P/N: an5-26a
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 | 74 Available |
The AN5-26A is a 5/16-24 UNF alloy steel airframe bolt designed for structural fastening in aircraft control systems. The undrilled shank (A designation) accommodates self-locking nuts, eliminating the need for secondary locking devices. This bolt handles combined shear and tension loads common in control-system linkages and structural connections.
Installation requires torque per FAA AC 43.13-1B guidance, with grip length matching the material stack-up specified in the aircraft Illustrated Parts Catalog. AN-series construction ensures aerospace-grade reliability and dimensional consistency.
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 AN5-26A is a 5/16-24 UNF alloy steel airframe bolt designed for structural fastening in aircraft control systems. The undrilled shank (A designation) accommodates self-locking nuts, eliminating the need for secondary locking devices.
The an5-26a is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The an5-26a 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.