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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
Figure 5-16
Sheet 1 of 2
March 2010
5-28 Information Manual
Section 5 Cirrus Design
Performance Data SR20
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 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
Sheet 2 of 2
March 2010
Information Manual 5-29
Cirrus Design Section 5
SR20 Performance Data
Range / Endurance Profile
• Note •
• Fuel Remaining For Cruise accounts for 10.1 gallons for 45 minutes IFR reserve
fuel at 75% power and fuel burn for descent.
• Range and endurance shown includes descent to final destination at 160 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 ...................................3000 LB Power Setting .............................75%
• Temperature ................. Standard Day Takeoff Press Alt .................. 2000 FT
• Winds ..........................................Zero Cruise Press Alt.................... 6000 FT
• Mixture ............................. See Tables
• Total Fuel........................... 56 Gallons Fuel to Climb ......................... 1.3 Gal.
Cruise Fuel Flow ................11.6 GPH
Endurance ................................ 4.0 Hr
Range.................................... 617 NM
True Airspeed .....................152 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
0 0.0 46.3 143 11.6 4.0 576 12.3
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 1148-126(43)
