P/N: 212-42000-05-1
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 | 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.
Aircraft hardware is manufactured to military and aviation specifications. The NUT STOP PLATE 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 212-42000-05-1.
Yes, we sell hardware in various quantities from single units to bulk lots. The NUT STOP PLATE is available in: New, New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.