EASA Regulations for Cirrus SF50

2 airworthiness directives and regulations affecting Cirrus SF50.

EASA AD US-2023-04-20

Auto Flight - Cirrus Airframe Parachute System - Configuration / Placard Installation; Aircraft Flight Manual / Airworthiness Limitations Section - Amendment

The Federal Aviation Administration's Airworthiness Directive 2023-04-20 addresses safety issues in Cirrus Design Corporation Model SF50 airplanes related to uncommanded activation of the Cirrus Airframe Parachute System (CAPS) autopilot mode. This directive mandates changes to avionics configuration, installation of information placards, and revisions to the Aircraft Flight Manual and Airworthiness Limitations Section. It also requires wiring modifications for certain airplanes to remove CAPS power timer functionality.

Mar 8, 2023

Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtCirrus Design Corporation SF50Cirrus SF50

EASA AD US-2019-08-51

[Final Rule] Flight Controls - Angle of Attack Sensors - Replacement

[Final Rule] Flight Controls - Angle of Attack Sensors - Replacement is a Federal Aviation Administration (FAA) airworthiness directive (AD) addressing all Cirrus Design Corporation Model SF50 airplanes. This AD mandates the replacement of angle of attack (AOA) sensors with improved versions due to incidents where the stall warning and protection system (SWPS) or Electronic Stability & Protection (ESP) System engaged inappropriately. The directive aims to mitigate unsafe flight conditions caused by faulty AOA sensors.

Jun 18, 2019

Airworthiness DirectiveMaintenanceSafety MgmtCirrus Design Corporation SF50Cirrus SF50