3120-01-037-8957, BEARING,SLEEVE

National Stock Number:
3120-01-037-8957

Federal Supply Class:
3120

National Item Identification Number:
010378957

Description:
BEARING,SLEEVE

Detail:
A tubular shaped item with or without flange(s) designed to reduce friction and carry a kinetic load on the surface(s) parallel to the axis of the bore. It must have a visible or detectable means of lubrication or be self-lubricated. The over all length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body, except for straight tubular (without flange or shoulder) items having a bearing surface(s) parallel to the axis of the bore only. Includes items which are divided into two or more segments which include 180 degrees (3.141 radians) or less of the bearing periphery. See also BUSHING, SLEEVE; SPACER, SLEEVE; and WASHER (as modified). Excludes PIN, HOLLOW.

Manufacturer Information:

07-382-08A009	09455	RBC TRANSPORT DYNAMICS CORP
10107695	A486G	NIMIKKEISTOKESKUS NCB FINLAND
119-00-08-009	77896	REXNORD INDUSTRIES, LLC
123-0208A009	77896	REXNORD INDUSTRIES, LLC
91087-08A009	09455	RBC TRANSPORT DYNAMICS CORP
ADLF08A009	15860	NEW HAMPSHIRE BALL BEARINGS INC
AHJF08A009	50294	NEW HAMPSHIRE BALL BEARINGS INC
AS81934	81343	SOCIETY OF AUTOMOTIVE ENGINEERS INC
AS81934/2	81343	SOCIETY OF AUTOMOTIVE ENGINEERS INC
ATTF08A009	15860	NEW HAMPSHIRE BALL BEARINGS INC
FBJW16TF-08A009	21335	TIMKEN CO
FBJW16TF09WM	21335	TIMKEN CO
FBJW16TF09WM	3NPS1	RBC AIRCRAFT PRODUCTS, INC.
FBRR-08A009	73134	ROLLER BEARING CO OF AMERICA INC
KDJ08A009	97613	SARGENT AEROSPACE & DEFENSE, LLC
KDJ08A009-342	97613	SARGENT AEROSPACE & DEFENSE, LLC
KRJ8YB-08A009M	50632	KAMATICS CORPORATION
M81934/2-08A009	81343	SOCIETY OF AUTOMOTIVE ENGINEERS INC
M81934/2-08A009	81349	MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-B-81934/2	81349	MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
ST4M127-08A009	76301	THE BOEING COMPANY

Techincal Specification:

BODY INSIDE DIAMETER	0.5005 INCHES MINIMUM AND 0.5015 INCHES MAXIMUM
BODY OUTSIDE DIAMETER	0.6260 INCHES MINIMUM AND 0.6270 INCHES MAXIMUM
CORNER SHAPE	SQUARE INSIDE LEFT CORNER
CORNER SHAPE	SQUARE INSIDE RIGHT CORNER
CORNER SHAPE	SQUARE LEFT FLANGE OUTSIDE RIGHT CORNER
CORNER SHAPE	SQUARE OUTSIDE LEFT CORNER
CORNER SHAPE	SQUARE OUTSIDE RIGHT CORNER
CORNER SHAPE	UNDERCUT LEFT FLANGE BODY CORNER
FLANGE OUTSIDE DIAMETER	0.9800 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
FLANGE WIDTH	0.0575 INCHES MINIMUM AND 0.0625 INCHES MAXIMUM
OVERALL LENGTH	0.3287 INCHES MINIMUM AND 0.3437 INCHES MAXIMUM
MATERIAL	ALUMINUM ALLOY 2024 OUTER LAYER
MATERIAL	PLASTIC INNER LAYER
SPECIAL FEATURES	PLASTIC LINER BONDED TO LEFT END SURFACE OF FLANGE
STYLE DESIGNATOR	SOLID, EXTERNAL FLANGE ONE END
SURFACE FINISH	125.0 MICROINCHES INSIDE DIAMETER SURFACE OF BODY
SURFACE FINISH	125.0 MICROINCHES RIGHT END SURFACE OF BODY
SURFACE FINISH	125.0 MICROINCHES RIGHT END SURFACE OF LEFT FLANGE
SURFACE FINISH	125.0 MICROINCHES OUTSIDE DIAMETER SURFACE OF FLANGE
SURFACE FINISH	25.0 MICROINCHES LEFT END SURFACE OF BODY AND FLANGE
SURFACE FINISH	63.0 MICROINCHES OUTSIDE DIAMETER SURFACE OF BODY
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OUTER LAYER
SURFACE TREATMENT	ANODIZE OUTER LAYER

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