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5. Exit icing conditions. Turn back and/or change altitude.
6. Cabin Heat .................................................................... MAXIMUM
7. Windshield Defrost ......................................................FULL OPEN
8. Alternate Induction Air............................................................... ON
9. When Icing Conditions Cleared, Ice Protection System...........OFF
10. Airspeed................................................ As flight conditions dictate
Revision 07: 05-13-08
P/N 13772-115 5 of 16
Cirrus Design Section 9
SR22 Supplements
Section 3A - Abnormal Procedures
The following Crew Alerting System (CAS) annuciations are available
only on Serial Numbers 2979 and subsequent with Cirrus Perspective
Integrated Avionics System installed.
Response to De-icing Fluid Low CAS Annunciation
Red ANTI ICE QTY Warning: The Ice Protection System is operating
in NORMAL or MAX mode and de-icing fluid quantity is less than 0.5
gallon (1.9 L).
Amber ANTI ICE QTY Caution: The Ice Protection System is
operating in NORMAL or MAX mode and de-icing fluid quantity is
between 0.5 - 1.0 gallon (1.9 - 3.8 L).
White ANTI ICE QTY Advisory: The Ice Protection System is ‘off”
and de-icing fluid is less than or equal to 1.0 gallon (3.8 L).
1. Ice Protection System.............................. MONITOR OPERATION
2. De-icing Fluid Level ................CHECK, SERVICE AS REQUIRED
ANTI ICE QTY
Revision 07: 05-13-08
6 of 16 P/N 13772-115
Section 9 Cirrus Design
Supplements SR22
Section 4 - Normal Procedures
Pre-Flight Inspection
1. Battery Master Switch ............................................................... ON
2. Ice Protection Switch .................................................... MAXIMUM
3. Anti-Icing Fluid Quantity.................................................Check Full
4. Fluid Vent (underside) ............................................... Unobstructed
5. Porous Panels .............................................Condition and Security
• Note •
If allowed to run dry, the system may require maintenance.
Refer to Section 8 for priming procedure.
6. Porous Panels .......................................Evidence of De-Icing Fluid
7. Slinger Ring ..........................................Evidence of De-Icing Fluid
8. Ice Protection Switch ...............................................................OFF
9. Battery Master Switch ..............................................................OFF
Section 5 - Performance
Cruise speed is lower by approximately three knots and range is
reduced by a maximum of 2%.
• Note •
Experience with your airplane’s power settings may result in
more accurate performance numbers than those given above.
1. Reduce KTAS shown on the Cruise Performance tables and the
Range/Endurance Profile tables by 3 knots.
2. Reduce range shown on the Range/Endurance Profiles by 2%.
During certain flight conditions, such as at higher operating altitudes
and/or higher airspeeds, the stagnation point on the leading edge of
the wing (the point where the airflow splits) will move up and aft
enough to hinder the deicing fluid from flowing adequately along the
top surface of the wing. Airspeed for optimum system performance is
95-139 KIAS. Do not exceed 175 KTAS above 14000 ft.
Revision 07: 05-13-08
P/N 13772-115 7 of 16
Cirrus Design Section 9
SR22 Supplements
Section 6 - Weight & Balance
De-icing fluid weight is 9.2 pounds per U.S gallon.
Refer to Section 6 - Weight and Balance of the basic POH for weight
and balance equipment data.
Loading Data
Fuselage De-Icing Fluid Reservoir - Serials before G3 Wing
Weight
LB
Moment/1000
Fluid Reservoir
FS 181.0
Weight
LB
Moment/1000
Fluid Reservoir
FS 181.0
0.5 0.09 15.0 2.72
1.0 0.18 16.0 2.90
2.0 0.36 17.0 3.08
3.0 0.54 18.0 3.26
4.0 0.72 19.0 3.44
5.0 0.91 20.0 3.62
6.0 1.09 21.0 3.80
7.0 1.27 22.0 3.98
8.0 1.45 23.0 4.16
9.0 1.63 24.0 4.34
10.0 1.81 25.0 4.53
11.0 1.99 26.0 4.71
12.0 2.17 27.0 4.89
13.0 2.35 28.0a
a.2.9 gallon (11.0 L) Capacity
5.07
14.0 2.53
Revision 07: 05-13-08
8 of 16 P/N 13772-115
Section 9 Cirrus Design
Supplements SR22
Loading Data (Continued)
Wing De-Icing Fluid Reservoir - Serials with G3 Wing
Weight
LB
Moment/1000
Fluid Reservoir
FS 148.0
Weight
LB
Moment/1000
Fluid Reservoir
FS 148.0
0.5 0.07 18.0 2.66
1.0 0.15 19.0 2.81
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(121)
