5306-99-037-0749

Machine Bolt

5306990370749 990370749 9102540338 ME262D

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

5306-99-037-0749 BOLT,MACHINE 5306990370749 990370749

Managed by United Kingdom
NSN Created on 13 Oct 1997
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5306-99-037-0749 BOLT,MACHINE 5306990370749 990370749 1/1
NSN 5306-99-037-0749 (Generic Image) 1/1

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9102540338 ME262D An externally threaded fastener designed for insertion through holes in assembled
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RQST NE Updated Every Day 5306-99-037-0749 RQST Updated Every Day 5306-99-037-0749 RQST NE Related Documents
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-99-624-6218Nonaircraft Gas Turbine Engine Turbine Assembly2835996246218 996246218 JRC2204 ME217D ME262D
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www.nsnlookup.com /fsg-28/fsc-2835/uk 2835-99-624-6218 https//www.nsnlookup.com /fsg-53/fsc-5306/uk 5306-99-037-0749
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DAC 2 ME217D K0582 - Ministry Of Defence (Navy), Dlo, (Active) NATO Reference RNCC 6 RNVC 9 DAC 9 ME262D
2835-01-677-0270 2835016770270 016770270 is consists of one or more stages of rotor, turbine, nonaircraft gas turbine engine and nozzle assembly, turbine, nonaircraft gas turbine engine.

5306-99-037-0749 Demil Restrictions 5306-99-037-0749

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

5306-99-037-0749 is a Machine Bolt

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