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5340-00-362-8400

Helical Compression Spring Seat

5340003628400 003628400 22013A 5163247 51996 2BL049 1A9730 512066 A163247 112066 643425 41459

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

5340-00-362-8400 SEAT,HELICAL COMPRESSION SPRING 5340003628400 003628400

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
31
NATO Data Quality
STYL Style N5 for 5340-00-362-8400 1/1
NSN 5340-00-362-8400 (Identification) 1/1

5340-00-362-8400 Stock and Availability Marketplace 5340-00-362-8400

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5340-00-362-8400 Related Documents Related Documents 5340-00-362-8400 5+ Documents (More...)

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5340-00-362-8400 Demil Restrictions 5340-00-362-8400

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

5340-00-362-8400 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.

5340-00-362-8400 End Users End Users 5340-00-362-8400

Austria (WB01)
Effective Date:
1 Feb 2005
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Nov 1998

5340-00-362-8400 Manufacturers Approved Sources 5340-00-362-8400

5340-00-362-8400 Technical Data Datasheet 5340-00-362-8400

Characteristic
Specifications
FIIG
T319-E
Distance From End To First Step [BZDH]
0.1250 Inches Nominal
End Diameter [BBRB]
0.5630 Inches Nominal
Bore Diameter [ABXV]
0.3760 Inches Minimum And 0.3780 Inches Maximum
Counterbore Diameter [AAWY]
0.5930 Inches Minimum And 0.5980 Inches Maximum
Counterbore Length [BZDL]
0.1880 Inches Nominal
Design Type [APGF]
Solid
First Step Diameter [ABPR]
0.7800 Inches Minimum And 0.7900 Inches Maximum
First Step Length [ABPS]
0.2190 Inches Nominal
Material Document And Classification [MDCL]
Sae 1112 Assn Std Single Material Response
Material [MATT]
Steel Comp 1212
Fsc Application Data [ZZZV]
Engine,Gasoline,Non-Aircraft
Second Step Diameter [ABPT]
1.0310 Inches Nominal
Overall Height [ABKW]
0.4380 Inches Nominal
Special Features [FEAT]
Not Casehardened
Style Designator [STYL]
Seat

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5340-00-362-8400 Freight Data Freight Information 5340-00-362-8400

5340-00-362-8400 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133300. A Sub NMFC of Z. It has a NMFC Description of MACHINERY/MACHINES NOI. 5340-00-362-8400 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5340-00-362-8400 is rated as class 85 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 5340-00-362-8400 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 593 for ocean manifesting and military sealift. 5340-00-362-8400 is not classified as a special type of cargo when transported by water. 5340-00-362-8400 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.