Cockpit Reference Guide for the Cirrus SR2x with Perspective Touch+ by Garmin
190-02954-01 Rev. A
192
Flight
InstrumentsEAS
Audio and
CNS
Flight
Management
Hazard
AvoidanceAFCS
Additional
Features
Abnormal
OperationAnnun/AlertsAppendixIndex
Abnormal Operation
Weather Request
Status Message
Description
No Connext Subscription The system is not currently subscribed to the Garmin Connext Weather
service, or the access code is incorrect. Verify the access code. Contact
Garmin Aviation Product Support using the information at flygarmin.com.
Reduce Request Area The weather data request area exceeds size limits. Reduce weather coverage
area and re-send data request.
Request Canceled The user has canceled a weather data request.
Request Failed - Try Again
The weather data request timed-out. Re-send data request.
Transfer Preempted
The data link is busy. Retry request later.
Abnormal Weather Data Request Status Messages
AFCS ABNORMAL OPERATIONS
ELECTRONIC STABILITY & PROTECTION
Underspeed Protection is available when the optional Electronic Stability and Protection
(ESP) system is installed and the autopilot is on. It is designed to discourage aircraft operation
below minimum established airspeeds.
When the aircraft reaches a predetermined airspeed (see pertinent flight manual for air-
speeds which are dependent upon flap setting, and anti-ice system on-board), a flashing amber
‘MINSPD’ annunciation will appear above the airspeed indicator.
When the airspeed trend vector reaches the predetermined airspeed, a single aural “AIR-
SPEED” will sound, alerting the pilot to the impending underspeed condition.
OVERSPEED PROTECTION
While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude
capture mode is active, airspeed is monitored by the flight director. Pitch commands are not
changed until overspeed protection becomes active. Overspeed protection is provided in situa-
tions where the flight director cannot acquire and maintain the mode reference for the selected
vertical mode without exceeding Vne.
When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box
above the Airspeed Indicator, flashing a yellow ‘MAXSPD’ annunciation. Engine power should
be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disap-
pears when the overspeed condition is resolved.
SUSPECTED AUTOPILOT MALFUNCTION
NOTE:
Consult the aircraft documentation for the location of circuit breakers as well
as specifics that may supplement or amplify this procedure.
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