P/N: a126e66
Category: General Aircraft Parts
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 | 24 Available |
The a126e66 is an all-metal prevailing-torque self-locking nut conforming to AN363/MS21045 aerospace standards. This stiffnut resists loosening under vibration through thread deformation, maintaining clamp load without polymer inserts. Steel construction enables operation at elevated temperatures unsuitable for nylon-insert nuts.
Used in airframe and engine attachments requiring reliable fastening in high-vibration environments. Install on undamaged threads and torque per aircraft maintenance manual specifications.
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 a126e66 is an all-metal prevailing-torque self-locking nut conforming to AN363/MS21045 aerospace standards. This stiffnut resists loosening under vibration through thread deformation, maintaining clamp load without polymer inserts.
The a126e66 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The a126e66 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.