P/N: f22na17a02
Category: Fasteners & Hardware
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 | 97 Available |
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.
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 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.
Aircraft hardware is manufactured to military and aviation specifications. The NUT conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the f22na17a02.
Yes, we sell hardware in various quantities from single units to bulk lots. The NUT is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.