Airframe Bolt, Drilled AN5-10

Description:

Length: 1-3/32", grip: 9/16", thread: 5/16-24, cadmium plated steel, drilled shank

AN5-10 Details

National Stock Number (NSN)	5306-01-446-9762
Alternate Part Number	N/A
Federal Supply Class (FSC)	5306
Unit of Measure (UOM)	10 /Ea.
Thread Class	3a
Thread Direction	Right-hand
Thread Length	Between 1.625 inches and 1.693 inches
Fastener Length	Between 1.078 inches and 1.125 inches
Head Style	Hexagon
Head Height	Between 0.172 inches and 0.204 inches
Width Between Flats	Between 0.490 inches and 0.502 inches
Grip Diameter	Between 0.309 inches and 0.312 inches
Thread Diameter	0.312 inches
Grip Length	Between 0.547 inches and 0.578 inches
Thready Qty Per Inch (tpi)	24
Part Name Assigned By Controlling Agency	Bolt, machine, aircraft
Special Features	Ultimate tensile strength at root dia. For steel 6500 pounds and for aluminum alloy 3220 pounds; yield tensile strength at root dia. For steel 4980 pounds and for aluminum alloy 2080 pounds; single shear strength at full dia. For steel 5750 pounds and for aluminum alloy 2685 pounds
Material	Steel or stainless steel or aluminum alloy
Test Data Document	88044-an5 specification (includes engineering type bulletins, brochures, etc., that reflect specification type data in specification format; excludes commercial catalogs, industry directories, and similar trade publications, reflecting general type data on certain environmental and performance requirements and test conditions that are shown as "typical", "average", "", etc.).
Thread Series Designator	Unf
Specification Data	88044-an5 professional/industrial association specification

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