
Cirrus Perspective
™
by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
190-00821-06 Rev. A
84
Annunciations & Alerts
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AlertsAppendixIndex
Condition Annunciation Description
Aileron Mistrim
Right
A condition has developed causing the roll servo to provide
a sustained right force.
Rudder Mistrim
Left
A condition has developed causing the yaw servo to
provide a sustained force (SR22 only).
Rudder Mistrim
Right
A condition has developed causing the yaw servo to provide a
sustained force (SR22 only).
Preflight Test Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
Preflight system test has failed.
GFC 700 SPEED CONDITION/STALL ALERT
Condition Annunciation Description
Overspeed Flashing annunciation indicating aircraft overspeed
condition. The flight director commands pitch up and, if
engaged, the autopilot will follow the pitch up command.
Engine power should be reduced and/or the pitch reference
adjusted to slow the aircraft. The annunciation disappears
when the condition is resolved.
Underspeed/Stall Flashing annunciation indicating aircraft underspeed or
imminent stall condition. An underspeed condition initiates
flight director commands for pitch down and, if engaged,
the autopilot will follow the pitch down command. Engine
power should be increased and/or the pitch reference
adjusted to increase airspeed. A stall condition causes
the flight director to capture the Stall Warning Reference
Airspeed (i.e., the speed at which Stall Warning Mode was
entered) and commands a pitch attitude to follow the
reference speed. The Stall Warning Reference Airspeed
is increased at a rate of one kt/sec. The annunciation
disappears when the condition is resolved.
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