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AN7-11A

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Country of Origin USA
Drilling Undrilled Head
Fastener Length 1.203 inches minimum and 1.250 inches maximum
Features Provided Finished head
Grip 9/16 in
Grip Length 0.547 inches minimum and 0.578 inches maximum, 9/16
Hardness Rating 26.0 rockwell c minimum and 32.0 rockwell c maximum
Head Height 0.234 inches minimum and 0.266 inches maximum
Head Style Hexagon Head
Head Type Hexagon
Industry Standards/Certification AN7
Length 1 1/4, 1 7/32 in
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 00-208-3652
NSN 5306-00-208-3652
Nominal Length 1 7/32
Surface Treatment Cadmium and chromate
Surface Treatment Specification Qq-p-416,type 2,class 3 fed spec single treatment response
Thread Class 3a
Thread Diameter 0.438
Thread Direction Right-hand
Thread Length 0.625 inches minimum and 0.703 inches maximum
Thread Qty 20
Thread Qty Per Inch (tpi) 20
Thread Series Designator UNF
Thread Size 7/16-20
Weight 0.07 lb
Width Between Flats 0.615 inches minimum and 0.627 inches maximum

Cross-reference

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