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5305-00-150-9210
Machine Screw
5305001509210 001509210 MILS7839 1887875 515-9 AN502-10-12 890003-12
An externally threaded fastener whose threaded portion is of one nominal diameter, No 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below No. 10 (0.190 in./5 mm). No. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. A locking feature may be incorporated in the design of the head or threads. Excludes BOLT, CLEVIS; BOLT, EXTERNALLY RELIEVED BODY; SCREW, EXTERNALLY RELIEVED BODY; and SCREW, ASSEMBLED WASHER. See also, SCREW, INSTRUMENT; BOLT, MACHINE; BOLT, INTERNAL WRENCHING; and SCREW, CAP SOCKET HEAD. View more Machine Screw
January 2023
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https//www.nsnlookup.com /fsg-53/fsc-5305/us 5305-00-150-9210 Machine Screw 5305001509210 001509210
Restrictions 5305-00-150-9210
5305-00-150-9210 is a Machine 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 5305-00-150-9210
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-00-150-9210
- Brazil (YA01)
- Effective Date:
- 1 Oct 2001
- 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
- Kuwait (YK01)
- Effective Date:
- 1 Feb 2015
- Belgium (ZB01)
- Effective Date:
- 1 Apr 1991
- 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 Apr 1991
- Portugal (ZP01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
- Denmark (ZS01)
- Effective Date:
- 1 Apr 1991
- Norway (ZT01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 5305-00-150-9210
- Part Number
- Manufacturer
- Status
- AN502-10-12
- Manufacturer
- 88044 - Aeronautical Standards Group (Active)
- Definitive Standard
- Definitive Standard
- MILS7839
- 81349 - Military Specifications (Active)
- Incomplete Standard
- Incomplete Standard
- 1887875
- 24617 - General Motors Corp (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 1887875
- 77592 - General Motors Corp Rochester (Obsolete)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 515-9
- 99167 - Hamilton Sundstrand Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 890003-12
- 64547 - Honeywell International, Inc (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 890003-12
- 83298 - Allied Signal Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 890003-12
- 19315 - Honeywell Intl Inc Defense Avionics (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 5305-00-150-9210
- Characteristic
- Specifications
- FIIG
- Specifications
- A500D0
- Fastener Length [AASB]
- 0.750 Inches Nominal
- Hardness Rating [CQFM]
- 26.0 Rockwell C Minimum And 32.0 Rockwell C Maximum
- Head Diameter [AASL]
- 0.292 Inches Minimum And 0.313 Inches Maximum
- Head Height [AASU]
- 0.123 Inches Minimum And 0.130 Inches Maximum
- Head Style [AASK]
- Fillister
- Head Hole Configuration Style [CYBG]
- Round
- Hole Diameter [AAUB]
- 0.046 Inches Nominal
- Hole Quantity [ASXK]
- 1
- Minimum Tensile Strength [CQBC]
- 125000 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 0.190 Inches
- Internal Drive Style [ABQZ]
- Cross Recess Type 1
- Screw Material Document And Classification [CYAW]
- Mil-S-6050 Mil Spec Single Material Response Or An-S-9 Mil Std Single Material Response
- Screw Surface Treatment Document And Classification [CYBE]
- Qq-P-416,Ty 1,Cl 3 Fed Spec Single Treatment Response
- Screw Surface Treatment [CYBA]
- Cadmium
- Screw Material [CYAU]
- Steel Comp 8630
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.594 Inches Minimum And 0.719 Inches Maximum
- Thread Quantity Per Inch [CMLP]
- 32
- Thread Series Designator [THSD]
- Unf
NATO Stock Numbers Related to 5305-00-150-9210
Freight Information 5305-00-150-9210
5305-00-150-9210 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). 5305-00-150-9210 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5305-00-150-9210 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. 5305-00-150-9210 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. 5305-00-150-9210 is not classified as a special type of cargo when transported by water. 5305-00-150-9210 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.