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5340-01-257-7247

Helical Compression Spring Seat

5340012577247 012577247 31073

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

5340-01-257-7247 SEAT,HELICAL COMPRESSION SPRING 5340012577247 012577247

Managed by United States
NSN Created on 23 Jun 1987
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
5340-01-257-7247 SEAT,HELICAL COMPRESSION SPRING 5340012577247 012577247 1/1
NSN 5340-01-257-7247 (Generic Image) 1/1

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6220-14-387-2569Aircraft Navigational Light6220143872569 143872569 704A46-8310-15 610-1463 31-073 31073
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-04-2 1065-31073-04-1 A definite length of CABLE, RADIO FREQUENCY having one or both ends processed

5340-01-257-7247 Demil Restrictions 5340-01-257-7247

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

5340-01-257-7247 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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