01-135-3134
Structural Component Air Support
Used on acft model a-10. c/o fitting p/n 160D116023-23, bushing p/n 160D637002-7, bushing p/n 160D637002-9
01-135-3148
Aircraft Skin
Used on acft model c135. magnesium alloy sheet per qq-m-44, condition h; 16.500 in. lg, 11.500 in. w, 0.040 in. thk; used on wing body fairing, fuselage stations 954 to 1120; opposite p/n 5-95800-37
01-135-3149
Aircraft Skin
Used on acft model c135. magnesium alloy sheet per qq-m-44, condition h; 16.500 in. lg, 11.500 in. w, 0.040 in. thk; used on wing body fairing, fuselage stations 954 to 1120
01-135-3150
Aircraft Skin
Used on acft model c135. magnesium alloy sheet per qq-m-44, condition h; 70.000 in. lg, 17.000 in. w, 0.040 in. thk; used on wing body fairing, fuselage stations 954 to 1120; opposite p/n 5-95800-15
01-135-3151
Aircraft Skin
Used on acft model c135. magnesium alloy sheet per qq-m-44, condition h; 70.000 in. lg, 17.000 in. w, 0.040 in. thk; used on wing body fairing, fuselage stations 954 to 1120
01-135-3152
Aircraft Skin
Used on acft model c135. magnesium alloy sheet per qq-m-44, condition h; 71.000 in. lg, 31.000 in. w, 0.040 in. thk; used on wing body fairing, fuselage stations 954 to 1120
01-135-3153
Aircraft Skin
Used on acft model c135. al alloy sheet, 2024-0 clad per qq-a-250/5, heat treat to condition T4, finish f-2.130; 54.000 in. lg, 18.000 in. w, 0.040 in. thk; opposite p/n 5-96330-60; used on flying boom fairing
01-135-3154
Aircraft Skin
Used on C-135. 54.000" overall length 18.000" overall width finish f 1.130; opposite p/n 5-96330-59
01-135-3155
Aircraft Skin
Used on acft model c135. al alloy sheet, 2024-0 clad per qq-a-362, 0 temper, heat treat to condition T4, finish f-2.130; 50.000 in. lg, 30.000 in. w, 0.040 in. thk; used on assembly of nacelle, t/c forward fairing
01-135-3515
Structural Aircraft Plate
01-135-3516
Structural Aircraft Plate
01-135-3671
Structural Component Air Fitting
01-135-3672
Aircraft Fairing
C/o 1 channel, 2 angle, 1 seal
01-135-3684
Structural Component Air Support
Used on c-141 acft. matl laminated steel; matl size 0.050 by 2.000 by 6.000 in. lg; used on fitting installation, beam splice, pylon station 220.298
01-135-3762
Structural Component Air Bracket
01-135-4338
Access Aircraft Door
Anodize surface treated
01-135-4632
Structural Component Air Support
Used on acft model f-16. consist of 1 bracket, 4 bushing; eff 61 0001 9999; nha 16K0680-20; superseded 16K0682-806 ow ecn 4D861
01-135-5225
Structural Aircraft Plate
6.000" overall length 2.000" overall width 0.032" material thickness used as retainer
01-135-5226
Structural Aircraft Plate
10.000" overall length 4.000" overall width 0.125" material thickness opposite to p/n 3W00514-103
01-135-5227
Aircraft Fairing
C.o angle 160D610103-91, innerfwdskin 160D610103-117, angle 160D610103-123, outer skin 160D610103-127, inner skin 160D610103-129, foam INSTALLATION160D611706-3
01-135-5228
Aircraft Fairing
Used on A-10A. 35.000" overall length 10.000" overall width 0.063" material thickness
01-135-5229
Structural Component Air Support
Used on c-141a/b acft. matl al alloy; matl size 0.032 by 2.000 by 6.000 in. lg; opposite to p/n 3P61525-163; used on fairing, power plant
01-135-5230
Structural Component Air Support
Used on c-141a/b acft. matl al alloy, 2024-T4 clad; matl size 0.032 by 2.000 by 6.000 in. lg; used as retainer on fairing power plant assy
01-135-5231
Structural Component Air Support
Used on c-141a/b acft. 13.750 in. lg; rectangular shaped; used as splice plate on front beam wing station 77.7
01-135-5232
Structural Component Air Support
Used on c-141a/b acft. 13.870 in. lg; rectangular shape; used as splice plate on front beam wing station 77.7
01-135-5233
Aircraft Former
22.000" overall length 21.000" overall width 0.050" material thickness
01-135-5648
Aircraft Wing Assembly
01-135-5668
Structural Aircraft Panel
Used on F-111.
01-135-5670
Structural Component Air Support
Used on acft model f-111. used on hand pump handle
01-135-5672
Structural Component Air Bracket
01-135-5678
Aircraft Skin
Used on acft model c-135. magnesium alloy sheet per qq-m-44, condition h, finish f-3.35 then f-3.75; 71.000 in. lg, 31.000 in. w, 0.040 in thk; used on fairing, wing to body
01-135-6202
Aircraft Fairing
Used on C-141. 9.080" overall length 3.250" overall width includes three nuts
01-135-6203
Structural Component Air Support
01-135-6212
Aircraft Stringer
01-135-7640
Structural Aircraft Plate
01-135-7646
Aircraft Stiffener
01-135-8703
Access Aircraft Cover
01-135-8705
Access Aircraft Cover
01-135-8865
Horizontal Stabilizer
69.627" overall length box assembly of
01-135-8867
Access Aircraft Door
Used on F-16. rh lower strake FS190 to FS217
01-135-8941
Aircraft Fairing
26.000" overall length 20.000" overall width 0.100" material thickness
01-135-8943
Pylon Aircraft Fairing
Used on aircraft model e-2c. cognizant service:navy;
01-135-8944
Structural Component Air Support
Used on acft model f-16. consists of 1 bracket, 4 bushing, used on left hand hinge canopy; eff 61 0001 9999; nha 16K0680-19; superseded 16K0682-805 ow ecn 40861
01-135-8945
Structural Component Air Support
19.000" overall length 7.000" overall width matl: al aly clad; 5 holes 0.220 in dia; u/a: support, elect wiring
01-135-8956
Aircraft Leading Edge
C/o 150 component parts
01-135-8958
Aircraft Skin
Used on aircraft model f-14a.
01-135-8967
Structural Aircraft Panel
01-135-8968
Outer Wing Section
Replacement for 861, 863, 865, 867, 869, 871
01-135-8969
Outer Wing Section
01-135-9223
Fluid Aircraft Manifold
