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AN8-32A
Aeronautical Standard Machine Bolt
Description
Airframe Bolt
Specifications
| Country of Origin | USA |
|---|---|
| Drilling | Undrilled Head |
| Fastener Length | 3.328 inches minimum and 3.360 inches maximum |
| Features Provided | Finished head |
| Grip | 2 9/16 in |
| Grip Length | 2 9/16, 2.546 inches minimum and 2.578 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 | 3 11/32 in, 3 23/64 |
| Material | Steel |
| Min. Tensile Strength (psi) | 125000 pounds per square inch |
| NIIN | 00-207-4574 |
| NSN | 5306-00-207-4574 |
| Nominal Length | 3 11/32 |
| Surface Treatment | Cadmium |
| Thread Class | 3a |
| Thread Diameter | 0.500 |
| Thread Direction | Right-hand |
| Thread Length | 0.781 inches minimum |
| Thread Qty | 20 |
| Thread Qty Per Inch (tpi) | 20 |
| Thread Series Designator | UNF |
| Thread Size | 1/2-20 |
| Weight | 0.218 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 AN8-32A. Try the cross-reference lookup to search by a different part number.
Catalog data updated 2026-07-05. Report a data error