P/N: 212-56218-02-1
Category: Linkages, Rods & Bellcranks
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 212-56218-02-1 is currently available in the following conditions: Serviceable. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-56218-02-1 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.