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SL 84 957 880 808 741 826
2000 84 841 767 698 634 729
4000 83 730 659 593 531 636
6000 82 624 555 492 545
8000 81 522 456 396 459
10000 80 425 362 377
Figure 5-10
March 2010
5-22 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-11
Takeoff Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude for unit time expended
expressed in Feet per Minute.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
• 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.
Conditions: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 20° C
• Mixture..................................Full Rich Weight...................................3000 LB
• Flaps........................................... 50% Pressure Altitude...................1750 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 85 Knots
Rate of Climb .......................725 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3000
SL 85 905 862 817 771 828
2000 85 807 761 712 663 734
4000 84 707 657 606 554 639
6000 83 607 553 499 444 545
8000 82 504 447 390 333 450
10000 82 401 341 356
2500
SL 84 1256 1201 1144 1086 1158
2000 84 1136 1077 1017 955 1044
4000 83 1014 952 888 824 929
6000 82 892 825 758 815
8000 81 768 698 627 701
10000 80 643 569 587
March 2010
Information Manual 5-23
Cirrus Design Section 5
SR20 Performance Data
Enroute Climb Gradient
• Note •
• Climb Gradients shown are the gain in altitude for the horizontal distance traversed
expressed as Feet per Nautical Mile.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
• 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.
• 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.......................20° C
• Mixture ................................. Full Rich Weight .................................. 3000 LB
• Flaps .....................................0% (UP) Pressure Altitude .................. 4200 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................94 Knots
Gradient............................359 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
3000
SL 96 650 589 533 481 549
2000 95 560 502 448 398 474
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
　
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