5340-01-244-3279

Helical Compression Spring Seat

5340012443279 012443279 30100525

A circular item, usually having a flat or grooved flange, boss(es), and/or counterbore designed to accommodate the end of the spring. It is used to position the spring, but does not encase the spring or restrain lateral motion. It may be used in conjunction with a RETAINER, HELICAL COMPRESSION SPRING. Excludes WASHER (1), (as modified); SEAT, BALL SOCKET and HOLDER, SPRING. See also ROTOR, ENGINE POPPET VALVE. View more Helical Compression Spring Seat

5340-01-244-3279 SEAT,HELICAL COMPRESSION SPRING 5340012443279 012443279

Managed by United States
NSN Created on 9 Nov 1986
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
5340-01-244-3279 SEAT,HELICAL COMPRESSION SPRING 5340012443279 012443279 1/1
NSN 5340-01-244-3279 (Generic Image) 1/1

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5340-01-244-3279 Related Documents Related Documents 5340-01-244-3279 1+ Documents (More...)

14 Dec 2000 4730-01-131-8592 End Chamber Plug 28003823RNCC: 3 | RNVC: 2 | DAC: 5 18 May 1982 5340-01-244-3279

5340-01-244-3279 Demil Restrictions 5340-01-244-3279

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

5340-01-244-3279 is a Helical Compression Spring Seat that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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 may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

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