5306-21-846-8930
Machine Bolt
5306218468930 218468930 AN10-37A AN10-37AM
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
Managed by Canada
NSN Created on 6 Jun 1968
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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AN10-37A AN10-37AM An externally threaded fastener designed for insertion through holes in assembled
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-21-846-8930Machine Bolt5306218468930 218468930 AN10 -37A AN10-37AM An externally threaded fastener designed
Restrictions 5306-21-846-8930
Approved Sources 5306-21-846-8930
- Part Number
- Manufacturer
- Status
- AN10-37A
- Manufacturer
- 88044 - Aeronautical Standards Group (Active)
- Related Standard
- Related Standard
- AN10-37AM
- 35925 - Transport Canadamateriel And (Active)
- Primary Buy
- Primary Buy
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