P/N: 212-4200-05-1
Category: Nuts
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 212-4200-05-1 is a self-locking aircraft nut designed to resist vibration loosening in threaded assemblies. Conforming to AN363 (all-metal) or AN365 (elastic-insert) specifications, this nut incorporates a locking mechanism that maintains prevailing torque under flight and operational vibration. Commonly used on airframe brackets and structural fastening applications where bolt security is critical.
Installation requires torquing per aircraft maintenance manual specifications and FAA AC 43.13-1B guidance. Replace if prevailing torque falls below acceptable limits during inspection.
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 212-4200-05-1 is a self-locking aircraft nut designed to resist vibration loosening in threaded assemblies. Conforming to AN363 (all-metal) or AN365 (elastic-insert) specifications, this nut incorporates a locking mechanism that maintains prevailing torque under flight and operational vibration.
The 212-4200-05-1 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-4200-05-1 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.