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5306-00-818-7516
Shear Bolt
5306008187516 008187516 NAS1304-18
A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. The head is designed to accommodate an external wrench or driver. The head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. The unthreaded portion is of specific grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. Items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015) of an inch (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the Screw Thread Standards, FED STD H28 and/or other nationally recognized standards. A locking feature may be incorporated in the design of the head or threads. See BOLT, MACHINE and BOLT, CLEVIS. View more Shear Bolt
June 2023
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Related Documents 5306-00-818-7516 5+ Documents (More...)
Shear Bolt 5306008187516 008187516,NAS1304-18 5306-00-818-7516 5306008187516 008187516 is a high
Shear Bolt 5306008187516 008187516,NAS1304-18 5306-00-818-7516 5306008187516 008187516 is a high
Shear Bolt 5306008187516 008187516,NAS1304-18 5306-00-818-7516 5306008187516 008187516 is a high
Shear Bolt 5306008187516 008187516,NAS1304-18 5306-00-818-7516 5306008187516 008187516 is a high
Restrictions 5306-00-818-7516
5306-00-818-7516 is a Shear Bolt 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. This item does not contain a precious metal.
Import and Export 5306-00-818-7516
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5306-00-818-7516
- Brazil (YA01)
- Effective Date:
- 1 Jan 2011
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Columbia (YC01)
- Effective Date:
- 1 Jul 2015
- Singapore (YJ01)
- Effective Date:
- 1 Apr 1991
- Kuwait (YK01)
- Effective Date:
- 1 Jan 2015
- Malaysia (YW01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC01)
- Effective Date:
- 1 Apr 2013
- New Zealand (ZE01)
- Effective Date:
- 1 Nov 2003
- France (ZF01)
- Effective Date:
- 1 Apr 1991
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
- United Kingdom (ZK01)
- Effective Date:
- 1 May 1998
- Denmark (ZS01)
- Effective Date:
- 1 Mar 2002
- Norway (ZT01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 5306-00-818-7516
- Part Number
- Manufacturer
- Status
- NAS1304-18
- Manufacturer
- 80205 - National Aerospace Standards (Active)
- Primary Buy
- Primary Buy
Datasheet 5306-00-818-7516
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Fastener Length [AASB]
- 1.550 Inches Nominal
- Grip Diameter [AAUR]
- 0.2485 Inches Minimum And 0.2495 Inches Maximum
- Grip Length [ANEE]
- 1.125 Inches Nominal
- Hardness Rating [CQFM]
- 34.0 Rockwell C Minimum Overall And 40.0 Rockwell C Maximum Overall
- Head Height [AASU]
- 0.125 Inches Nominal
- Head Style [AASK]
- Dished Hexagon
- Material Document And Classification [MDCL]
- Mil-S-5626 Mil Spec 1St Material Response Overall Or Mil-S-5000 Mil Spec 2Nd Material Response Overall Or Mil-S-8503 Mil Spec 3Rd Material Response Overall Or Mil-S-6098 Mil Spec 4Th Material Response Overall Or Mil-S-6049 Mil Spec 5Th Material Response Overall
- Material [MATT]
- Steel Comp 4140 Overall Or Steel Comp E4340 Overall Or Steel Comp 6150 Overall Or Steel Comp 8735 Overall Or Steel Comp 8740 Overall
- Minimum Tensile Strength [CQBC]
- 160000 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 0.250 Inches
- Single Shear Strength [AAWU]
- 96000 Pounds Per Square Inch
- Width Between Flats [AATB]
- 0.430 Inches Minimum And 0.439 Inches Maximum
- Surface Treatment Document And Classification [STDC]
- Qq-P-416,Ty 2 Cl 2 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]
- 0.425 Inches Minimum
- Thread Series Designator [THSD]
- Unf
- Thread Quantity Per Inch [CMLP]
- 28
NATO Stock Numbers Related to 5306-00-818-7516
Freight Information 5306-00-818-7516
5306-00-818-7516 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). 5306-00-818-7516 is rated as a variable freight class 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. 5306-00-818-7516 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. 5306-00-818-7516 is not classified as a special type of cargo when transported by water. 5306-00-818-7516 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.