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AN4-6A

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Country of Origin USA
Drilling Undrilled Head
End Application Phoenix (aim-54) air-to-air hc-130); missile ec-130e mc-130h sof (ac-130h harpoon (agm-84); aircraft all-weather anti-ship ec-135h/k/p); missile aircraft tf33-pw-102 (c-135e t56-a-7/15 (c-130b/e/h/n/p); close in weapon system (ciws-phalanx); engine aircraft b-52h); engine aircraft tf33-p-3/5/9 (c/ec-135 mini-sace; engine b-1 aircraft; test consoles w/s:support equipment
Fastener Length 0.781
Features Provided Finished head
Grip 5/16 in
Grip Length 0.383, 5/16
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 25/32 in, 3/4
Material Steel
Min. Tensile Strength (psi) 125000 pounds per square inch
NIIN 00-151-1426
NSN 5306-00-151-1426
Nominal Length 25/32
Pre-Packaged Bag Quantity 100
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 0.397
Thread Qty 28
Thread Qty Per Inch (tpi) 28
Thread Series UNF
Thread Series Designator Unf (fine thread)
Thread Size 1/4-28
Weight 0.02 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