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5305-00-069-0301
Socket Head Cap Screw
5305000690301 000690301 1C6368P06 46068-04046S NAS1352C04-6 947463-406 947463-0406 B68161 15650103-6 10124957
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
57
Marketplace 5305-00-069-0301
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Updated Every Day Related Documents 5305-00-069-0301 2+ Documents (More...)
NAS1352C04-6 SCREW,CAP,SOCKET HEAD 674 EA NS Request Quotation Updated Every Day 5305-00-069-0301 RQST
NE Updated Every Day 5305-00-069-0301 RQST Updated Every Day 5305-00-069-0301 RQST NE Related Documents
4806-030 92200A108 12-Z-1007-3 N171P9006-1 1C6368P06 NASM16995-10 MS16995-10 352250020266 011924 140300200
MS16995-10 SCREW,CAP,SOCKET HEAD 1200 HD NS Request Quotation NAS1352C04-6 SCREW,CAP,SOCKET HEAD 500
Restrictions 5305-00-069-0301
5305-00-069-0301 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 5305-00-069-0301
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-00-069-0301
- Finland (WF01)
- Effective Date:
- 1 May 2009
- Brazil (YA01)
- Effective Date:
- 1 Dec 2008
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Columbia (YC01)
- Effective Date:
- 1 Jul 2015
- Israel (YD01)
- Effective Date:
- 1 Apr 1991
- Singapore (YJ01)
- Effective Date:
- 1 Apr 1991
- Saudi Arabia (YS01)
- Effective Date:
- 1 Feb 2015
- Malaysia (YW01)
- Effective Date:
- 1 Aug 1997
- Belgium (ZB01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
- South Africa (ZD01)
- Effective Date:
- 1 Oct 2009
- New Zealand (ZE01)
- Effective Date:
- 1 Apr 1991
- France (ZF01)
- Effective Date:
- 1 Jun 2015
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Aug 1995
- United Kingdom (ZK01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Dec 1995
- NATO Maintenance and Supply Agency (ZX01)
- Effective Date:
- 1 Mar 2003
Approved Sources 5305-00-069-0301
- Part Number
- Manufacturer
- Status
- 46068-04046S
- Manufacturer
- 27914 - Honeywell International Inc (Active)
- Primary Buy
- Primary Buy
- NAS1352C04-6
- 80205 - National Aerospace Standards (Active)
- Primary Buy
- Primary Buy
- 947463-406
- 06481 - Northrop Grumman Systems Corporation (Active)
- Secondary Buy
- Secondary Buy
- 947463-0406
- 06481 - Northrop Grumman Systems Corporation (Active)
- Secondary Buy
- Secondary Buy
- B68161
- K0967 - Mbda Uk Ltd (Active)
- Secondary Buy
- Secondary Buy
- 15650103-6
- F6151 - Safran (Active)
- Secondary Buy
- Secondary Buy
- 947463-406
- 13973 - Litton Systems Inc. Div Navigation (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 10124957
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
- 1C6368P06
- 07482 - General Electric Company (Active)
- Advisory Reference
- Advisory Reference
Datasheet 5305-00-069-0301
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Fastener Length [AASB]
- 0.375 Inches Nominal
- Hardness Rating [CQFM]
- 80.0 Rockwell B Minimum Overall
- Head Diameter [AASL]
- 0.176 Inches Minimum And 0.183 Inches Maximum
- Head Height [AASU]
- 0.108 Inches Minimum And 0.112 Inches Maximum
- Head Style [AASK]
- Flat Chamfer
- Material [MATT]
- Steel Comp 302 Overall Or Steel Comp 303 Overall Or Steel Comp 304 Overall Or Steel Comp 305 Overall Or Steel Comp 316 Overall
- Minimum Tensile Strength [CQBC]
- 80000 Pounds Per Square Inch
- Minimum Yield Strength [CQHQ]
- 30000 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 0.112 Inches
- Internal Drive Style [ABQZ]
- Hexagon
- Material Document And Classification [MDCL]
- 66 Fed Std All Material Responses Overall
- Width Across Flats [ASDB]
- 0.094 Inches Minimum And 0.095 Inches Maximum
- Surface Treatment Document And Classification [STDC]
- Qq-P-35 Fed Spec Single Treatment Response Overall
- Surface Treatment [SFTT]
- Passivate Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.341 Inches Minimum And 0.375 Inches Maximum
- Thread Quantity Per Inch [CMLP]
- 40
- Thread Series Designator [THSD]
- Unc
DLA Procurement Analysis 5305-00-069-0301
NATO Stock Numbers Related to 5305-00-069-0301
Freight Information 5305-00-069-0301
5305-00-069-0301 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). 5305-00-069-0301 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5305-00-069-0301 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. 5305-00-069-0301 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. 5305-00-069-0301 is not classified as a special type of cargo when transported by water. 5305-00-069-0301 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.