Cirrus DESIGN SR20 - Cruise Performance (Continued)

5-22 P/N 11934-004
Section 5 Cirrus Design
Performance Data SR20
Cruise Performance (Continued)
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 22.2 82% 157 12.9 77% 157 11.6 73% 154 11.4
2500 22.2 73% 150 11.4 69% 150 11.0 65% 147 10.6
2500 21.2 69% 146 10.9 65% 146 10.5 62% 143 10.2
2500 20.1 64% 142 10.4 60% 142 10.0 57% 139 9.7
2500 18.9 59% 136 9.8 55% 136 9.5 52% 134 9.2
2500 17.7 53% 131 9.2 50% 131 8.9 48% 128 8.7
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 20.6 76% 155 11.7 72% 155 11.2 68% 152 10.9
2500 20.6 68% 148 10.8 64% 148 10.5 61% 145 10.1
2500 19.6 64% 144 10.4 60% 144 10.0 57% 141 9.7
2500 18.5 59% 139 9.8 55% 139 9.5 53% 136 9.2
2500 17.3 54% 134 9.3 50% 134 9.0 48% 131 8.7
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 19.0 70% 153 11.1 66% 153 10.7 63% 150 10.3
2500 19.0 63% 146 10.3 59% 146 9.9 56% 143 9.6
2500 18.0 59% 141 9.8 55% 141 9.5 52% 138 9.2
2500 16.8 53% 136 9.2 50% 136 8.9 47% 133 8.6
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 17.6 66% 151 10.5 62% 151 10.2 58% 148 9.8
2500 17.6 59% 144 9.8 55% 144 9.5 52% 141 9.2
2500 16.5 54% 142 9.3 50% 142 9.0 48% 139 8.7
Original Issue