24 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Cruise
During icing encounters in cruise, increase engine power to maintain
cruise speed as ice accumulates on the unprotected areas and causes
the aircraft to slow down.
The autopilot may be used in icing conditions. However, every 30
minutes the autopilot should be disconnected to detect any out-of-trim
conditions caused by ice buildup. If significant out-of-trim or other
anomalous conditions are detected, the autopilot should remain off for
the remainder of the icing encounter.
When disconnecting the autopilot with ice accretions on the airplane,
the pilot should be alert for out-of-trim forces.
Approach and Landing
If Icing Conditions Exist:
1. ICE PROTECT System Switch.................................................. ON
2. ICE PROTECT Mode Switch..................................................HIGH
3. Monitor ice accumulation.
If ice continues accumulating on protected surfaces:
a. ICE PROTECT Mode Push-Button................................... MAX
If ice accretions do not shed from protected surfaces:
b. PUMP BKUP Switch........................................................... ON
c. Perform Anti-Ice System Failure checklist.
4. WIND SHLD Push-Button .........................PRESS AS REQUIRED
• Caution •
To pr even t an obstr uc ted view due to residual deic ing fluid on
windshield, do not operate windshield de-ice system within 30
seconds of landing.
5. Ice-Inspection Lights .............................................. AS REQUIRED
6. Flaps ........................................................................................50%
7. Airspeed......................................................... Minimum of 95 KIAS
8. Airspeed on Short Final .....................................................88 KIAS
Original Issue: 02-01-13
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