3120-14-344-9761

Sleeve Bearing

3120143449761 143449761 BP25C16-20X20 428210 ST406M41P103 4111-07 4111-0700 BAZM00241

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

3120-14-344-9761 BEARING,SLEEVE 3120143449761 143449761

Managed by France
NSN Created on 5 Oct 1977
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
3120-14-344-9761 BEARING,SLEEVE 3120143449761 143449761 1/1
NSN 3120-14-344-9761 (Generic Image) 1/1

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3120-14-344-9761 Related Documents Related Documents 3120-14-344-9761 5+ Documents (More...)

Documents 3120-14-393-6198 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-31/fsc-3120/fr 3120-14-344-9761
Sleeve Bearing 3120143449761 143449761 https//www.nsnlookup.com /cage Federal Mogul Operations
https//www.nsnlookup.com /cage Federal Mogul Operations France Sas (CAGE Code F0737) Jun 1984 3120-14-344-9761
Jul 1987 3120-14-393-6198 Sleeve Bearing BP25-16/20X16RNCC: 3 | RNVC: 2 | DAC: 4 7 Jun 1984 3120-14-344-9761
5841-01-084-8376 5841010848376 010848376 is two or more different types of items, having a common mounting or mounted on each other, which together form a portion of a radar set, but, which in itself is not a complete functioning item and cannot be assigned a more definite item name.
1630-01-511-2905 1630015112905 015112905 is a nonferrous forging or casting machined to support pistons with integral connecting fluid passages. provisions are provided for attachment to a brake torque tube and the aircraft landing gear strut. provisions for automatic adjusters and pressure plate return springs may be included.

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