ROD END-TAB ACT STAB (P/N 45-524563) - New Surplus

The 45-524563 is a rod end for horizontal stabilizer tab actuation linkages. This component connects the tab actuator to the lever arm, transmitting control input to position the stabilizer tab during flight. Typically manufactured from steel or aluminum with a threaded end and clevis pin interface.

Installation requires proper hardware, torque specifications, and safetying per aircraft maintenance manual. Verify compatibility with your aircraft's illustrated parts catalog before installation.

What is the ROD END-TAB ACT STAB (P/N 45-524563)?

The 45-524563 is a rod end for horizontal stabilizer tab actuation linkages. This component connects the tab actuator to the lever arm, transmitting control input to position the stabilizer tab during flight.

Is the 45-524563 a PMA or OEM part?

The ROD END-TAB ACT STAB 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 Surplus. Contact us for sourcing details.

Does the 45-524563 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 END-TAB ACT STAB. We stock related hardware and can help identify companion parts.

Can the 45-524563 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 45-524563.