P/N: 212-56218-02-1
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
The 212-56218-02-1 is a pivoted mechanical lever that converts input force into controlled, repeatable motion within aircraft linkage systems. This component transmits force through a fulcrum point to actuate latch mechanisms and control surfaces. Constructed from corrosion-resistant aluminum or steel, the lever integrates with mechanical control cables, rods, and fastening points per aircraft specifications.
Installation requires verification against your aircraft's Illustrated Parts Catalog and adherence to rigging procedures outlined in the Aircraft Maintenance Manual.
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 212-56218-02-1 is a pivoted mechanical lever that converts input force into controlled, repeatable motion within aircraft linkage systems. This component transmits force through a fulcrum point to actuate latch mechanisms and control surfaces.
The LEVER 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: Serviceable. 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 LEVER. 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 212-56218-02-1.