NUT (P/N f22na17a02) - New Surplus

The f22na17a02 is an all-metal self-locking plate nut designed for aircraft structural applications. This prevailing-torque fastener prevents vibration-induced loosening through an integral metal element that resists rotation. Installed behind access panels and structural covers, it provides a captive threaded anchor point for screw fastening.

Conforms to MS/NAS plate-nut specifications for airframe use. Verify thread size in your aircraft's Illustrated Parts Catalog before installation. Follow AC 43.13-1B guidance and applicable maintenance manual procedures for proper torque and assembly.

What is the NUT (P/N f22na17a02)?

The f22na17a02 is an all-metal self-locking plate nut designed for aircraft structural applications. This prevailing-torque fastener prevents vibration-induced loosening through an integral metal element that resists rotation.

What conditions is the f22na17a02 available in?

The f22na17a02 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.

How do I get pricing for the f22na17a02?

The f22na17a02 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.

Do you offer expedited shipping for the f22na17a02?

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.