01-114-8627
Thermal Insulation Pipe Covering
01-114-9155
Structural Aircraft Plate
81.000" overall length 12.000" overall width 0.750" material thickness
01-114-9446
Structural Aircraft Panel
Used on A-10.
01-114-9477
Airfoil Rib
34.350" overall length 12.000" overall width 5.500" material thickness
01-114-9479
Aircraft Skin
Used on c-135 and kc-135 airplane.. 66.000" overall length 6.000" overall width finish f-12.10
01-114-9520
Inlet Aircraft Lip
Used on uh-60, rotary wing aircraft. inlet, assembly, air-engine
01-114-9521
Structural Component Air Support
Al alloy 2024, qq-a-250/5, cond o; thk 0.040 in.; height 3.380 in.; length 2.750 in.; width 2.680 in.; 8 mounting holes 0.098 in. dia
01-115-0315
Structural Component Air Fitting
Finish f-18.04; make 5-86026-2
01-115-0316
Structural Component Air Fitting
Finish f-18.04; make 5-86026-2
01-115-0317
Structural Component Air Support
01-115-0318
Structural Component Air Support
01-115-0328
Aircraft Latch Assembly
Used on f-15a acft. matl ams 6411; 3.250 in. lg; 2.250 in. wd; 0.500 in. thk
01-115-0340
Fuselage Parts Kit
Used on c-141a/b acft. sta 998
01-115-0354
Structural Component Air Support
Used on c-5 acft. 14.919 in. lg; includes two bushings; 0.499 in. dia six places; used on hinge no 2 aileron station 85.9635
01-115-0355
Structural Component Air Support
Used on c-5a acft. matl al alloy; used on fitting hinge no. 4, outboard actuator, aileron assembly
01-115-0356
Structural Component Air Support
Used on c-5a acft. matl al alloy qq-a-367 7075-f-T6, part of aileron assembly
01-115-0357
Structural Component Air Support
Used on c-5a acft. matl al alloy qq-a-367 7075-f-T6, part of aileron assembly
01-115-0358
Structural Component Air Support
Used on c-5a acft.
01-115-1450
Aircraft Elevator
01-115-2123
Aircraft Windshield Panel
Clear plexiglass, 25.000 in.by 41.000 in.by 72.000 in.o/a, has an 18.000 in.radius, part of 3150220-601-105 windshield assy;
01-115-2710
Structural Component Aircraf Web
63.000" overall length 16.000" overall width 0.100" material thickness
01-115-2767
Structural Aircraft Plate
1.500" material thickness bronze; dia 1.500 in.
01-115-2768
Aircraft Elevator
01-115-2769
Structural Component Air Support
Used on c-5a acft. matl al alloy qq-a-225/9 7075-T651, matl size 2 by 2
01-115-2770
Structural Component Air Support
Used on c-5a acft. matl al alloy qq-a-225/9 7075-T651, matl size 2 by 2
01-115-2771
Structural Component Air Support
Used on c-5a acft. matl al alloy qq-a-225/9 7075-T651, matl size 2 by 2
01-115-2776
Aircraft Former
Used on T-39. 18.000" overall length 7.250" overall width
01-115-2778
Aircraft Pylon
Fuel tank pylon
01-115-2779
Airfoil Rib
36.720" overall length 8.000" overall width 2.000" material thickness
01-115-2780
Aircraft Skin
24.000" overall length 6.000" overall width superseded p/n 16T4670-9, i/c code ni, effectivity 6k 0024-9999, ecn 95002, nha p/n 16T4660-71
01-115-2782
Aircraft Skin
C/o--47 skin, -61 plate .100 x 4 X6, -63 plate .100 x 3 x 6, -65 plate .100 x 2 x 4, -67 plate .100 x 2 x 4, -69 plate .050 x 3 x 6, -71 plate .050 x 3 X6, -75 skin .100 x 55 x 66, modified -829 skin, support; finish A403; superseded -829 two way after modification, retroffit; nha 16B410-69; eff on 62 0003 0024
01-115-2784
Aircraft Skin
Used on F-111. 78.000" overall length 20.000" overall width fm-1053, type i
01-115-2786
Aircraft Skin
Used on F-111. 70.000" overall length 18.000" overall width fms-1053, type i
01-115-2787
Aircraft Skin
36.000" overall length 33.000" overall width function-inboard empennage support beam closure
01-115-2788
Aircraft Trailing Edge
C/o stiffener p/n 12W8042-7, skin p/n 12W8150-7, 4 ea. rub strip
01-115-3178
Access Aircraft Cover
Used on h-53 acft. c/o 4 window, 2 plate, misc hadwr
01-115-3215
Structural Component Air Support
Used on c-5a acft. matl al alloy, qq-a-367 7075-T6; used on station 33.280, aileron assembly
01-115-3578
Structural Component Air Bracket
Used on H-60A. bracket assy, deicing-tail rotor blade consists of 2 angles
01-115-3589
Aircraft Window Panel
Used on uh-60, rotary wing aircraft.
01-115-3596
Structural Component Air Support
01-115-3657
Structural Component Air Bracket
Used on 1520010350266 and 1520010820686.
01-115-3669
Aircraft Fairing
01-115-3852
Aircraft Fairing
14.000" overall length 6.000" overall width 0.071" material thickness pilots foot guide
01-115-3856
Structural Component Air Support
7.200" overall length 5.700" overall width 0.063" material thickness finish f-8.07
01-115-3857
Structural Aircraft Plate
2.800" overall length 1.400" overall width 0.063" material thickness finish f-8.07
01-115-3859
Structural Component Air Fitting
Nuclear hardness; finish f-2.44
01-115-3860
Structural Component Air Fitting
Nuclear hardness; finish f-2.44
01-115-3861
Structural Component Air Fitting
Nuclear hardness; finish f-2.44
