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less 9.8 gallons for 45 minutes IFR reserve fuel at 47% power (ISA @ 10,000
ft PA), less descent fuel, less fuel used prior to takeoff.
Range and endurance shown includes descent to final destination at
approximately 178 KIAS and 500 fpm.
Range is decreased by 5% if nose wheel pant and fairings removed.
Range is decreased by 15% if nose and main wheel pants and fairings
removed.
Aircraft with optional air-conditioning system - Range is decreased by 1%. For
maximum range the air-conditioner should be off.
Conditions:
• Weight ........................................................................................................3400 LB
• Temperature ...................................................................................... Standard Day
• Winds................................................................................................................Zero
• Mixture.............................................................................................. Best Economy
• Total Fuel ................................................................................................ 92 Gallons
75% POWER Mixture: Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 81.3 166 17.8 4.6 763 9.3
2000 0.7 81.1 170 17.8 4.6 775 9.6
4000 1.3 80.4 173 17.8 4.5 786 9.8
6000 2.0 79.7 177 17.8 4.5 797 10.0
8000 2.7 79.0 180 17.8 4.4 811 10.3
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-25
Range / Endurance Profile (Continued)
65% POWER Mixture: Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 81.3 158 15.4 5.3 838 10.3
2000 0.7 81.1 161 15.4 5.3 850 10.5
4000 1.3 80.4 165 15.4 5.2 862 10.7
6000 2.0 79.7 168 15.4 5.2 874 11.0
8000 2.7 79.0 171 15.4 5.1 887 11.2
10000 3.5 78.2 174 15.4 5.1 899 11.5
12000 4.4 77.1 178 15.4 5.0 912 11.8
55% POWER Mixture: Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 81.8 149 13.1 6.3 931 11.4
2000 0.7 81.1 152 13.1 6.2 943 11.6
4000 1.3 80.4 154 13.1 6.2 955 11.9
6000 2.0 79.7 157 13.1 6.1 968 12.2
8000 2.7 79.0 160 13.1 6.0 980 12.4
10000 3.5 78.3 163 13.1 6.0 993 12.7
12000 4.4 77.4 166 13.1 5.9 1005 13.0
14000 5.3 76.5 169 13.1 5.8 1018 13.4
55% POWER Mixture: Best Economy
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 81.8 149 11.3 7.2 1074 13.1
2000 0.7 81.1 152 11.3 7.2 1088 13.4
4000 1.3 80.4 154 11.3 7.1 1108 13.7
6000 2.0 79.7 157 11.3 7.0 1115 14.0
8000 2.7 79.0 160 11.3 7.0 1129 14.3
10000 3.5 78.3 163 11.3 6.9 1143 14.6
12000 4.4 77.4 166 11.3 6.8 1156 15.0
14000 5.3 76.5 169 11.3 6.7 1170 15.4
March 2010
5-26 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Balked Landing Climb Gradient
• Note •
Balked Landing Climb Gradients shown are the gain in altitude for the
horizontal distance traversed expressed as Feet per Nautical Mile.
For operation in air colder than this table provides, use coldest data shown.
For operation in air warmer than this table provides, use extreme caution.
This chart is required data for certification. However, significantly better
performance can be achieved by climbing at Best Rate of Climb speeds
shown with flaps down or following the Go-Around / Balked Landing
procedure in Section 4.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture............................................................................................ Set per Placard
• Flaps...................................................................................................... 100% (DN)
• Climb Airspeed ...............................................................................................VREF
　
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