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AN7-25A

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Country of Origin USA
Drilling Undrilled Head
Fastener Length 2.703 inches minimum and 2.750 inches maximum
Features Provided Finished head
Grip 2 1/16 in
Grip Length 2 1/16, 2.047 inches minimum and 2.078 inches maximum
Hardness Rating 26.0 rockwell c minimum and 32.0 rockwell c maximum
Head Height 0.234 inches minimum and 0.266 inches maximum
Head Style Hexagon Head
Head Type Hexagon
Industry Standards/Certification AN7
Length 2 23/32 in, 2 3/4
Material Steel
Material Specification Mil-s-5626 mil spec 1st material response or mil-s-6049 mil spec 2nd material response or mil-s-6050 mil spec 3rd material response or mil-s-6098 mil spec 4th material response or mil-s-6758 mil spec 5th material response or ams 6300 assn std 6th material response
Min. Tensile Strength (psi) 125000 pounds per square inch
NIIN 00-208-1359
NSN 5306-00-208-1359
Nominal Length 2 23/32
Surface Treatment Cadmium
Thread Class 3a
Thread Diameter 0.438
Thread Direction Right-hand
Thread Length 0.625 inches minimum and 0.703 inches maximum
Thread Qty 20
Thread Qty Per Inch (tpi) 20
Thread Series Designator UNF
Thread Size 7/16-20
Weight 0.133 lb
Width Between Flats 0.615 inches minimum and 0.627 inches maximum

Cross-reference

No interchangeable or dimensionally similar parts are on record for AN7-25A. Try the cross-reference lookup to search by a different part number.

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