NSN 5305-00-420-8248
High Torque Screw
Between 1.011 inches and 1.041 inches fastener length, between 0.122 inches and 0.133 inches head height, 160000 pounds per square inch min. tensile strength (psi), surface finish: 32.0 microinches threads.
Manufacturer part number NAS1133V12 for national stock number 5305004208248.
Datasheet
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Product description
Close Tolerance Screw NSN 5305-00-420-8248.
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MPN or Model
NAS1133V12
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Schedule B
8109.90.0000 (Zirconium and articles thereof nesoi) -
NMF (National Motor Freight)
136500 - Metal NOI/metal Alloys NOI -
Unit Weight (Est.)
0.1 lb -
Thread Class
3a -
Thread Length
Between 0.251 inches and 0.301 inches -
Fastener Length
Between 1.011 inches and 1.041 inches -
Head Height
Between 0.122 inches and 0.133 inches -
Min. Tensile Strength (psi)
160000 pounds per square inch -
Surface Finish
32.0 microinches threads -
Material
Titanium alloy uns r54520 -
Material Specification
Nas 621, 6al-4v assn standard single material response
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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.
Pricing and Availability
Get a quote for 5305-00-420-8248 close tolerance screwManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
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NAS1133V12 | National Aerospace Standards |