NSN 5306-01-519-2347
Coaxial Connector
Bolt is shot peened prior to chroium plating per sae-ams-s-13165; bolt is passivated after chromium plating.
Manufacturer part number NAS6704G16 for national stock number 5306015192347.
Datasheet
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Product description
Shear Bolt NSN 5306-01-519-2347.
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MPN or Model
NAS6704G16
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Schedule B
7318.15.2000 (Bolts and bolts and their nuts or washers exported in the same shipment) -
Thread Class
3a -
Thread Direction
Right-hand -
Thread Length
0.425 inches -
Fastener Length
Between 1.410 inches and 1.440 inches -
Head Style
Dished hexagon -
Head Height
Between 0.125 inches and 0.140 inches -
Width Between Flats
Between 0.429 inches and 0.439 inches -
Grip Diameter
Between 0.2485 inches and 0.2495 inches -
Single Shear Strength
95000 pounds per square inch -
End Application
Boeing b757 aircraft -
Thread Diameter
0.250 inches -
Grip Length
Between 0.990 inches and 1.010 inches -
Thready Qty Per Inch (tpi)
28 -
Min. Tensile Strength (psi)
160000 pounds per square inch -
Material
Iron alloy 660 -
Material Specification
Sae-ams5731 assn standard single material response or sae-ams5732 assn standard single material response or sae-ams5737 assn standard single material response or sae-ams5853 assn standard single material response -
Surface Treatment
Passivate -
Surface Treatment Specification
Sae-ams-qq-p-35 assn standard single treatment response -
Thread Series Designator
Unjf
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A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. The head is designed to accommodate an external wrench or driver. 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. The unthreaded portion is of specific 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. A locking feature may be incorporated in the design of the head or threads. See bolt, machine and bolt, clevis.
Pricing and Availability
Get a quote for 5306-01-519-2347 shear boltManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |
BACB30LM4C16 | The Boeing Company |
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |
NAS6704G16 | National Aerospace Standards |
BACB30LM4C16 | The Boeing Company |