T73511
01-450-4966
Structural Aircraft Panel
9.500" overall length 3.500" overall width manufacturer suggested name-closeout-lower nac skin; nuclear hardness critial item; matl:alclad sh alloy; u/o acft 1 & subq; n/a: L3226900; heat treat to temper T62 per ST0111LA0009; opp -004
01-450-5361
Longeron
Manfacturer suggested name; upper center longeron; nha L3000007; c/o 1 -011 assy, 2 angle, 3 strap 12 shim, 1 fitting, 1 frame, 850 bolt, 204 nut, 12 screw, 1172 washer, 234 nutplate, 12 spacer
01-450-5363
Access Aircraft Door
Used on B-1B. located YN107.0 to YN117.8; manufacturer suggested name; ctr antenna support assy; c/o 1 door, 2 angle, 11 nutplate, rivet a/r; nuclear hardness critical item
01-450-5364
Access Aircraft Door
01-450-5365
Access Aircraft Door
Used on B-1B. T3 temper; al clad sheet; heat treat T81 per ST0111LA0009; nha L3226350; matl 2024 per qq-a-250; 9.750 in lg, 24.000 in wd, 0.160 in thk; nuclear hardness critical item
01-450-5367
Aircraft Fairing
01-450-5368
Structural Aircraft Panel
01-450-5370
Access Aircraft Door
Used on ab-1b acft. tmanufacturer suggested name; moveable lip actuator doors attach pin access fwd nacelle; opposite -004; nha L3226900; nuclear hardness critical item; 2024-T851 bare al alloy plate per qq-a-250/4; 4.440 in lg, 2.120 in wd, 0.250 in thk
01-450-5373
Structural Aircraft Panel
01-450-5374
Structural Aircraft Panel
Manufacturer suggested name-skin assy; c/o: -037 inner skin, -043 outer skin, & -045 core. p/o; -301 assy u/o acft 1 & subq; finish 80ab except for dorsal ml surface finish 80af
01-450-5375
Aircraft Fairing
01-450-5376
Structural Aircraft Panel
01-450-5377
Aircraft Fairing
01-450-5378
Aircraft Fairing
01-450-5380
Aircraft Fairing
Manf. drawing name, leading edge, horiz. stabilizer assy.
01-450-5381
Aircraft Fairing
Manf. drawing name, leading edge, horiz. stabilizer, assy.
01-450-5386
Structural Component Air Support
7.100" overall length 0.800" overall width manufacturer suggested name-cushion cut shape, foam
01-450-5388
Aircraft Skin
24.000" overall length 21.000" overall width manufacturer suggested name; upper wing leading edge horn; al clad sheet only one side per LB0170-202; opp -15
01-450-5389
Structural Aircraft Panel
44.600" overall length 21.300" overall width manufacturer suggested name; baffle panel; heat treat T4; 0 temper
01-450-5390
Structural Aircraft Panel
9.500" overall length 3.500" overall width manufacturer suggested name-closeout-lower nac skin; nuclear hardness critical item; matl:alclad sh alloy; u/o acft 1 & subq; n/a: L3226900; heat treat to temper T62 per ST0111LA0009; opp -003
01-450-5392
Structural Aircraft Panel
31.700" overall length 21.300" overall width manufacturer suggested name; baffle panel; heat treat T4; 0 temper
01-450-5537
Structural Component Air Fitting
Used on f-15, eagle aircraft.
01-450-5834
Aircraft Fairing
01-450-5835
Structural Aircraft Panel
01-450-5839
Structural Aircraft Panel
01-450-5840
Structural Aircraft Panel
01-450-5842
Structural Aircraft Panel
Manufacturer suggested name - panel, inbd, hinge no.2 fairing, aft flap; nha 17P6P4402
01-450-5843
Structural Aircraft Panel
01-450-6489
Structural Aircraft Panel
01-450-6491
Structural Aircraft Panel
01-450-6494
Structural Aircraft Panel
01-450-6496
Structural Aircraft Panel
01-450-6497
Structural Component Air Support
20.320" overall length 2.930" overall width manufacturer suggested name-bracket; made from 1MT360B01-10056 x 20.50; u/o f-15s CUM39
01-450-6504
Aircraft Skin
60.000" overall length 9.500" overall width u/o f-15e CUM210 up, f-15i CUM15 up, f-15s CUM44 up; next higher assy 68A314022
01-450-6505
Aircraft Skin
37.170" overall length 15.320" overall width used on next assembly p/n 68A321000 on f-15s CUM37
01-450-6507
Aircraft Skin
11.800" overall length 8.300" overall width u/o f-15e CUM210 up, f-15i CUM10 up, f-15s CUM37 up
01-450-6510
Structural Aircraft Plate
6.560" overall length 2.390" overall width 0.016" material thickness manufacturer suggested name-seal; part of next asssembly p/n 68A321303-1006 on f-15c CUM38
01-450-6513
Structural Aircraft Plate
5.300" overall length 4.150" overall width 0.016" material thickness manufacturer suggested name-seal; u/o f-15c CUM38 up, f-15d CUM3 up
01-450-6514
Structural Aircraft Plate
5.900" overall length 5.500" overall width 0.016" material thickness manufacturer suggested name-cover; u/o f-15c CUM1-37, f-15d CUM1-7
01-450-6518
Structural Aircraft Plate
6.560" overall length 2.390" overall width 0.016" material thickness manufacturer suggested name-seal; part of next assembly p/n 68A321303-1005 on f-15c CUM38
01-450-6519
Structural Aircraft Plate
5.900" overall length 5.740" overall width 0.016" material thickness manufacturer suggested name-cover; used on f-15c CUM38-BLK24, f-15d CUM8-BLK24
01-450-6520
Structural Aircraft Plate
5.900" overall length 5.740" overall width 0.016" material thickness manufacturer suggested name-cover; used on f-15c CUM38-BLK24, f-15d CUM8-BLK24
01-450-6521
Structural Aircraft Plate
5.300" overall length 4.540" overall width 0.016" material thickness manufacturer suggested name-seal; u/o f-15c CUM38 up, f-15d CUM3 up
01-450-6522
Structural Aircraft Plate
5.900" overall length 5.740" overall width 0.016" material thickness manufacturer suggested name-cover; u/o f-15c, d BLK25 up
01-450-6524
Structural Aircraft Plate
5.900" overall length 5.740" overall width 0.016" material thickness manufacturer suggested name-cover; used on f-15c/d blocks 25
01-450-6535
Aircraft Skin
36.000" overall length 8.500" overall width used on next assembly p/n 68A321000 on f-15s CUM25
01-450-6536
Aircraft Skin
37.170" overall length 15.320" overall width used on next assembly p/n 68A321000 on f-15s CUM37
01-450-6629
Aircraft Elevator
Used on BQM-34.
