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5306-01-056-8750

Externally Relieved Body Bolt

5306010568750 010568750 337062

An externally threaded fastener whose threaded portion is of one nominal diameter, and whose unthreaded portion has been machined or ground in one or more places or over its entire length to a maximum diameter less than the minimum pitch diameter of the thread (excludes undercuts for thread relief). It is No. 10 (0.190 IN.) (5 mm) or larger in size and has a head which is not designed to be held or driven with an inserted driver or designed for rotation by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. Excludes BOLT, INTERNAL WRENCHING and THUMBSCREW. See also SCREW, EXTERNALLY RELIEVED BODY. View more Externally Relieved Body Bolt

5306-01-056-8750 BOLT,EXTERNALLY RELIEVED BODY 5306010568750 010568750

Managed by United States
NSN Created on 3 Mar 1978
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
5306-01-056-8750 BOLT,EXTERNALLY RELIEVED BODY 5306010568750 010568750 1/1
NSN 5306-01-056-8750 (Generic Image) 1/1

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5306-01-056-8750 Related Documents Related Documents 5306-01-056-8750 5+ Documents (More...)

01-074-3665 Externally Relieved Body Bolt 3-140-013-03RNCC: 3 | RNVC: 2 | DAC: 5 30 Mar 1979 5306-01-056-8750
1560-99-430-8733 1560994308733 994308733 is an item designed as a principal member of various primary structures within an aircraft. it provides strength, rigidity and the like while maintaining the proper dimensional distances as required. it may include holes for mounting and/or joining to other items to form an assembly.
1560-99-301-1457 1560993011457 993011457 is an item designed as a principal member of various primary structures within an aircraft. it provides strength, rigidity and the like while maintaining the proper dimensional distances as required. it may include holes for mounting and/or joining to other items to form an assembly.
1560-99-931-0064 1560999310064 999310064 is a light, secondary structural member that does not completely partition various components such as the fuselage, boom, wing, and the like. it is designed to give cross-sectional shape and strength to the item of which it is a part.
1560-99-881-8165 1560998818165 998818165 is an item of various configuration that is an integral member of the airframe structure. it is specifically designed for the purpose of maintaining, positioning, joining, and strengthening the aircraft structure. it may include holes for mounting purposes or to form an assembly.

5306-01-056-8750 Demil Restrictions 5306-01-056-8750

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

5306-01-056-8750 is a Externally Relieved Body Bolt that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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. The precious metals content of this item is unknown.

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