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5310-00-676-8907

Hexagon Plain Nut

5310006768907 006768907 210-16 1787815PC8

A nut, flat on top and bottom having 6 flat sides. For items which have internal tapered or straight (parallel) pipe threads, specific electrical conduit size designation, and which when installed, provide a method of tightening to lock the connection, see LOCKNUT, ELECTRICAL CONDUIT. See also LOCKNUT, TUBE FITTING. For items having a thickness (or height) exceeding two times the width across the flats, use POST, ELECTRICAL-MECHANICAL EQUIPMENT. (When height or thickness and/or width across the flats is designated as a tolerance dimension, the maximum dimension will be used to determine compliance.) View more Hexagon Plain Nut

5310-00-676-8907 NUT,PLAIN,HEXAGON 5310006768907 006768907

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
12
NATO Data Quality
ACTA Style A12 for 5310-00-676-8907 1/1
NSN 5310-00-676-8907 (Identification) 1/1

5310-00-676-8907 Stock and Availability Marketplace 5310-00-676-8907

5310-00-676-8907 Related Documents Related Documents 5310-00-676-8907 5+ Documents (More...)

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-5 KP1838-210-16 190002210 https//www.nsnlookup.com /fsg-53/fsc-5310/us 5310-00-676-8907 Hexagon Plain
1560-14-416-8441 1560144168441 144168441 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.
1560-14-429-2797 1560144292797 144292797 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.
1560-14-459-2326 1560144592326 144592326 is a rigid or flexible item of various shapes attached to a structure for the purpose of providing access for inspection, service, replacement of components and/or adjustments or mounting operations. it is designed to be attached by means of bolt holes, slots, mounting ears, tabs, and the like. to permit access, the mounted cover requires partial or complete removal. it may include an observation window. for items permanently attached by hinges and the like, see door, access (as modified). excludes all covers not specifically designed to provide access for the purposes listed above.

5310-00-676-8907 Demil Restrictions 5310-00-676-8907

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

5310-00-676-8907 is a Hexagon Plain Nut that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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.

5310-00-676-8907 HTS and ScheduleB Import and Export 5310-00-676-8907

5310-00-676-8907 End Users End Users 5310-00-676-8907

Spain (YB01)
Effective Date:
23 Feb 1992
Turkey (ZW01)
Effective Date:
1 Dec 2005

5310-00-676-8907 Manufacturers Approved Sources 5310-00-676-8907

5310-00-676-8907 Technical Data Datasheet 5310-00-676-8907

Characteristic
Specifications
FIIG
A021A0
Bearing Surface Type [CRTM]
Chamfered Or Washer Faced
Material Document And Classification [MDCL]
Qq-S-633 Fed Spec Single Material Response Overall
Material [MATT]
Steel Comp 1018 Overall
Nominal Thread Size [CQJX]
1.500 Inches
Nut Height [ADEA]
0.406 Inches Nominal
Nut Style [ACTA]
Hexagon
Width Across Flats [ASDB]
1.750 Inches Nominal
Surface Treatment [SFTT]
Phosphate Overall
Thread Direction [AAJF]
Right-Hand
Thread Class [AAJD]
2B
Thread Quantity Per Inch [CMLP]
12
Thread Series [BZRR]
Unf

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5310-00-676-8907 Freight Data Freight Information 5310-00-676-8907

5310-00-676-8907 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 093483. A Sub NMFC of X. It has a NMFC Description of BOLTS,NUTS OR SCREWS,NOI IRON OR. 5310-00-676-8907 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 48950 which rates the freight between FCL and LCL. 5310-00-676-8907 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 573 for ocean manifesting and military sealift. 5310-00-676-8907 is not classified as a special type of cargo when transported by water. 5310-00-676-8907 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.