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5340-01-052-5609

Helical Compression Spring Seat

5340010525609 010525609 164B8260P1

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

5340-01-052-5609 SEAT,HELICAL COMPRESSION SPRING 5340010525609 010525609

Managed by United States
NSN Created on 15 Dec 1977
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
5340-01-052-5609 SEAT,HELICAL COMPRESSION SPRING 5340010525609 010525609 1/1
NSN 5340-01-052-5609 (Generic Image) 1/1

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5340-01-052-5609 Related Documents Related Documents 5340-01-052-5609 1+ Documents (More...)

4920-01-021-2934 Aircraft Maintenance Fixture 113D9047G1RNCC: 3 | RNVC: 2 | DAC: 4 12 May 1976 5340-01-052-5609

5340-01-052-5609 Demil Restrictions 5340-01-052-5609

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

5340-01-052-5609 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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