5340-00-836-9775

Helical Compression Spring Seat

5340008369775 008369775 113B4002P1

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

5340-00-836-9775 SEAT,HELICAL COMPRESSION SPRING 5340008369775 008369775

Managed by United States
NSN Created on 5 Dec 1966
Data Last Changed
November 2023
NATO Update Count
11
NATO Data Quality
5340-00-836-9775 SEAT,HELICAL COMPRESSION SPRING 5340008369775 008369775 1/1
NSN 5340-00-836-9775 (Generic Image) 1/1

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5340-00-836-9775 Related Documents Related Documents 5340-00-836-9775 1+ Documents (More...)

25 Jul 1973 4920-00-586-7817 Preflight Checker 196C368G1RNCC: 3 | RNVC: 2 | DAC: 5 1 Jan 1963 5340-00-836-9775

5340-00-836-9775 Demil Restrictions 5340-00-836-9775

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

5340-00-836-9775 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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