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5306-01-516-5538

Machine Bolt

5306015165538 015165538 MS14181-04011L

An externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. The threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. The head is not designed to be held or driven with an inserted driver or by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. Head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. For items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, BOLT, SHEAR. See also SCREW, CAP, HEXAGON HEAD and SCREW, MACHINE. View more Machine Bolt

5306-01-516-5538 BOLT,MACHINE 5306015165538 015165538

Managed by United States
NSN Created on 9 Jan 2004
Data Last Changed
May 2023
NATO Update Count
1
NATO Data Quality
5306-01-516-5538 BOLT,MACHINE 5306015165538 015165538 1/1
NSN 5306-01-516-5538 (Generic Image) 1/1

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5306-01-516-5538 Demil Restrictions 5306-01-516-5538

DEMIL: A | DEMILI: 7 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

5306-01-516-5538 is a Machine Bolt that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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 is not suspected to be hazardous. This item does not contain a precious metal.

5306-01-516-5538 End Users End Users 5306-01-516-5538

US Air Force (FLL5)
Effective Date:
1 Jan 2004

5306-01-516-5538 Manufacturers Approved Sources 5306-01-516-5538

5306-01-516-5538 Technical Data Datasheet 5306-01-516-5538

Characteristic
Specifications
FIIG
A003B0
End Item Identification [AGAV]
F-22
Part Name Assigned By Controlling Agency [CXCY]
Bolt,Machine

5306-01-516-5538 Management Data Management Data 5306-01-516-5538

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2022
Department of the Air Force (DF)
EA
Subscribe
1
Aug 2018
Department of the Air Force (DF)
EA
Subscribe
1

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5306-01-516-5538 Freight Data Freight Information 5306-01-516-5538

5306-01-516-5538 has freight characteristics.. 5306-01-516-5538 has a variance between NMFC and UFC when transported by rail and the description should be consulted.