2840-00-768-2995 HOUSING,GEARBOX,TURBINEENGINE Index 2840-00-768-3005 NOZZLE,TURBINE,AIRCRAFT GAS TURB

National Stock Number:
3120-00-768-3004

Federal Supply Class:
3120

National Item Identification Number:
007683004

Description:
BUSHING,SLEEVE

Detail:
A tubular shaped unthreaded item with or without a flange at one end designed to be inserted into a hole to reduce the inside diameter of the hole and to protect the surrounding body structure from damage resulting from stress, strain, and/or vibration. The overall length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body. Includes items which are divided into two or more segments which includes 180 degrees (3.141 radians) or less of the bearing periphery. For items made of rubber, see BUSHING, NONMETALLIC. See also BEARING, SLEEVE; BUSHING, TAPERED; SPACER, SLEEVE; INSULATOR, BUSHING; and BUSHING, ELECTRICAL CONDUCTOR. Excludes BUSHING, DRILL, JIG.


Manufacturer Information:
38893830859TUBE PROCESSING CORP MILTURN DIV
38893852661RTX CORPORATION
38893860411AMERICAN TOOL AND MACHINE CORP
38893877445RTX CORPORATION
38893899106AMERICAN AIRCRAFT PARTS MFG. CO.


Techincal Specification:
BODY INSIDE DIAMETER1.4580 INCHES MINIMUM AND 1.4600 INCHES MAXIMUM
BODY OUTSIDE DIAMETER1.6430 INCHES MINIMUM AND 1.6570 INCHES MAXIMUM
CORNER SHAPECHAMFERED OUTSIDE RIGHT CORNER
CORNER SHAPESQUARE INSIDE LEFT CORNER
CORNER SHAPESQUARE INSIDE RIGHT CORNER
CORNER SHAPESQUARE LEFT FLANGE BODY CORNER
CORNER SHAPESQUARE LEFT FLANGE OUTSIDE RIGHT CORNER
CORNER SHAPESQUARE OUTSIDE LEFT CORNER
CRITICALITY CODE JUSTIFICATIONFEAT
FLANGE OUTSIDE DIAMETER2.0000 INCHES MINIMUM AND 2.0300 INCHES MAXIMUM
FLANGE WIDTH0.0600 INCHES MINIMUM AND 0.0700 INCHES MAXIMUM
HARDNESS RATING32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM OVERALL
LUBRICANT ACCOMMODATION STYLEGROOVED CIRCULAR
OVERALL LENGTH0.8050 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM
MATERIALSTEEL COMP 8740 OVERALL
SPECIAL FEATURESFIT FORM AND FUNCTION
STYLE DESIGNATORSOLID, EXTERNAL FLANGE ONE END
SURFACE FINISH125.0 MICROINCHES INTERMEDIATE LAYER
SURFACE GROOVE LOCATION AND QUANTITY1 EXTERNAL
SURFACE TREATMENTCADMIUM OVERALL


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