Cirrus DESIGN SR20 - Cruise Performance

Cirrus Design Section 5
SR20 Performance Data
P/N 11934-004 5-21
Cruise Performance
• Note •
Subtract 10 KTAS if nose wheel pant and fairing removed. Lower KTAS by
10% if nose and main wheel pants & fairings are removed.
Shaded data cells: Cruise Power above 85% not recommended.
Conditions:
• Cruise Weight............................................................................................. 2600 LB
• Winds ............................................................................................................... Zero
2000 Feet Pressure Altitude
ISA - 30° C (-19° C) ISA (11° C) ISA + 30° C (41° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 27.8 101% 160 16.0 95% 160 15.0 91% 157 14.2
2500 27.8 90% 154 14.1 85% 154 13.4 81% 151 12.9
2500 26.6 85% 151 13.4 80% 151 12.8 76% 148 11.7
2500 25.4 80% 147 12.7 75% 147 11.6 72% 144 11.3
2500 24.1 74% 143 11.5 70% 143 11.1 67% 140 10.7
2500 22.9 69% 139 11.0 65% 139 10.6 62% 136 10.2
2500 22.0 65% 136 10.5 62% 136 10.2 59% 133 9.9
2500 19.7 55% 127 9.5 52% 127 9.20 50% 124 8.9
4000 Feet Pressure Altitude
ISA - 30° C (-23° C) ISA (7° C) ISA + 30° C (37° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 25.8 94% 159 14.8 89% 159 14.4 84% 157 13.4
2500 25.8 84% 153 13.3 79% 153 12.7 75% 150 11.7
2500 24.8 80% 150 12.7 75% 150 11.6 72% 147 11.2
2500 23.6 75% 146 11.5 70% 146 11.1 67% 143 10.8
2500 22.3 69% 141 10.9 65% 141 10.5 62% 138 10.2
2500 21.0 63% 136 10.3 60% 136 10.0 57% 133 9.7
2500 19.8 58% 131 9.8 55% 131 9.4 52% 129 9.2
6000 Feet Pressure Altitude
ISA - 30° C (-27° C) ISA (3° C) ISA + 30° C (33° C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 24.0 88% 159 13.8 83% 159 13.1 79% 156 12.6
2500 24.0 79% 152 12.0 74% 152 11.5 71% 149 11.1
2500 23.0 74% 148 11.5 70% 148 11.1 67% 145 10.7
2500 21.8 69% 144 11.0 65% 144 10.6 62% 141 10.2
2500 20.8 65% 140 10.4 61% 140 10.0 58% 137 9.7
2500 19.4 59% 134 9.8 55% 134 9.5 53% 131 9.2
Original Issue