01-268-2092
Aircraft Former
Used on C-141.
01-268-2098
Aircraft Skin
01-268-2099
Aircraft Skin
Used on acft model e-3a,b. 7075-0 per qq-a-283 0 temp; finish f-2.26; located fss 222.59 to 305.80; nha 65-31923
01-268-2100
Aircraft Skin
Used on C-141. 11.000" overall length 9.000" overall width cond 0 clad
01-268-2101
Aircraft Skin
Used on F-15. 37.000" overall length 29.000" overall width
01-268-2102
Aircraft Spar
01-268-2103
Aircraft Spar
01-268-2104
Aircraft Spar
01-268-2105
Aircraft Spar
01-268-2106
Aircraft Stringer
01-268-2772
Access Aircraft Door
Used on acft model a-7d/k. located sta 308.83 to 352.34 systems access door assembly
01-268-2803
Aircraft Scoop
Scoop, ram air inlet-fuel heat sink, assembly of
01-268-2804
Aircraft Scoop
Ram air scoop
01-268-2805
Structural Aircraft Plate
Used on C-141. part of -101 segment assembly, duct, aft cowl; cap
01-268-2806
Structural Aircraft Plate
Used on C-141. 21.000" overall length 6.000" overall width 0.050" material thickness
01-268-2807
Structural Aircraft Plate
Used on C-141. 63.000" overall length 4.000" overall width 0.080" material thickness channel
01-268-2808
Structural Aircraft Plate
Used on C-141. 3.000" overall length 3.000" overall width 0.020" material thickness anld; channel
01-268-2809
Structural Aircraft Plate
Used on C-141. 10.000" overall length 6.000" overall width 0.050" material thickness
01-268-2810
Structural Aircraft Plate
Used on F-15. 57.030" overall length 5.600" overall width 0.030" material thickness
01-268-2813
Structural Component Air Support
3.000" overall length 2.000" overall width 0.050" material thickness
01-268-2814
Structural Component Air Support
17.000" overall length 2.000" overall width 0.040" material thickness
01-268-2815
Structural Component Air Support
9.000" overall length 3.000" overall width 0.050" material thickness
01-268-2833
Aircraft Former
Used on C-141. frame
01-268-3400
Access Hole Aircraft Frame
01-268-4209
Structural Component Air Support
Used on aircraft model av-8. aluminum alloy
01-268-4210
Structural Component Air Support
Used on aircraft model av-8. aluminum alloy
01-268-4215
Aircraft Floor
Used on aircraft model av-8.
01-268-4216
Aircraft Floor
Used on aircraft model av-8.
01-268-4217
Aircraft Floor
Used on aircraft model av-8.
01-268-4218
Aircraft Former
Used on aircraft model av-8.
01-268-4220
Horizontal Stabilizer
Used on c-2a acft. cognizant service:navy; 314.0 in.lg, 13.0 in.w, 86.750 in.h, spare for 1560-00-218-4412;
01-268-4619
Structural Aircraft Plate
Used on C-141. 11.000" overall length 6.000" overall width 0.050" material thickness
01-268-4620
Structural Aircraft Plate
Used on C-141. 25.000" overall length 20.000" overall width 0.032" material thickness
01-268-4621
Structural Aircraft Plate
Used on C-141. 11.000" overall length 6.000" overall width 0.050" material thickness
01-268-4622
Structural Aircraft Plate
Used on C-141. cap
01-268-4623
Structural Aircraft Plate
Used on C-141. cap
01-268-4624
Structural Aircraft Plate
Used on C-141. cap
01-268-4625
Structural Aircraft Plate
Used on C-141. 30.000" overall length 15.000" overall width 0.063" material thickness
01-268-4626
Structural Aircraft Plate
Used on C-141. 41.000" overall length 8.000" overall width 0.071" material thickness
01-268-4627
Structural Aircraft Plate
Used on C-141. 16.000" overall length 12.000" overall width 0.063" material thickness
01-268-4629
Structural Component Air Support
3.000" overall length 2.000" overall width 0.050" material thickness
01-268-4637
Airfoil Rib
Used on C-141.
01-268-5459
Structural Component Aircr Patch
4.000 in. o/a lg; 2.000 in. o/a w
01-268-5884
Structural Component Air Support
01-268-5885
Structural Component Air Support
01-268-5886
Structural Component Air Support
