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AN4-4A

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Country of Origin USA
Drilling Undrilled Head
End Application Tf-33-p-7 aircraft c-2a (reprocured);engine b-1 support equipment;sof aircraft;tf-33 engine;phoenix missile;harpoon missile;tf-56 engine;aircraft
Fastener Length Between 0.516 inches and 0.562 inches
Features Provided Finished head
Grip 1/16 in
Grip Length 1/8, Between 0.046 inches and 0.078 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 17/32 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 00-150-9105
NSN 5306-00-150-9105
Nominal Length 17/32
Pre-Packaged Bag Quantity 100
Surface Treatment Cadmium and chromate
Surface Treatment Specification Cl3 federal specification all treatment responses ty2 qq-p--16
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 0.015 lb
Width Between Flats Between 0.428 inches and 0.440 inches

Cross-reference

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