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AN178-22A

Aeronautical Standard Close Tolerance Bolt

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Description

Close Tolerance Bolt

Specifications

Country of Origin USA
Fastener Length Between 2.328 inches and 2.375 inches
Grip Diameter Between 0.4986 inches and 0.4991 inches
Grip Length Between 1.546 inches and 1.578 inches
Hardness Rating 26.0 rockwell c and 32.0 rockwell c
Head Height Between 0.265 inches and 0.297 inches
Head Style Hexagon Head
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 ams 6300 assn standard 6th material response
Min. Tensile Strength (psi) 125000 pounds per square inch
Surface Finish 63.0 microinches grip, 63.0 microinches surface of head
Surface Treatment Cadmium and chromate
Surface Treatment Specification Cl 3 federal specification all treatment responses type 2 qq-p-416
Thread Class 3a
Thread Diameter 0.500
Thread Direction Right-hand
Thread Length Between 0.750 inches and 0.829 inches
Thread Qty 20
Thread Qty Per Inch (tpi) 20
Thread Series UNF
Thread Series Designator Unf (fine thread)
Thread Size 1/2
Weight 0.16 lb
Width Between Flats Between 0.740 inches and 0.752 inches

Other sizes

Parts that share this base number, ordered by size. Always verify the full specification before substituting.

Cross-reference

No interchangeable or dimensionally similar parts are on record for AN178-22A. Try the cross-reference lookup to search by a different part number.

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