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5306-00-150-9535

Machine Bolt

5306001509535 001509535 B6812 AN5-74A

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

5306-00-150-9535 BOLT,MACHINE 5306001509535 001509535

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
May 2023
NATO Update Count
9
NATO Data Quality
AASK Style C1 for 5306-00-150-9535 1/1
NSN 5306-00-150-9535 (Identification) 1/1

5306-00-150-9535 Stock and Availability Marketplace 5306-00-150-9535

5306-00-150-9535 Related Documents Related Documents 5306-00-150-9535 5+ Documents (More...)

B6812 AN5-74A An externally threaded fastener designed for insertion through holes in assembled parts
B6812 BOLT,MACHINE 49 EA NS Request Quotation Updated Every Day 5306-00-150-9535 RQST NE Updated Every
Day 5306-00-150-9535 RQST Updated Every Day 5306-00-150-9535 RQST NE Related Documents 5306-00-150-9535
B6812 BOLT,MACHINE 116 EA NS Request Quotation Subscribe to View Vendor Details...
B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe to View Vendor Details...
/fsg-53/fsc-5306/us 5306-00-150-9534 Machine Bolt 5306001509534 001509534,B6812 B6812 BOLT,MACHINE 116
B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe to View Vendor Details...
B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe to View Vendor Details...
Machine Bolt 5306001509535 001509535,B6812 B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe
B6812 BOLT,MACHINE 116 EA NS Request Quotation Subscribe to View Vendor Details...
B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe to View Vendor Details...
B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe to View Vendor Details...
Machine Bolt 5306001509535 001509535,B6812B6812 BOLT,MACHINE 116 https//www.nsnlookup.com /cage
B6812 BOLT,MACHINE 12 EA NS Request Quotation Subscribe to View Vendor Details...
/fsg-53/fsc-5306/us 5306-00-151-1146 Machine Bolt 5306001511146 001511146,B6812 B6812 BOLT,MACHINE 116

5306-00-150-9535 Demil Restrictions 5306-00-150-9535

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

5306-00-150-9535 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.

5306-00-150-9535 End Users End Users 5306-00-150-9535

Brazil (YA01)
Effective Date:
1 Aug 2000
Canada (ZC01)
Effective Date:
1 Apr 1991

5306-00-150-9535 Manufacturers Approved Sources 5306-00-150-9535

5306-00-150-9535 Technical Data Datasheet 5306-00-150-9535

Characteristic
Specifications
FIIG
A003B0
Fastener Length [AASB]
7.578 Inches Minimum And 7.625 Inches Maximum
Features Provided [CBBL]
Finished Head
Grip Length [ANEE]
7.047 Inches Minimum And 7.078 Inches Maximum
Hardness Rating [CQFM]
26.0 Rockwell C Minimum Overall And 32.0 Rockwell C Maximum Overall
Head Height [AASU]
0.172 Inches Minimum And 0.204 Inches Maximum
Head Style [AASK]
Hexagon
Material Document And Classification [MDCL]
Mil-S-5626 Mil Spec 1St Material Response Overall Or Mil-S-6049 Mil Spec 2Nd Material Response Overall Or Mil-S-6050 Mil Spec 3Rd Material Response Overall Or Mil-S-6098 Mil Spec 4Th Material Response Overall Or Mil-S-6758 Mil Spec 5Th Material Response Overall Or Ams 6300 Assn Std 6Th Material Response Overall
Material [MATT]
Steel Comp 4140 Overall Or Steel Comp 8740 Overall Or Steel Comp 8630 Overall Or Steel Comp 8735 Overall Or Steel Comp 4130 Overall Or Steel Comp 4037 Overall
Minimum Tensile Strength [CQBC]
125000 Pounds Per Square Inch
Nominal Thread Diameter [AHYM]
0.312 Inches
Width Between Flats [AATB]
0.490 Inches Minimum And 0.502 Inches Maximum
Surface Treatment Document And Classification [STDC]
Qq-P-416 Ty2 Cl3 Fed Spec Single Treatment Response Overall
Surface Treatment [SFTT]
Cadmium Overall And Chromate Overall
Thread Class [AAJD]
3A
Thread Direction [AAJF]
Right-Hand
Thread Length [AASA]
0.500 Inches Minimum And 0.578 Inches Maximum
Thread Quantity Per Inch [CMLP]
24
Thread Series Designator [THSD]
Unf

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5306-00-150-9535 Freight Data Freight Information 5306-00-150-9535

5306-00-150-9535 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). 5306-00-150-9535 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5306-00-150-9535 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. 5306-00-150-9535 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. 5306-00-150-9535 is not classified as a special type of cargo when transported by water. 5306-00-150-9535 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.