P/N: 68518
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 | 21 Available |
The 68518 is a Lycoming lockplate that mechanically secures fasteners by bending tabs against bolt or nut flats. This steel component prevents rotation in engine and accessory assemblies where safety wire installation is impractical or restricted. Commonly used in powerplant brackets, engine mount points, and structural connections requiring positive locking.
Install per the applicable engine or airframe maintenance manual, ensuring tabs engage flats correctly and bend direction follows OEM specifications. Verify part application against the Illustrated Parts Catalog before installation.
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 68518 is a Lycoming lockplate that mechanically secures fasteners by bending tabs against bolt or nut flats. This steel component prevents rotation in engine and accessory assemblies where safety wire installation is impractical or restricted.
The LOCKPLATE 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 LOCKPLATE. 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 68518.