01-134-8436
Aircraft Former
01-134-9188
Access Aircraft Cover
Used on acft model a-10a.
01-134-9216
Structural Aircraft Panel
Used on A-10. c/o panel p/n 160D611517-11, channel p/n 160D611511-169, channel p/n 160D611511-171, support p/n 160D345441-177, clip p/n S166-5a, as required rivet
01-134-9218
Structural Component Air Support
Used on acft model a-10. c/o support 60D145122-11, 6 ea. plate nut p/n MS21069L3, rivet as required p/n MS20426AD3
01-134-9219
Structural Component Air Support
Used on acft model a-10a. located in tail cone
01-134-9220
Structural Component Air Support
Used on acft model a-10a. located on door
01-134-9221
Structural Component Air Support
Used on h-53 acft. matl al alloy, qq-a-225/9, 7075-77351; matl size 2.750 by 2.750 by 4.000 in. lg; used as fitting, radar-outboard, radar mount structure
01-134-9226
Aircraft Former
7.000" overall length 0.063" material thickness
01-134-9228
Aircraft Skin
Used on F-111.
01-134-9229
Aircraft Skin
Used on F-111.
01-134-9230
Aircraft Window Panel
Used on acft model f-16.
01-134-9236
Thermal Special Purpo Insulation
F-111
01-134-9239
Thermal Special Purpo Insulation
F-111
01-134-9241
Thermal Special Purpo Insulation
F-111
01-134-9243
Thermal Special Purpo Insulation
F-111
01-134-9244
Thermal Special Purpo Insulation
F-111
01-134-9245
Thermal Special Purpo Insulation
End item identification:aircraft, model f-111
01-135-0235
Aircraft Stiffener
4.690" overall length 2.000" overall width 0.063" material thickness
01-135-0236
Aircraft Stiffener
01-135-0237
Aircraft Stiffener
01-135-0238
Aircraft Stiffener
01-135-0239
Aircraft Stiffener
01-135-0240
Aircraft Stiffener
01-135-0241
Aircraft Stiffener
01-135-0242
Aircraft Stiffener
01-135-0243
Aircraft Stiffener
01-135-0244
Aircraft Stiffener
01-135-0245
Aircraft Stiffener
01-135-0246
Aircraft Stiffener
01-135-0247
Aircraft Stiffener
01-135-0286
Structural Aircraft Plate
Matl:lam st, LAC07-665, class 3; u/a: shim
01-135-1707
Structural Component Air Support
Used on mh-53d aircraft code for japan. navy) structural assembly, tail pylon
01-135-1832
Structural Component Air Support
Used on f-15 acft. location-upper fuselage station 626.900-conformal fuel tank
01-135-1833
Structural Component Air Support
Used on f-15 acft. location-upper fuselage-conformal fuel tank
01-135-1838
Aircraft Skin
Used on aircraft model f-14a. aluminum alloy qq-a-250/5 alloy 2024 temper T81, 0.070 in. thk
01-135-1957
Fluid Aircraft Manifold
01-135-1958
Fluid Aircraft Manifold
01-135-2266
Structural Component Air Bracket
01-135-3051
Fuel Tank Aircraft Baffle
8.060" overall length 1.460" overall width
01-135-3052
Aileron Balance Weight
Used on acft model c135. fansteel 77, finish zinc chromate primer; 7.420 in. lg, 1.230 in. w, 0.480 in. h tapering to 0.380 in. h; located at outboard nose of aileron
01-135-3053
Aileron Balance Weight
Used on acft model c135. antimony lead, l-16 (6% antimony) , finish cadmium plate per qq-p-416 type ii or iii class b
01-135-3054
Aileron Balance Weight
Used on acft model c135. antimony lead, l-16 (6% antimony) , finish cadmium plate per qq-p-416 type ii or iii class b
01-135-3055
Aileron Balance Weight
Used on acft model c135. antimony lead, l-16 (6% antimony) , finish 2 coats zinc chromate primer per mil-p-6889; 8.570 in. lg, 1.06 in. w, 0.43 in. h tapering to 0.340 in. h; used on outboard noseof aileron
01-135-3056
Aileron Balance Weight
Used on acft model c135. antimony lead, l-16 (6% antimony) , finish 2 coats zinc chromate primer per mil-p-6889; 8.810 in. lg. 1.060 in. w, 0.440 in. h tapering to 0.340 in. h; located on outboard nose of aileron
01-135-3103
Access Aircraft Door
Used on uh-1 helicopter. location-lower installation, left hand, station 178.00 to 211.06
01-135-3129
Structural Aircraft Panel
C/o core p/n 160D514113 -55, core p/n 160D514113-57, core p/n 160D514113-58, skin p/n 160D514113
01-135-3130
Structural Aircraft Plate
2.750" overall length 1.750" overall width 0.040" material thickness
01-135-3131
Structural Aircraft Plate
Used on acft model c135. al alloy sheet, 2024-0 clad per qq-a-250/5, heat treat to condition T4, finish f-2.115; 52.000 in. lg, 4.900 in. w, 0.064 in. thk; used on flying boom fairing
01-135-3132
Structural Component Air Support
Used on acft model c135. made from casting 5-85688-1, finish f-3.71; 16.100 in. lg, 5.000 in. w, 4.929 in. h; contains 24 mounting holes in base; used as flap screw support, located at inboard flap, wing station 453.014
01-135-3133
Structural Component Air Support
Used on acft model c135. nmade from casting 5-85688-1, finish f-3.71; 16.100 in. lg, 5.000 in. w, 4.929 in. h; contains 24 mounting holes in base; opposite p/n 5-85687-1; used as flap screw support, located at inboard flap, wing station 453.014
