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Conditions: Example:
• Weight .................................. 3400 LB Power Setting ............................. 55%
• Temperature .................Standard Day Takeoff Press Alt ..................2000 FT
• Winds.......................................... Zero Cruise Press Alt ....................6000 FT
• Mixture.........................Best Economy
• Total Fuel .......................... 81 Gallons Fuel to Climb..........................1.3 Gal.
Cruise Fuel Flow................ 11.3 GPH
Endurance................................ 6.1 Hr
Range ....................................962 NM
True Airspeed..................... 157 Knots
75% POWERMixture = 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 70.8 166 17.8 4.0 661 9.3
2000 0.7 69.0 170 17.8 3.9 670 9.6
4000 1.3 67.2 173 17.8 3.9 680 9.8
6000 2.0 65.3 177 17.8 3.9 689 10.0
8000 2.7 63.5 180 17.8 3.8 700 10.3
Sheet 1 of 3
June 2007
Information Manual 5-31
Cirrus Design Section 5
SR22 Performance Data
Range / Endurance Profile
65% POWERMixture = 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 70.8 158 15.4 4.6 725 10.3
2000 0.7 69.0 161 15.4 4.5 735 10.5
4000 1.3 67.2 165 15.4 4.5 745 10.7
6000 2.0 65.3 168 15.4 4.5 755 11.0
8000 2.7 63.5 171 15.4 4.4 765 11.2
10000 3.5 61.6 174 15.4 4.4 775 11.5
12000 4.4 59.8 178 15.4 4.3 785 11.8
55% POWERMixture = 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 70.8 149 13.1 5.4 806 11.4
2000 0.7 69.0 152 13.1 5.4 815 11.6
4000 1.3 67.2 154 13.1 5.3 825 11.9
6000 2.0 65.3 157 13.1 5.3 835 12.2
8000 2.7 63.5 160 13.1 5.2 845 12.4
10000 3.5 61.6 163 13.1 5.1 856 12.7
12000 4.4 59.8 166 13.1 5.1 865 13.0
14000 5.3 57.8 169 13.1 5.0 875 13.4
Figure 5-17
Sheet 2 of 3
June 2007
5-32 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Figure 5-17
Range / Endurance Profile
55% POWERMixture = 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 70.8 149 11.3 6.2 930 13.1
2000 0.7 69.0 152 11.3 6.2 941 13.4
4000 1.3 67.2 154 11.3 6.1 951 13.7
6000 2.0 65.3 157 11.3 6.1 962 14.0
8000 2.7 63.5 160 11.3 6.0 974 14.3
10000 3.5 61.6 163 11.3 5.9 985 14.6
12000 4.4 59.8 166 11.3 5.9 995 15.0
14000 5.3 57.8 169 11.3 5.8 1006 15.4
Sheet 3 of 3
June 2007
Information Manual 5-33
Cirrus Design Section 5
SR22 Performance Data
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: Example:
• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ...................... Set per Placard Weight .................................. 3400 LB
• Flaps ................................ 100% (DN) Pressure Altitude .................. 4000 FT
• Climb Airspeed...........................VREF
Climb Airspeed .....................77 Knots
Rate of Climb....................633 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile Best
Rate
of
Climb
KIAS
Temperature ~ °C
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(45)
