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5340-00-679-3288

Helical Compression Spring Seat

5340006793288 006793288 75232

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

5340-00-679-3288 SEAT,HELICAL COMPRESSION SPRING 5340006793288 006793288

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
17
NATO Data Quality
5340-00-679-3288 SEAT,HELICAL COMPRESSION SPRING 5340006793288 006793288 1/1
NSN 5340-00-679-3288 (Generic Image) 1/1

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Helical Compression Spring Seat 006793288 75232 A circular item, usually having a flat or grooved flange
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5340-00-679-3288 Demil Restrictions 5340-00-679-3288

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

5340-00-679-3288 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. The precious metals content of this item is unknown.

5340-00-679-3288 End Users End Users 5340-00-679-3288

New Zealand (ZE01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Nov 2005

5340-00-679-3288 Manufacturers Approved Sources 5340-00-679-3288

5340-00-679-3288 Technical Data Datasheet 5340-00-679-3288

Characteristic
Specifications
FIIG
T319-E
Distance From End To First Step [BZDH]
0.0500 Inches Minimum And 0.0700 Inches Maximum
End Diameter [BBRB]
0.6000 Inches Minimum And 0.6100 Inches Maximum
Bore Diameter [ABXV]
0.1240 Inches Minimum And 0.1280 Inches Maximum
Counterbore Diameter [AAWY]
0.4400 Inches Minimum And 0.4600 Inches Maximum
Counterbore Length [BZDL]
0.0500 Inches Minimum And 0.0600 Inches Maximum
Design Type [APGF]
Solid
First Step Diameter [ABPR]
0.7400 Inches Minimum And 0.7600 Inches Maximum
Material Document And Classification [MDCL]
Qq-A-225/6, Alloy 2024 Fed Spec Single Material Response
Material [MATT]
Aluminum Alloy 2024
Fsc Application Data [ZZZV]
Fuel Pressure Regulators,Engine,Except Aircraft And Guided Missile Prime Moving
Overall Height [ABKW]
0.1100 Inches Minimum And 0.1300 Inches Maximum
Special Features [FEAT]
Not Casehardened
Surface Treatment [SFTT]
Anodize

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5340-00-679-3288 Freight Data Freight Information 5340-00-679-3288

5340-00-679-3288 has freight characteristics.. 5340-00-679-3288 has a variance between NMFC and UFC when transported by rail and the description should be consulted.