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5306-00-900-2518
Machine Bolt
5306009002518 009002518 AN20-45A
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
January 2023
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Marketplace 5306-00-900-2518
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Restrictions 5306-00-900-2518
5306-00-900-2518 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.
Import and Export 5306-00-900-2518
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5306-00-900-2518
- NASA (G860)
- Effective Date:
- 1 Apr 1991
Approved Sources 5306-00-900-2518
- Part Number
- Manufacturer
- Status
- AN20-45A
- Manufacturer
- 88044 - Aeronautical Standards Group (Active)
- Definitive Standard
- Definitive Standard
Datasheet 5306-00-900-2518
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Fastener Length [AASB]
- 4.812 Inches Nominal
- Features Provided [CBBL]
- Finished Head
- Grip Length [ANEE]
- 3.125 Inches Nominal
- Hardness Rating [CQFM]
- 26.0 Rockwell C Minimum Overall And 32.0 Rockwell C Maximum Overall
- Head Height [AASU]
- 0.640 Inches Minimum And 0.672 Inches Maximum
- Head Style [AASK]
- Hexagon
- Material [MATT]
- Steel Comp 4037 Overall Or Steel Comp 4130 Overall Or Steel Comp 8630 Overall Or Steel Comp 8735 Overall Or Steel Comp 8740 Overall Or Steel Comp 4140 Overall
- Minimum Tensile Strength [CQBC]
- 125000 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 1.250 Inches
- Material Document And Classification [MDCL]
- Mil-B-6812 Mil Spec All Material Responses Overall
- Width Between Flats [AATB]
- 1.802 Inches Minimum And 1.815 Inches Maximum
- Surface Treatment [SFTT]
- Cadmium Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 1.687 Inches Minimum
- Thread Series Designator [THSD]
- Unf
- Thread Quantity Per Inch [CMLP]
- 12
NATO Stock Numbers Related to 5306-00-900-2518
Freight Information 5306-00-900-2518
5306-00-900-2518 has freight characteristics.. 5306-00-900-2518 has a variance between NMFC and UFC when transported by rail and the description should be consulted.