Cirrus Design Section 7
SR22T Systems Description
P/N 13772-005 7-33P/N 13772-005 7-33
Engine Indicating
Engine information is displayed as analog-style gages, bar graphs,
and text on the MFD’s ENGINE page. When the ENGINE page is not
active or in the case of an electronic display failure (backup mode), all
essential engine information is displayed along the LH edge of the
display. Engine data is acquired by the Engine Airframe Unit which
transmits the data to the Engine Indicating System for display as
described in the following pages.
• Note •
A “Red X” through any electronic display field indicates that
the display field is not receiving valid data and should be
considered inoperative.
Engine System Annunciations
Engine system health, caution, and warning messages are displayed
in color-coded text in the Crew Alerting System (CAS) window located
to the right of the Altimeter and Vertical Speed Indicator. In
combination with a CAS alert, the affected engine parameter displayed
on the ENGINE page changes to the corresponding color of CAS alert
and the annunciation system issues an audio alert.
For specific pilot actions in response to Engine System
Annunciations, refer to Section 3 - Emergency Procedures,
Engine System Emergencies, and Section 3A - Abnormal
Procedures, Engine System.
For additional information on Engine Instrument Markings and
Annunciations, refer to Section 2: Limitations.
For additional information on the System Annunciations And
Alerts, refer to the Perspective Integrated Avionics System
description in this section.
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