ROD PUSH-PULL CONTROL (P/N 212-46131.1) - As Removed

The 212-46131.1 is a push-pull control rod that transmits linear motion through aircraft control linkages. This component carries tension and compression forces between bellcranks and levers, typically constructed from aerospace aluminum or steel tubing with threaded rod-end attachments for secure connection points. Commonly found in throttle linkage assemblies, it enables pilot control inputs to reach engine or system actuators.

Installation and rigging must follow the applicable aircraft maintenance manual and FAA AC 43.13-1B acceptable methods. Verify applicability through your aircraft's Illustrated Parts Catalog before installation.

What is the ROD PUSH-PULL CONTROL (P/N 212-46131.1)?

The 212-46131. 1 is a push-pull control rod that transmits linear motion through aircraft control linkages.

Is the 212-46131.1 a PMA or OEM part?

The ROD PUSH-PULL CONTROL 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: As Removed. Contact us for sourcing details.

Does the 212-46131.1 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 ROD PUSH-PULL CONTROL. We stock related hardware and can help identify companion parts.

Can the 212-46131.1 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 212-46131.1.