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3. Time ................................................................................... NOTED
4. Exit icing conditions. Turn back and/or change altitude.
5. Cabin Heat .................................................................... MAXIMUM
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Cirrus Design Section 9
SR22 Supplements
6. Windshield Defrost...................................................... FULL OPEN
7. Alternate Induction Air ...............................................................ON
8. When Icing Conditions Cleared, Ice Protection System ..........OFF
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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%.
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Cirrus Design Section 9
SR22 Supplements
Section 6 - Weight & Balance
Ice Protection System installation adds the optional (Sym = O)
equipment at the weight, arm, and moment/1000 shown in the
following figure.
• Note •
De-icing fluid weight is 9.2 pounds per U.S gallon.
ATA/
Item
Description Sym Qty Part Number
Unit
Wt
Arm
30-01 Propeller Slinger Ring O 1 15321-001 1.5 55.0
30-02 De-Icing Fluid Reservoira
a. Serials before G3 Wing only. Note: Serials with G3 Wing, reservoir is integral
to wing.
O 1 15269-001 4.2 181.0
30-03 Metering Pumpa O 1 15165-013 4.5 176.0
30-04 Metering Pumpb
b. Serials with G3 Wing.
O 1 17351-102 4.5 176.0
30-05 Priming Pumpb O 1 17351-103 0.70 176.0
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Supplements SR22
Figure - 2 (Sheet 1 of 2)
De-Icing Fluid Reservoir, Fuselage
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 5.07
14.0 2.53
a. 2.96 U.S. Gallons Capacity
Loading Data - Serials before G3 Wing
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Cirrus Design Section 9
SR22 Supplements
De-Icing Fluid Reservoir, 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
2.0 0.30 20.0 2.96
3.0 0.44 21.0 3.11
4.0 0.59 22.0 3.26
5.0 0.74 23.0 3.40
6.0 0.89 24.0 3.55
7.0 1.04 25.0 3.70
8.0 1.18 26.0 3.85
9.0 1.33 27.0 4.00
10.0 1.48 28.0 4.14
11.0 1.63 29.0 4.29
12.0 1.78 30.0 4.44
13.0 1.92 31.0 4.59
14.0 2.07 32.0 4.74
15.0 2.22 33.0 4.88
16.0 2.37 34.50a 5.11
17.0 2.52
a. 3.75 U.S. Gallons Capacity
Figure - 2 (Sheet 2 of 2)
Loading Data - Serials with G3 Wing
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Section 9 Cirrus Design
Supplements SR22
Section 7 - System Description
The Ice Protection System can prevent, and in certain conditions,
　
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