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5306-00-350-3012

Machine Bolt

5306003503012 003503012 97D 19W0664 83988

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

5306-00-350-3012 BOLT,MACHINE 5306003503012 003503012

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
19
NATO Data Quality
5306-00-350-3012 BOLT,MACHINE 5306003503012 003503012 1/1
NSN 5306-00-350-3012 (Generic Image) 1/1

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5306-00-350-3012 Demil Restrictions 5306-00-350-3012

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

5306-00-350-3012 is a Machine 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.

5306-00-350-3012 HTS and ScheduleB Import and Export 5306-00-350-3012

5306-00-350-3012 End Users End Users 5306-00-350-3012

New Zealand (ZE01)
Effective Date:
1 Apr 1991

5306-00-350-3012 Manufacturers Approved Sources 5306-00-350-3012

5306-00-350-3012 Technical Data Datasheet 5306-00-350-3012

Characteristic
Specifications
Fastener Length [AASB]
2.125 Inches Nominal
Features Provided [CBBL]
Finished Head
Grip Length [ANEE]
1.000 Inches Nominal
Hardness Rating [CQFM]
30.0 Rockwell C Minimum Overall And 38.0 Rockwell C Maximum Overall
Head Height [AASU]
0.328 Inches Nominal
Head Style [AASK]
Hexagon
Material Document And Classification [MDCL]
Qq-S-624 Fed Spec Single Material Response Overall
Material [MATT]
Steel Comp 4037 Overall Or Steel Comp 4042 Overall Or Steel Comp 5140 Overall Or Steel Comp 8640 Overall
Nominal Thread Diameter [AHYM]
0.438 Inches
Width Between Flats [AATB]
0.625 Inches Nominal
Surface Treatment [SFTT]
Cadmium Overall Or Zinc Overall
Thread Direction [AAJF]
Right-Hand
Thread Class [AAJD]
3A
Thread Length [AASA]
1.125 Inches Minimum
Thread Quantity Per Inch [CMLP]
14
Thread Series Designator [THSD]
Unc

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5306-00-350-3012 Freight Data Freight Information 5306-00-350-3012

5306-00-350-3012 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 093486. A Sub NMFC of Z. It has a NMFC Description of BOLTS,NUTS OR SCREWS, NOI (SUB 3). 5306-00-350-3012 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5306-00-350-3012 is rated as class 50 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 48950 which rates the freight between FCL and LCL. 5306-00-350-3012 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. 5306-00-350-3012 is not classified as a special type of cargo when transported by water. 5306-00-350-3012 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.