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5306-00-423-8121

Machine Bolt

5306004238121 004238121 M276 S1614 0S-1614 0S1614

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

5306-00-423-8121 BOLT,MACHINE 5306004238121 004238121

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
28
NATO Data Quality
AASK Style C1 for 5306-00-423-8121 1/1
NSN 5306-00-423-8121 (Identification) 1/1

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S1614 M276 0S-1614 0S1614 An externally threaded fastener designed for insertion through holes in assembled
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5306-00-423-8121 Demil Restrictions 5306-00-423-8121

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

5306-00-423-8121 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.

5306-00-423-8121 HTS and ScheduleB Import and Export 5306-00-423-8121

5306-00-423-8121 End Users End Users 5306-00-423-8121

Brazil (YA01)
Effective Date:
1 Mar 2010
Spain (YB01)
Effective Date:
1 Apr 1991
Australia (ZA01)
Effective Date:
1 Apr 1991
New Zealand (ZE01)
Effective Date:
1 Apr 1991
France (ZF01)
Effective Date:
1 Apr 1991
United Kingdom (ZK01)
Effective Date:
1 Jul 2000
Greece (ZU01)
Effective Date:
1 Jul 1995
Turkey (ZW01)
Effective Date:
1 Nov 1998

5306-00-423-8121 Manufacturers Approved Sources 5306-00-423-8121

5306-00-423-8121 Technical Data Datasheet 5306-00-423-8121

Characteristic
Specifications
FIIG
A003B0
Head Style [AASK]
Hexagon
Thread Series Designator [THSD]
Unc
Nominal Thread Diameter [AHYM]
0.250 Inches
Thread Quantity Per Inch [CMLP]
20
Thread Class [AAJD]
2A
Thread Direction [AAJF]
Right-Hand
Thread Length [AASA]
0.500 Inches Maximum
Fastener Length [AASB]
0.500 Inches Nominal
Material [MATT]
Steel Overall
Hardness Rating [CQFM]
30.0 Rockwell C Nominal Overall
Minimum Yield Strength [CQHQ]
145000 Pounds Per Square Inch
Head Height [AASU]
0.188 Inches Nominal
Width Between Flats [AATB]
0.438 Inches Nominal
Features Provided [CBBL]
Finished Head

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5306-00-423-8121 Freight Data Freight Information 5306-00-423-8121

5306-00-423-8121 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). 5306-00-423-8121 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5306-00-423-8121 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. 5306-00-423-8121 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. 5306-00-423-8121 is not classified as a special type of cargo when transported by water. 5306-00-423-8121 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.