P/N: nas68613
Category: Structural Components
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 | 20 Available |
The NAS68613 is a steel lock plate designed to prevent fastener rotation in aircraft structural applications. This positive locking device bends around bolt or nut heads to secure them against vibration-induced loosening. Installation involves torquing the fastener to specification, then bending the plate tabs to lock position per AC 43.13-1B guidance.
Commonly used on structural brackets, control surface hinges, and engine mount points where vibration poses a loosening risk. The lock plate provides a simple, reliable safetying method recognized across general and commercial aviation 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 NAS68613 is a steel lock plate designed to prevent fastener rotation in aircraft structural applications. This positive locking device bends around bolt or nut heads to secure them against vibration-induced loosening.
The LOCK PLATE may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: New Surplus. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the LOCK PLATE. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the nas68613.