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AN8-17

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Country of Origin USA
Distance From Head Largest Bearing Surface To Shank Hole Center 1.781 inches minimum first hole and 1.812 inches maximum first hole
Drilling Drilled Head
Fastener Length 1.953 inches minimum and 2.000 inches maximum
Features Provided Finished head
Grip 1 3/16 in
Grip Length 1 3/16, 1.172 inches minimum and 1.203 inches maximum
Hardness Rating 26.0 rockwell c minimum and 32.0 rockwell c maximum
Head Height 0.265 inches minimum and 0.297 inches maximum
Head Style Hexagon Head
Head Type Hexagon
Industry Standards/Certification AN8
Length 1 31/32 in, 1 63/64
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 00-150-9997
NSN 5306-00-150-9997
Nominal Length 1 31/32
Shank Unthreaded Hole Diameter 0.106 inches minimum first hole and 0.116 inches maximum first hole
Surface Treatment Cadmium
Surface Treatment Specification Qq-p-416,type 2,class 3 fed spec single treatment response
Thread Class 3a
Thread Diameter 0.500
Thread Direction Right-hand
Thread Length 0.750 inches minimum and 0.828 inches maximum
Thread Qty 20
Thread Qty Per Inch (tpi) 20
Thread Series Designator UNF
Thread Size 1/2-20
Weight 0.144 lb
Width Between Flats 0.740 inches minimum and 0.752 inches maximum

Cross-reference

No interchangeable or dimensionally similar parts are on record for AN8-17. Try the cross-reference lookup to search by a different part number.

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