WARNING ALERTS
Annunciation
Window Text
ANTI ICE
CTL
ANTI ICE
FLOW
ANTI ICE
QTY
ANTI ICE
QTY
AOA
OVERHEAT
AUTO DESCENT
AUTO DESCENT
AUTO DESCENT
AUTO DESCENT
BRAKE TEMP
CHT
CO LVL HIGH
DUCT OVERHEAT
ESS BUS
FUEL
FLOW*
FUEL IMBALANCE
FUEL QTY
M BUS 1
M BUS 2
MAN
PRESSURE*
OIL PRESSURE
OIL TEMP
190-00821-09 Rev. A
Cirrus Perspective
Alerts Window Text
Tank valves cannot be controlled
(closed) (TKS).
Flow rate is low (TKS).
Left and right fluid quantities are
unknown (TKS)
Fluid quantity is low (TKS).
AOA probe is overheated.
2
Automatic descent to 14,000FT in
60 seconds
2
Aircraft descending to 14,000FT
2
Aircraft descending to 12,500FT
2
Aircraft descended due to pilot
incapacitation
Brake temperature is high.
Cylinder head temperature is high.
Carbon monoxide level is too high.
3
Cabin heat duct temperature is high
Check essential power bus voltage.
Check fuel flow.
Fuel quantity imbalance has been
detected
Check fuel tank levels.
Check main power bus 1 voltage.
Check main power bus 2 voltage.
Check manifold pressure.
Oil pressure is out of range.
Oil temperature is high.
™
by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
Annunciations & Alerts
Audio Alert
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
None
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
Repeating Double Chime
(after 30 seconds)
Repeating Double Chime
Repeating Double Chime
1
1
119