P/N: 212-42000-05-1
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 | 2 Available |
| New Surplus | 2 Available |
The 212-42000-05-1 is a nut stop plate designed to prevent nut rotation under vibration and flight loads. This lock plate functions as a positive-locking device, securing a nut to structural brackets and fastened assemblies. Installation follows FAA AC 43.13-1B safetying practices and applicable aircraft maintenance manuals, with proper torque specification observed.
Commonly used in primary and secondary structural retention applications where vibration resistance is critical. The plate engages the nut flats to create mechanical lock-up, eliminating the need for additional locking methods in certified aircraft maintenance.
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 212-42000-05-1 is a nut stop plate designed to prevent nut rotation under vibration and flight loads. This lock plate functions as a positive-locking device, securing a nut to structural brackets and fastened assemblies.
The 212-42000-05-1 is currently available in the following conditions: New, New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-42000-05-1 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.