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5305-00-271-2005
Socket Head Cap Screw
5305002712005 002712005 AN148660
An externally threaded fastener whose threaded portion is of one nominal diameter. The head has an internal socket or multiple spline for use with an inserted driver. A locking feature may be incorporated in the design of the head or threads. Excludes items with bevel (conical) heads. See BOLT, INTERNAL WRENCHING. Excludes SCREW, SHOULDER; and SCREW, MACHINE. View more Socket Head Cap Screw
January 2023
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Related Documents 5305-00-271-2005 1+ Documents (More...)
(Active) Primary Buy RNCC 3 RNVC 2 DAC 1 AN148660 88044 - Aeronautical Standards Group (Active) Incomplete
Restrictions 5305-00-271-2005
5305-00-271-2005 is a Socket Head Cap Screw 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. The precious metals content of this item is unknown.
Import and Export 5305-00-271-2005
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-00-271-2005
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Denmark (ZS01)
- Effective Date:
- 1 Apr 1991
Approved Sources 5305-00-271-2005
- Part Number
- Manufacturer
- Status
- AN148660
- Manufacturer
- 88044 - Aeronautical Standards Group (Active)
- Definitive Standard
- Definitive Standard
Datasheet 5305-00-271-2005
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Fastener Length [AASB]
- 0.750 Inches Nominal
- Hardness Rating [CQFM]
- 32.0 Rockwell C Minimum Overall And 36.0 Rockwell C Maximum Overall
- Head Diameter [AASL]
- 0.438 Inches Nominal
- Head Height [AASU]
- 0.260 Inches Nominal
- Head Style [AASK]
- Flat Chamfer
- Hole Configuration Style [CRHC]
- Round
- Hole Diameter [AAUB]
- 0.070 Inches Nominal
- Hole Quantity [ASXK]
- 6
- Hole Type [BQDM]
- Drilled
- Material [MATT]
- Steel Comp 8740 Overall
- Nominal Thread Diameter [AHYM]
- 0.250 Inches
- Internal Drive Style [ABQZ]
- Hexagon
- Material Document And Classification [MDCL]
- Ams 6322 Assn Std Single Material Response Overall
- Width Across Flats [ASDB]
- 0.219 Inches Minimum And 0.221 Inches Maximum
- Surface Finish [CSYM]
- 32.0 Microinches Threads
- Surface Finish [CSYM]
- 63.0 Microinches Bearing Surface Of Head
- Surface Treatment Document And Classification [STDC]
- Ams 2400 Assn Std Single Treatment Response Overall
- Surface Treatment [SFTT]
- Cadmium Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.679 Inches Minimum
- Thread Quantity Per Inch [CMLP]
- 28
- Thread Series Designator [THSD]
- Unf
NATO Stock Numbers Related to 5305-00-271-2005
Freight Information 5305-00-271-2005
5305-00-271-2005 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). 5305-00-271-2005 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. 5305-00-271-2005 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 713 for ocean manifesting and military sealift. 5305-00-271-2005 is not classified as a special type of cargo when transported by water. 5305-00-271-2005 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.