EASA Regulations for Cirrus SR20

4 airworthiness directives and regulatory documents affecting Cirrus SR20.

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.

Sep 6, 2011

Safety Information BulletinMaintenanceSafety MgmtCirrus SR20Cirrus SR22Cirrus SR22T

EASA SIB CE-11-09

Avidyne Corporation - Flight Management Computing Software System [Piper PA-46R-350T / Cirrus SR20, SR22]

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-09 informs operators and maintenance personnel about a software issue in the Avidyne Corporation Flight Management Computing Software System installed on Piper PA-46R-350T and Cirrus SR20/SR22 aircraft. The bulletin highlights a faulty transition logic causing incorrect altitude limits to be displayed on the Flight Management System. This issue affects aircraft equipped with the Avidyne Entegra Integrated Flight Display system, part number 700-00083-( ), across any software release.

Jan 17, 2011

Safety Information BulletinFlight OpsMaintenanceSafety MgmtPiper PA-46R-350TCirrus SR20Cirrus SR22

EASA SIB CE-09-46

Cirrus SR20 and SR22 Aeroplanes - Nose Landing Gear Cracking

The Special Airworthiness Information Bulletin SAIB: CE-09-46 is an FAA informational bulletin addressing nose landing gear cracking concerns on Cirrus Design Corporation Models SR20 and SR22 airplanes. It highlights observed cracking and nose gear collapses in SR20 training aircraft and cracking in SR22 models, although no collapses have occurred on the latter. The bulletin is intended to alert owners and installers but does not mandate regulatory action.

Aug 10, 2009

Safety Information BulletinMaintenanceSafety MgmtCirrus SR20Cirrus SR22

EASA SIB CE-09-32

Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount

The Special Airworthiness Information Bulletin Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount is an FAA informational bulletin addressing airworthiness concerns for Cirrus Models SR20 and SR22 airplanes equipped with GPS/WAAS antennas mounted under the glareshield. It highlights potential issues with antenna mounting robustness and signal loss due to airframe shadowing that may affect GPS/WAAS navigation service. The bulletin applies specifically to Cirrus aircraft using the original under-glareshield mounting location for GPS/WAAS antennas.

Jun 30, 2009

Safety Information BulletinSafety MgmtCirrus SR20Cirrus SR22