LEVER (P/N 212-46441-7) - New

The 212-46441-7 is a machined metal lever designed for mechanical linkage actuation in aircraft control and latch assemblies. This component transmits motion and force between connected systems, converting operator input or automated signals into controlled mechanical movement. Commonly found in access panel mechanisms, door latches, and flight control linkages on general aviation aircraft.

The lever interfaces with AN/MS/NAS hardware and connects to drive shafts or control cables. Installation requires verification against your aircraft's Illustrated Parts Catalog and compliance with applicable maintenance manual procedures.

What is the LEVER (P/N 212-46441-7)?

The 212-46441-7 is a machined metal lever designed for mechanical linkage actuation in aircraft control and latch assemblies. This component transmits motion and force between connected systems, converting operator input or automated signals into controlled mechanical movement.

Is the 212-46441-7 a PMA or OEM part?

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: New. Contact us for sourcing details.

Does the 212-46441-7 include installation hardware?

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.

Can the 212-46441-7 be shipped internationally?

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 212-46441-7.