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5305-01-174-6541
Close Tolerance Screw
5305011746541 011746541 NAS5203PU1
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
January 2023
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Restrictions 5305-01-174-6541
5305-01-174-6541 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. The precious metals content of this item is unknown.
Import and Export 5305-01-174-6541
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-01-174-6541
- United Kingdom (ZK01)
- Effective Date:
- 1 Mar 1997
Approved Sources 5305-01-174-6541
- Part Number
- Manufacturer
- Status
- NAS5203PU1
- Manufacturer
- 80205 - National Aerospace Standards (Active)
- Primary Buy
- Primary Buy
Datasheet 5305-01-174-6541
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Fastener Length [AASB]
- 0.370 Inches Minimum And 0.400 Inches Maximum
- Grip Diameter [AAUR]
- 0.1890 Inches Minimum And 0.1895 Inches Maximum
- Grip Length [ANEE]
- 0.052 Inches Minimum And 0.072 Inches Maximum
- Head Height [AASU]
- 0.103 Inches Minimum And 0.118 Inches Maximum
- Head Diameter [AASL]
- 0.357 Inches Minimum And 0.373 Inches Maximum
- Head Style [AASK]
- Pan No. 2
- Material [MATT]
- Titanium Alloy Overall
- Minimum Tensile Strength [CQBC]
- 160000 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 0.190 Inches
- Internal Drive Style [ABQZ]
- Tri-Wing Recess
- Material Document And Classification [MDCL]
- Ams4928 Assn Std Single Material Response Overall Or Ams4967 Assn Std Single Material Response Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.323 Inches Nominal
- Thread Series Designator [THSD]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 32
NATO Stock Numbers Related to 5305-01-174-6541
Freight Information 5305-01-174-6541
5305-01-174-6541 has freight characteristics managed by the United Kingdom (UK).. 5305-01-174-6541 has a variance between NMFC and UFC when transported by rail and the description should be consulted.