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AN4-25A

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Alternate Part Number 400-018
Country of Origin USA
Drilling Undrilled Head
Fastener Length Between 2.641 inches and 2.688 inches
Features Provided Finished head
Grip 2 3/16 in
Grip Length 2 3/16, Between 2.172 inches and 2.203 inches
Hardness Rating 26.0 rockwell c and 32.0 rockwell c
Head Height Between 0.140 inches and 0.172 inches
Head Style Hexagon Head
Head Type Hexagon
Industry Standards/Certification AN4
Length 2 21/32 in
Material Steel
Material Specification Mil-s-5626 military specification 1st material response or mil-s-6049 military specification 2nd material response or mil-s-6050 military specification 3rd material response or mil-s-6098 military specification 4th material response or mil-s-6758 military specification 5th material response or ams 6300 assn standard 6th material response
Min. Tensile Strength (psi) 125000 pounds per square inch
NIIN 00-151-1411
NSN 5306-00-151-1411
Nominal Length 2 21/32
Surface Treatment Cadmium and chromate
Surface Treatment Specification Class 3 federal specification all treatment responses type 2 qq-p-416
Thread Class 3a
Thread Diameter 0.250
Thread Direction Right-hand
Thread Length Between 0.438 inches and 0.516 inches
Thread Qty 28
Thread Qty Per Inch (tpi) 28
Thread Series UNF
Thread Series Designator Unf (fine thread)
Thread Size 1/4-28
Weight 0.042 lb
Width Between Flats Between 0.428 inches and 0.440 inches

Cross-reference

No interchangeable or dimensionally similar parts are on record for AN4-25A. Try the cross-reference lookup to search by a different part number.

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