5306-27-036-9732

Machine Bolt

5306270369732 270369732 1543412

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

5306-27-036-9732 BOLT,MACHINE 5306270369732 270369732

Managed by Turkey
NSN Created on 9 Jul 2007
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
5306-27-036-9732 BOLT,MACHINE 5306270369732 270369732 1/1
NSN 5306-27-036-9732 (Generic Image) 1/1

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5306-27-036-9732 Related Documents Related Documents 5306-27-036-9732 5+ Documents (More...)

(CAGE Code T0528) DAC: 3 3 Jul 2007 5306-27-036-9732 Machine Bolt 1543412RNCC: 2 | RNVC: 1 | DAC: 3 9
4720-66-154-3412 4720661543412 661543412 is a length of nonmetallic hose with fittings on one or both ends. for items without fittings, see hose, nonmetallic. excludes hose assembly, air duct; and hose assembly, air duct, air breathing.
3110-33-154-3412 3110331543412 331543412 is a nonadjustable roller bearing consisting of a single or multiple-row of hardened cylindrical rollers and a retainer used with or without inner or oute r rings. excludes bearing, roller, airframe.
1560-01-154-3412 1560011543412 011543412 is a flat or preformed item of metallic or nonmetallic material. it may vary in shape and its surface may be smooth and/or serrated. its thickness is small in comparison to both its length and width. it is designed to be mounted upon a surface or between two surfaces. its primary function is to strengthen, join, or separate aircraft structural parts. excludes plate, mending; shim; and spacer, plate.

5306-27-036-9732 Demil Restrictions 5306-27-036-9732

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

5306-27-036-9732 is a Machine Bolt

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