EASA Regulations for Cirrus Design Corporation SR20

2 airworthiness directives and regulations affecting Cirrus Design Corporation SR20.

EASA AD US-2024-24-11

Engine Controls - Upper Power Lever - Inspections

The document titled 'Engine Controls - Upper Power Lever - Inspections' is a regulatory directive focusing on the inspection requirements for the upper power lever components in aircraft engine controls. It addresses maintenance and inspection protocols to ensure the reliability and safety of engine power lever operations. The document is intended for aviation maintenance professionals and operators responsible for engine control systems.

Dec 9, 2024

Airworthiness DirectiveMaintenanceSafety MgmtCirrus Design Corporation SR20Cirrus Design Corporation 22

EASA SIB CE-08-12R1

Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes - Possible Failure of a Transient Voltage Suppressor (TVS)

The Special Airworthiness Information Bulletin SAIB: CE-08-12R1 addresses a potential failure of a transient voltage suppressor (TVS) in Cirrus Design Corporation Models SR20 and SR22 airplanes. This failure may cause loss of NAV/COMM 1 functionality and produce short-term smoke and fumes in the cockpit, increasing pilot workload. The bulletin provides updated service information from Cirrus Design Corporation to mitigate this issue.

May 11, 2011

Safety Information BulletinMaintenanceSafety MgmtCirrus Design Corporation SR20Cirrus Design Corporation SR22