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3120-01-531-7568

Sleeve Bearing

3120015317568 015317568 54594

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. View more Sleeve Bearing

3120-01-531-7568 BEARING,SLEEVE 3120015317568 015317568

Managed by United States
NSN Created on 20 Jul 2005
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
STYL Style 18C for 3120-01-531-7568 1/1
NSN 3120-01-531-7568 (Identification) 1/1

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3120-01-531-7568 Demil Restrictions 3120-01-531-7568

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

3120-01-531-7568 is a Sleeve Bearing that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

3120-01-531-7568 HTS and ScheduleB Import and Export 3120-01-531-7568

3120-01-531-7568 End Users End Users 3120-01-531-7568

US Air Force (FBB5)
Effective Date:
1 Jul 2005

3120-01-531-7568 Manufacturers Approved Sources 3120-01-531-7568

3120-01-531-7568 Technical Data Datasheet 3120-01-531-7568

Characteristic
Specifications
FIIG
A045A0
End Item Identification [AGAV]
C-17A Aircraft
Body Inside Diameter [ADAS]
0.2500 Inches Minimum And 0.2510 Inches Maximum
Body Outside Diameter [ADAR]
0.6160 Inches Minimum And 0.6360 Inches Maximum
Corner Shape [BZLX]
Square All Corners
Material [MATT]
Aluminum Alloy 2024 Overall
Left Flange Outside Diameter [AGFQ]
0.7250 Inches Minimum And 0.7450 Inches Maximum
Left Flange Width [AGFS]
0.0500 Inches Minimum And 0.0700 Inches Maximum
Right Flange Outside Diameter [AGFR]
0.7970 Inches Minimum And 0.7980 Inches Maximum
Right Flange Width [AGFT]
0.1550 Inches Minimum And 0.1600 Inches Maximum
Overall Length [ABHP]
0.7150 Inches Minimum And 0.7200 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]
Guide
Style Designator [STYL]
Solid, External Flanges Both Ends

3120-01-531-7568 Management Data Management Data 3120-01-531-7568

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jul 2005
Department of the Air Force (DF)
EA
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3120-01-531-7568 Freight Data Freight Information 3120-01-531-7568

3120-01-531-7568 has freight characteristics.. 3120-01-531-7568 has a variance between NMFC and UFC when transported by rail and the description should be consulted.