ROD UPPER (P/N 36-430012-23) - As Removed

Part 36-430012-23 is an upper rod for aircraft control linkage assemblies. This metal member transmits axial loads while maintaining precise alignment between connected mechanical components. The rod features attachment ends designed for secure installation in airframe linkage systems.

Used in flight control, landing gear, and flap actuation linkages on general aviation aircraft. Installation must follow the aircraft's maintenance manual and comply with FAA regulations 14 CFR Part 43 and AC 43.13-1B. Verify compatibility with your specific aircraft's Illustrated Parts Catalog before installation.

What is the ROD UPPER (P/N 36-430012-23)?

Part 36-430012-23 is an upper rod for aircraft control linkage assemblies. This metal member transmits axial loads while maintaining precise alignment between connected mechanical components.

Is the 36-430012-23 a PMA or OEM part?

The ROD UPPER 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 36-430012-23 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 UPPER. We stock related hardware and can help identify companion parts.

Can the 36-430012-23 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 36-430012-23.