P/N: 3101688-2
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 | 1 Available |
The 3101688-2 is a lock plate designed to prevent fastener loosening in aircraft structural assemblies. This mechanical safetying device installs under bolt heads or nuts on structural brackets, using deformation or tabs to positively lock fasteners against vibration. Common in airframe construction where critical connections must remain secure during flight operations.
Installation follows Aircraft Maintenance Manual procedures and FAA AC 43.13-1B safetying practices. Verify fitment in the Illustrated Parts Catalog before use on certificated aircraft.
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 3101688-2 is a lock plate designed to prevent fastener loosening in aircraft structural assemblies. This mechanical safetying device installs under bolt heads or nuts on structural brackets, using deformation or tabs to positively lock fasteners against vibration.
The PLATE, LOCK 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 PLATE, LOCK. 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 3101688-2.