P/N: an8-16a
Category: Bolts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The AN8-16A is a hex head airframe bolt with a 1/2-20 UNF thread and undrilled shank, designed for use with self-locking nuts. Constructed from alloy steel with a minimum tensile strength of 125,000 psi, this AN-series fastener meets military aerospace standards for structural integrity. Used in airframe structural joints and primary load-bearing connections on general and commercial aircraft.
Installation requires proper grip length selection and torque application per FAA AC 43.13-1B guidance. The undrilled shank prevents accidental cotter pin installation, ensuring the fastener works exclusively with self-locking nut designs.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The AN8-16A is a hex head airframe bolt with a 1/2-20 UNF thread and undrilled shank, designed for use with self-locking nuts. Constructed from alloy steel with a minimum tensile strength of 125,000 psi, this AN-series fastener meets military aerospace standards for structural integrity.
The an8-16a is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The an8-16a requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.