5-22 Information Manual
Section 5 Cirrus Design
Performance Data SR22
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.
• Fuel flow must be set to the placarded limit for all takeoffs and climbs.
• 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 ...................... 10° C
• Mixture.......................Set per Placard Weight...................................3400 LB
• Flaps........................................... 50% Pressure Altitude...................6000 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 88 Knots
Rate of Climb .......................948 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 91 1326 1317 1300 1277 1304
2000 90 1214 1200 1179 1153
1189
4000 89 1100 1082 1057 1028
1074
6000 88 985 962 934 901 958
8000 87 869 842 809 774
843
10000 86 851 719 683 644
727
2900
SL 91 1646 1638 1621 1598 1626
2000 90 1518 1505 1484 1457
1494
4000 89 1389 1371 1346 1316
1363
6000 88 1259 1236 1207 1172 1232
8000 87 1128 1100 1066 1028
1101
10000 86 995 962 924 883
971
March 2010
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