5306-14-330-6711
Close Tolerance Bolt
5306143306711 143306711 4A1034 RA48949-1 86-266-9061
An externally threaded fastener whose unthreaded portion is of a specified grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. Items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten-thousandths (0.0015) of an inch (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (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 not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. For items having close tolerance, and fabricated from material having 160,000 pounds per square inch (1100 megapascals) minimum tensile strength, see BOLT, SHEAR. For items fabricated from material having less than 160,000 pounds per square inch (1100 megapascals) minimum tensile strength and not having a close tolerance, see BOLT, MACHINE. View more Close Tolerance Bolt
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January 2023
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NumberManufacturerStatus4A1035 F0300 - Dassault Aviation (Active) Primary Buy RNCC 3 RNVC 2 DAC 2 RA48949-1
NumberManufacturerStatus4A1036 F0300 - Dassault Aviation (Active) Primary Buy RNCC 3 RNVC 2 DAC 2 RA48949-1
Restrictions 5306-14-330-6711
End Users 5306-14-330-6711
- Argentina (YF)
- France (ZF)
Approved Sources 5306-14-330-6711
- Part Number
- Manufacturer
- Status
- 4A1034
- Manufacturer
- F0300 - Dassault Aviation (Active)
- Primary Buy
- Primary Buy
- RA48949-1
- K0654 - Safran Landing Systems Uk Ltd (Active)
- Secondary Buy
- Secondary Buy
- 86-266-9061
- F5385 - Section De Codification 85 (Cancelled)
- NATO Reference
- NATO Reference
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