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4000 94 474 418 367 319 402
6000 93 392 338 289 244 332
8000 92 313 216 214 171 265
10000 91 237 188 200
12000 91 164 118 139
14000 90 95 51 80
2500
SL 93 846 777 712 652 728
2000 92 741 674 612 554 640
4000 92 640 576 516 461 555
6000 91 543 482 425 473
8000 90 451 392 337 395
10000 89 363 306 320
12000 88 279 224 248
14000 88 198 147 180
Figure 5-12
March 2010
5-24 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-13
Enroute Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude in feet per unit time expressed in
Feet per Minute.
• For operation in air colder than this table provides, use coldest data shown.
• For operation in air warmer than this table provides, use extreme caution.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
• The Maximum Operating Altitude of 17,500 feet MSL may be obtained if the
airplane’s gross weight does not exceed 2900 lb and the ambient temperature is
-20° C or less.
Conditions: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 10° C
• 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
Figure 5-14
March 2010 Density Altitude ~
Feet
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
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
　
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