EASA Regulations for Cirrus SR22T

EASA SIB CE-11-50

Cirrus Design Corporation SR20, SR22 and SR22T Aeroplanes — Partial Asymmetric Flap and Flap Actuator Over-Extension

The Cirrus Design Corporation SR20, SR22 and SR22T Aeroplanes — Partial Asymmetric Flap and Flap Actuator Over-Extension is a Special Airworthiness Information Bulletin issued by the FAA to alert owners and installers about a flap actuator over-extension issue affecting Cirrus SR20, SR22, and SR22T aircraft. This bulletin highlights a potential flap actuator rod end bending and partial asymmetric flap condition that could occur due to a 0-percent proximity sensor failure. The bulletin provides information and recommendations but does not mandate regulatory action.