Posts Tagged ‘Cirrus SR20’

FAA Bulletin on Flight Controls and Flaps for Cirrus SR20 and SR22 Aircraft

Sunday, August 28th, 2011

Special Airworthiness Information Bulletin (SAIB) CE-11-50 is being issued to alert owners and installers to an airworthiness concern regarding a possible partial asymmetric flap and flap actuator over-extension condition on Cirrus Design Corporation (CDC) Models SR20, SR22, and SR22T airplanes.

pdf iconce-11-50.pdf

Flight Management AD affecting Cirrus and Piper Aircraft

Saturday, January 22nd, 2011

Navigation and Flight Management Computing Software System

Special Airworthiness Bulletin CE-11-09 affecting Cirrus SR20 and SR22 as
well as Piper Aircraft, PA-46R-350T

SR22

pdf iconce-11-09.pdf

SAIB Cirrus Design Corporation SR20 and SR22 GPS/WAAS Antenna

Friday, May 29th, 2009

This Special Airworthiness Information Bulletin applies to all Cirrus
aircraft with GPS/WAAS antennas installed using the original
under-glareshield mounting location when replacing the non-WAAS GPS antenna.
The airworthiness concern is not an unsafe condition that would warrant
airworthiness directive (AD)Action.

The FAA We recommends that owners and operators of Cirrus Models SR20 and
SR22 airplanes using the under-glareshield location for GPS/WAAS antennas
relocate the antennas to upper fuselage external locations following Cirrus
Optional Service Bulletins SB 2X-34-23 R1 (for aircraft without a primary
flight display) or SB 2X-34-24 R1 (for aircraft with a primary flight
display).

AD Airworthiness CE-09-32 for Cirrus SR20 and SR22

CE-09-32 – Cirrus Design Corporation – SR20
CE-09-32 – Cirrus Design Corporation – SR22

CE-09-32.pdf