5307-15-156-5879

Plain Stud

5307151565879 151565879 4871873

A headless fastener not exceeding 12 inches (304.8 mm) in length, threaded externally on both ends with threads of the same nominal diameter. The maximum diameter of the unthreaded portion must not be greater than the nominal thread diameter plus 0.020 inches (0.508 mm). The unthreaded portion must be without locking or wrenching provisions. It may be thread relieved. See also ROD, THREADED END and ROD, CONTINUOUS THREAD. View more Plain Stud

5307-15-156-5879 STUD,PLAIN 5307151565879 151565879

Managed by Italy
NSN Created on 28 Feb 2003
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
5307-15-156-5879 STUD,PLAIN 5307151565879 151565879 1/1
NSN 5307-15-156-5879 (Generic Image) 1/1

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5307-15-156-5879 Related Documents Related Documents 5307-15-156-5879 3+ Documents (More...)

7610-14-487-1873 7610144871873 144871873 is two or more sheets, written or printed,or stored on electonic media, containing no programs or software, outlining maintenance, installation and/or operating information applicable to one or more related pieces of equipment. it may have a cover. the sheets may be fastened by staple(s), loosely folded, and/or punched for loose-leaf binding. see also book. for single sheet items, see chart (as modified) and sheet, technical.
1560-01-487-1873 1560014871873 014871873 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.

5307-15-156-5879 Demil Restrictions 5307-15-156-5879

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

5307-15-156-5879 is a Plain Stud

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