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NSN 5306-00-680-5898

Coaxial Connector

About this product

Between 3.327 inches and 3.374 inches fastener length, hexagon head style, between 0.265 inches and 0.297 inches head height, width between flats: between 0.740 inches and 0.752 inches .

Manufacturer part number 2356378-32 for national stock number 5306006805898.

Datasheet

  • Product description

    Shear Bolt NSN 5306-00-680-5898.

  • MPN or Model

    2356378-32

  • Schedule B
    7318.15.2000 (Bolts and bolts and their nuts or washers exported in the same shipment)
  • NMF (National Motor Freight)
    093486 - Bolts, Nuts Or Screws, NOI (sub 3)
  • Thread Class
    3a
  • Thread Direction
    Right-hand
  • Thread Length
    Between 0.781 inches and 0.796 inches
  • Fastener Length
    Between 3.327 inches and 3.374 inches
  • Head Style
    Hexagon
  • Head Height
    Between 0.265 inches and 0.297 inches
  • Width Between Flats
    Between 0.740 inches and 0.752 inches
  • Grip Diameter
    Between 0.4986 inches and 0.4991 inches
  • Single Shear Strength
    18650 pounds per square inch
  • Thread Diameter
    0.500 inches
  • Grip Length
    Between 2.546 inches and 2.578 inches
  • Thready Qty Per Inch (tpi)
    20
  • Min. Tensile Strength (psi)
    160000 pounds per square inch
  • Material
    Steel comp 8740
  • Material Specification
    Mil-s-6049, cond f military specification 1st material response
  • Surface Treatment
    Cadmium
  • Surface Treatment Specification
    Qq-p-416, type 1, cl 3 federal specification single treatment response
  • Thread Series Designator
    Unf
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Shear Bolt

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.

Mechanic Bill explains Coaxial Connector

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Manufacturer Part Numbers and Alternates
MPN manufacturer part number Registrant or Supplier
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
2356378-32 Boeing Company, The
S2356378-32 Boeing Company, The
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