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ISA - 30° C (-35° C) ISA (-5° C) ISA + 30° C (25° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 20.0 77% 182 18.2 73% 182 17.3 69% 176 16.4
2600 20.0 71% 177 17.0 68% 177 16.1 64% 172 15.3
2500 20.0 67% 173 16.0 64% 173 15.1 61% 167 14.4
2500 19.0 63% 168 14.9 59% 168 14.1 56% 163 13.4
2500 18.0 58% 163 13.8 55% 163 13.1 52% 158 12.5
2500 17.0 54% 158 12.8 51% 158 12.1 48% 153 11.5
12,000 Feet Pressure Altitude
ISA - 30° C (-39° C) ISA (-9° C) ISA + 30° C (21° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 18.5 71% 180 16.9 67% 180 16.0 64% 175 15.2
2600 18.5 68% 177 16.2 64% 177 15.3 61% 172 14.5
2500 18.5 64% 173 15.2 60% 173 14.4 58% 167 13.7
2500 17.5 59% 168 14.1 56% 168 13.4 53% 162 12.7
2500 16.5 55% 162 13.0 52% 162 12.3 49% 157 11.7
2500 15.5 50% 156 12.0 48% 156 11.3 45% 151 10.8
14,000 Feet Pressure Altitude
ISA - 30° C (-43° C) ISA (-13° C) ISA + 30° C (17° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 17.1 66% 178 15.6 62% 178 14.8 59% 173 14.1
2600 17.1 63% 175 14.9 60% 175 14.1 57% 170 13.5
2500 17.1 59% 171 14.1 56% 171 13.3 53% 165 12.7
2500 16.1 55% 165 13.0 52% 165 12.3 49% 159 11.7
2500 15.1 50% 159 11.9 47% 159 11.2 45% 153 10.7
Sheet 2 of 3
Revision A5
P/N 13772-001 5-29
Cirrus Design Section 5
SR22 Performance Data
Cruise Performance
16,000 Feet Pressure Altitude
ISA - 30° C (-47° C) ISA (-17° C) ISA + 30° C (13° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 15.8 61% 176 14.5 58% 176 13.7 55% 171 13.0
2600 15.8 58% 173 13.8 55% 173 13.1 52% 167 12.5
2500 15.8 55% 168 13.0 52% 168 12.3 49% 163 11.7
2500 14.8 50% 162 11.9 47% 162 11.3 45% 156 10.7
17,000 Feet Pressure Altitude
ISA - 30° C (-49° C) ISA (-19° C) ISA + 30° C (9° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 15.2 59% 175 13.9 55% 175 13.2 53% 169 12.5
2600 15.2 56% 171 13.3 53% 171 12.6 50% 166 12.0
2500 15.2 53% 167 12.5 50% 167 11.9 47% 162 11.3
2500 14.2 48% 160 11.4 45% 160 10.8 43% 155 10.3
Figure 5-16
Sheet 3 of 3
Revision A7
5-30 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
Figure 5-17
Range / Endurance Profile
• Note •
• Fuel Remaining For Cruise is equal to 81.0 gallons usable, less climb fuel, 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.
Conditions: Example:
• Weight .................................. 3400 LB Power Setting ............................. 75%
• 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..........................2.0 Gal.
Cruise Fuel Flow................ 17.8 GPH
Endurance................................ 3.9 Hr
Range ....................................689 NM
True Airspeed..................... 177 Knots
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 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
Revision A8
P/N 13772-001 5-31
Cirrus Design Section 5
SR22 Performance Data
Range / Endurance Profile
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 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
　
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