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5305-01-530-9349
Close Tolerance Screw
5305015309349 015309349 NAS 1142-4 NAS1142-4
A SCREW, MACHINE or SCREW, CAP, SOCKET HEAD whose unthreaded portion is of specified grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001 IN.) (0.025 mm) or less of a specific diameter for items (1.000 IN.) (25 mm) or less in diameter. Items over (1.000 IN.) (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015 IN.) (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001 IN.) (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. The head is designed to be held or driven with an inserted driver. It is not designed for rotation by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. View more Close Tolerance Screw
May 2023
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Restrictions 5305-01-530-9349
5305-01-530-9349 is a Close Tolerance 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. This item does not contain a precious metal.
Import and Export 5305-01-530-9349
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-01-530-9349
- NASA (G180)
- Effective Date:
- 1 Jun 2005
- Spain (YB01)
- Effective Date:
- 1 Jul 2007
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 2008
Approved Sources 5305-01-530-9349
- Part Number
- Manufacturer
- Status
- NAS 1142-4
- Manufacturer
- 80205 - National Aerospace Standards (Active)
- Incomplete Reference
- Incomplete Reference
- NAS1142-4
- Y9993 - Royal Malaysian Airforce (Active)
- NATO Reference
- NATO Reference
Datasheet 5305-01-530-9349
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Thread Series Designator [THSD]
- Unjc
- Nominal Thread Diameter [AHYM]
- 0.164 Inches
- Thread Quantity Per Inch [CMLP]
- 32
- Thread Class [AAJD]
- 3A
- Thread Length [AASA]
- 0.276 Inches Nominal
- Fastener Length [AASB]
- 0.526 Inches Nominal
- Material [MATT]
- Steel Corrosion Resisting Overall
- Surface Treatment [SFTT]
- Cadmium Overall
- Surface Treatment Document And Classification [STDC]
- Qq-P-416, Ty2cl2 Fed Spec All Treatment Responses Overall
- Head Style [AASK]
- Modified Pan
- Internal Drive Style [ABQZ]
- Torque
- Grip Length [ANEE]
- 0.250 Inches Nominal
- Grip Diameter [AAUR]
- 0.250 Inches Nominal
- Special Features [FEAT]
- Ultimate Tensile Strenght 160,000Min. To 180,000Max. Pounds Per Sq. Inch; In Accordance W/ Nas1141 Thru Nas1148; Short Thread
NATO Stock Numbers Related to 5305-01-530-9349
Freight Information 5305-01-530-9349
5305-01-530-9349 has freight characteristics.. 5305-01-530-9349 has a variance between NMFC and UFC when transported by rail and the description should be consulted.