CIRRUS DESIGN SR20, Pilot Operating Handbook, Page: 140 / 508

5-22 P/N 11934-003
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 83 607 553 499 545
8000 82 504 447 390 450
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
Revision A4