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National Stock Number:
3120-99-604-1124
Federal Supply Class:
3120
National Item Identification Number:
996041124
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.
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Manufacturer Information:
| F133837 | K0289 | BRITISH AEROSPACE MILITARY AIRCRAFT & AEROSTRUCTURES | | F133837 | K1987 | BAE SYSTEMS PLC | | F133837 | K2089 | LUSHINGTON TOOL & GAUGE CO LTD | | F133837 | U9143 | BAE SYSTEMS (OPERATIONS) LIMITED |
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Techincal Specification:
| BODY INSIDE DIAMETER | 0.3125 INCHES NOMINAL | | BODY OUTSIDE DIAMETER | 0.4378 INCHES MINIMUM AND 0.4380 INCHES MAXIMUM | | CORNER SHAPE | SQUARE ALL CORNERS | | MATERIAL DOCUMENT AND CLASSIFICATION | BS 369 PB102 NATIONAL STD/SPEC SINGLE MATERIAL RESPONSE OVERALL | | MATERIAL | COPPER ALLOY OVERALL | | OVERALL LENGTH | 0.1900 INCHES MINIMUM AND 0.1940 INCHES MAXIMUM | | STYLE DESIGNATOR | SOLID, PLAIN, NO OUTSIDE FLANGES | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | HAWKER SIDDELEY AVIATION LTD 1000 B1 MFR REF 1ST TREATMENT RESPONSE OVERALL AND HAWKER SIDDELEY AVIATION LTD 100 B1 MFR REF 2ND TREATMENT RESPONSE OVERALL AND MOD(PE)/DMAT DTD 900 4404 MIL STD 3RD TREATMENT RESPONSE OVERALL OR HAWKER SIDDELEY AVIATION LTD 1000 2 MFR REF SINGLE TREATMENT RESPONSE OVERALL | | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL AND PAINT OVERALL OR CADMIUM OVERALL AND CHROMATE OVERALL |
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