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AN5-55A
Aeronautical Standard Machine Bolt
Description
Airframe Bolt
Specifications
| Country of Origin | USA |
|---|---|
| Drilling | Undrilled Head |
| Fastener Length | 5.703 inches minimum and 5.750 inches maximum |
| Features Provided | Finished head |
| Grip | 5 3/16 in |
| Grip Length | 5 3/16, 5.172 inches minimum and 5.203 inches maximum |
| Hardness Rating | 26.0 rockwell c minimum and 32.0 rockwell c maximum |
| Head Height | 0.172 inches minimum and 0.204 inches maximum |
| Head Style | Hexagon Head |
| Industry Standards/Certification | AN5 |
| Length | 5 23/32 in, 5 3/4 |
| Material | Steel |
| Min. Tensile Strength (psi) | 125000 pounds per square inch |
| NIIN | 00-151-0999 |
| NSN | 5306-00-151-0999 |
| Nominal Length | 5 23/32 |
| Surface Treatment | Cadmium and dichromate |
| Thread Class | 3a |
| Thread Diameter | 0.312 |
| Thread Direction | Right-hand |
| Thread Length | 0.531 inches minimum |
| Thread Qty | 24 |
| Thread Qty Per Inch (tpi) | 24 |
| Thread Series Designator | UNF |
| Thread Size | 1/4, 5/16-24 |
| Weight | 0.13 lb |
| Width Between Flats | 0.490 inches minimum and 0.502 inches maximum |
Cross-reference
No interchangeable or dimensionally similar parts are on record for AN5-55A. Try the cross-reference lookup to search by a different part number.
Catalog data updated 2026-07-05. Report a data error