CIRRUS DESIGN SR22 - Page 142

5-28 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Figure 5-16
Cruise Performance
8000 Feet Pressure Altitude
ISA - 30° C (-31° C) ISA (-1° C) ISA + 30° C (29° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 21.7 83% 183 19.7 78% 183 18.6 75% 178 17.7
2600 21.7 79% 180 18.8 75% 180 17.8 71% 175 17.0
2500 21.7 75% 176 17.7 71% 176 16.8 67% 171 16.0
2500 20.7 70% 172 16.7 66% 172 15.8 63% 167 15.0
2500 19.7 66% 168 15.6 62% 168 14.8 59% 163 14.0
2500 18.7 61% 163 14.5 58% 163 13.8 55% 158 13.1
2500 17.7 57% 159 13.5 54% 159 12.8 51% 153 12.1
10,000 Feet Pressure Altitude
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
March 2010