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Climb
FPM
TIME, FUEL, DISTANCE ~ From Sea Level
Time
Minutes
Fuel
U.S. Gal
Distance
NM
SL 15 96 880 0.0 0.0 0
1000 13 96 828 1.3 0.3 2
2000 11 95 775 2.4 0.6 4
3000 9 94 723 3.8 1.0 6
4000 7 94 671 5.2 1.3 8
5000 5 93 618 6.7 1.7 11
6000 3 93 566 8.4 2.0 14
7000 1 92 514 10.3 2.4 17
8000 -1 92 462 12.3 2.9 21
9000 -3 91 409 14.6 3.3 25
10000 -5 91 357 17.2 3.8 29
11000 -7 91 305 20.3 4.4 35
12000 -9 91 252 23.8 5.0 41
13000 -11 91 200 28.3 5.8 49
14000 -13 90 148 34.0 6.8 60
March 2010
Information Manual 5-27
Cirrus Design Section 5
SR20 Performance Data
Cruise Performance
Conditions: Example:
• Mixture ............................. Best Power Outside Air Temp29° C
• Cruise Weight........................2600 LB RPM 2700 RPM
• Winds ..........................................Zero Cruise Press Alt8000 FT
Note: Subtract 10 KTAS if nose wheel pant
and fairing removed. Lower KTAS by 10% if % Power (22.2 MAP)73%
nose & main wheel pants & fairings removed. True Airspeed154 Knots
Cruise Pwr above 85% not recommended. Fuel Flow11.4 GPH
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
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
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(44)
