ROD (P/N 5141-028-901) - As Removed

The 5141-028-901 is a rigid control rod for aircraft flight-control linkage systems. This component transfers push-pull motion between control mechanisms, such as from a bellcrank to a control-surface horn. Typically constructed from aluminum or steel tubing, the rod connects via AN/MS rod ends or clevis fittings at each end.

Installation requires proper rigging and torque per the applicable aircraft maintenance manual. Used across general aviation and commercial aircraft control systems where precise, rigid motion transfer is essential for flight control authority.

What is the ROD (P/N 5141-028-901)?

The 5141-028-901 is a rigid control rod for aircraft flight-control linkage systems. This component transfers push-pull motion between control mechanisms, such as from a bellcrank to a control-surface horn.

Is the 5141-028-901 a PMA or OEM part?

The ROD 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 5141-028-901 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. We stock related hardware and can help identify companion parts.

Can the 5141-028-901 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 5141-028-901.