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• Mixture..................................Full Rich Weight...................................3000 LB
• Flaps.....................................0% (UP) Pressure Altitude...................6500 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 93 Knots
Rate of Climb .......................513 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3000
SL 96 979 923 866 808 880
2000 95 868 808 748 688 775
4000 94 756 693 630 567 671
6000 93 642 576 510 445 566
8000 92 527 458 389 321 462
10000 91 411 339 357
12000 91 294 218 252
14000 90 175 97 148
2500
SL 93 1231 1175 1117 1058 1132
2000 92 1109 1050 988 926 1016
4000 92 987 923 858 793 900
6000 91 863 796 727 785
8000 90 738 667 595 670
10000 89 612 537 555
12000 88 484 405 440
14000 88 355 273 325
March 2010
Information Manual 5-25
Cirrus Design Section 5
SR20 Performance Data
Enroute Rate of Climb Vs Density Altitude
Conditions:
• Power .................................................................................................... Full Throttle
• Mixture ....................................................................................................... Full Rich
• Flaps ...........................................................................................................0% (UP)
• Airspeed..................................................................................... Best Rate of Climb
1,000
2,000
3,000
4,000
5,000
6,000
7,000
8,000
9,000
10,000
11,000
12,000
13,000
14,000
15,000
100
200
300
400
500
600
700
800
900
1000
1100
1200
2500 LB
3000 LB
Rate of Climb ~ Feet Per Minute
Figure 5-14
March 2010
5-26 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-15
Time, Fuel and Distance to Climb
Factors:
• Taxi Fuel - Add 1 gallon for start, taxi, and takeoff.
• Temperature - Add 10% to computed values for each 10º C above standard.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
Conditions: Example:
• Power...............................Full Throttle Outside Air Temp ......................... ISA
• Mixture..................................Full Rich Weight...................................3000 LB
• Fuel Density..................... 6.0 LB/GAL Airport Press.........................1000 FT
• Weight .................................. 3000 LB Pressure Altitude.................12000 FT
• Winds.......................................... Zero
• Climb Airspeed .........................Noted Time to Climb.................22.5 Minutes
Fuel to Climb......................4.7 Gallon
Distance to Climb.....................39 NM
Press
Alt
FT
OAT
(ISA)
°C
Climb
Speed
KIAS
Rate Of
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 Temp...................29° C
• Cruise Weight........................2600 LB RPM ..............................2700 RPM
• Winds ..........................................Zero Cruise Press Alt................ 8000 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 Airspeed ................ 154 Knots
Cruise Pwr above 85% not recommended. Fuel Flow........................11.4 GPH
2000 Feet Pressure Altitude
ISA - 30° C (-19° C) ISA (11° C) ISA + 30° C (41° C)
　
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