EASA AD 2024-0181R1
Flight Controls — Rudder Trim Tab Installation / Threaded Bolts — Replacement
EASA Airworthiness Directive 2024-0181R1 is an updated regulatory requirement addressing the installation and replacement of rudder trim tab threaded bolts on Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 and above. The directive mandates replacing affected short rudder-trim control rod assemblies with serviceable parts to prevent potential failure of titanium bolts. This directive applies to the rudder trim tab installation and threaded bolts identified by specific part numbers.