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AN23-12

Aeronautical Standard Clevis Bolt

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Description

Clevis Bolt

Specifications

Alternate Part Number 400-674
Country of Origin USA
Departure From Cited Document Thread t per m1l-s-7742 except major d1a is not to exceed max allow bolt shank d1a
Drilling Drilled Head
Fastener Length Between 0.771 inches and 0.791 inches
Grip 7/16 in
Groove Diameter 0.141
Hardness Rating 26.0 rockwell c and 32.0 rockwell c
Head Diameter Between 0.365 inches and 0.385 inches
Head Height Between 0.083 inches and 0.103 inches
Head Style Button
Industry Standards/Certification AN23
Internal Drive Style Slot
Length 25/32 in
Material Steel
Material Specification Mil-s-6049 military specification 1st material response or mil-s-6050 military specification 2nd material response or mil-s-6098 military specification 3rd material response or mil-s-5626 military specification 4th material response or mil-s-6758 military specification 5th material response or mil-s-8695 military specification 6th material response
Min. Tensile Strength (psi) 125000 pounds per square inch
NIIN 00-151-1964
NSN 5306-00-151-1964
Shank Unthreaded Hole Diameter 0.070 inches first hole and 0.080 inches first hole
Single Shear Strength 2125 pounds per square inch
Surface Treatment Cadmium and chromate
Surface Treatment Specification Qq-p-416 type 2 cl 3 federal specification single treatment response
Thread Class 3a
Thread Diameter 0.190
Thread Direction Right-hand
Thread Length Between 0.323 inches and 0.363 inches
Thread Qty 32
Thread Qty Per Inch (tpi) 32
Thread Series UNF
Thread Series Designator Unf (fine thread)
Thread Size 10-32
Weight 0.007 lb

Cross-reference

Similar parts

Parts with matching key dimensions — often from a different standards family. Candidates for comparison only; verify the full specification before substituting.

  • AN23-12A AN #10-32 · 25/32 in · Button · Steel

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Catalog data updated 2026-07-05. Report a data error