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5. Windshield Defrost.....................................................................ON
6. Ice-Inspection Lights .............................................. AS REQUIRED
7. Verify airframe is free of contamination immediately before takeoff.
8. Flaps ............................................. RETRACT as soon as practical
In Flight
If Icing Conditions Exist:
1. PITOT HEAT Switch.........................................................Verify ON
2. ICE PROTECT System Switch ..................................................ON
3. ICE PROTECT Mode Switch ...................................NORM / HIGH
4. WIND SHLD Push-Button......................... PRESS AS REQUIRED
5. Monitor ice accumulation.
If ice accumulation occurs:
a. ICE PROTECT Mode ......................................................HIGH
If ice continues accumulating:
b. ICE PROTECT Mode Push-Button................................... MAX
If ice accretions do not shed:
c. PUMP BKUP Switch............................................................ON
d. Perform Anti-Ice System Failure checklist.
Revision 02: 11-17-09
22 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Inadvertent Icing Encounter:
1. PITOT HEAT Switch .........................................................Verify ON
2. ICE PROTECT System Switch.................................................. ON
a. ICE PROTECT Mode Push-Button...................................MAX
to initially dissipate ice accumulation, then
b. ICE PROTECT Mode Switch .............................HIGH / NORM
If excess ice accumulation occurs, then:
c. ICE PROTECT Mode Push-Button...................................MAX
If ice does not shed perform Anti-Ice System Failure checklist.
3. WIND SHLD Push-Button .........................PRESS AS REQUIRED
4. Airspeed....................................................MAINTAIN 95-177 KIAS
or less than 204 KTAS
While in Icing Conditions:
1. FLAPS........................................................................................UP
2. Ice-Inspection Lights .............................................. AS REQUIRED
3. Cabin Heat .............................................................................. HOT
4. Windshield Defrost .................................................................... ON
5. Anti-Ice Fluid Quantity....................................................MONITOR
a. Ensure adequate quantity to complete flight.
After Leaving Icing Conditions:
1. Anti-Ice System........................................................................OFF
2. Airspeed...................................... as flight CONDITIONS DICTATE
3. Ice-Inspection Lights .............................................. AS REQUIRED
4. Cabin Heat ............................................................. AS REQUIRED
5. Windshield Defrost ................................................. AS REQUIRED
6. WIND SHLD Push-Button .........................PRESS AS REQUIRED
Revision 02: 11-17-09
P/N 13772-134 23 of 44
Cirrus Design Section 9
SR22 Supplements
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 does not shed:
a. ICE PROTECT Mode Push-Button................................... MAX
b. Perform Anti-Ice System Failure checklist.
4. WIND SHLD Push-Button......................... PRESS AS REQUIRED
• Caution •
To prevent an obstructed view due to residual anti-ice 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
　
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本文鏈接地址：西銳20飛機(jī)信息手冊 SR22 AIRPLANE INFORMATION MANUAL 2979(105)