Cirrus SR22 Pilot Operating Handbook page 448

Plane
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Section 9
Supplements
Takeoff Rate of Climb
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture............................................................................................ Set per Placard
• Flaps................................................................................................................. 50%
• Airspeed .................................................................................... Best Rate of Climb
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.
Weight
Press
Altitude
LB
FT
SL
2000
4000
3400
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
24 of 48
• Note •
RATE OF CLIMB ~ Feet per Minute
Climb
Speed
KIAS
-20
91
1326
90
1214
89
1100
88
985
88
869
87
851
91
1646
90
1518
89
1389
88
1259
88
1128
87
995
Temperature ~°C
0
20
1317
1300
1200
1179
1082
1057
962
934
842
809
719
683
1638
1621
1505
1484
1371
1346
1236
1207
1100
1066
962
924
Revision 03: 05-09-11
Cirrus Design
SR22
40
ISA
1277
1304
1153
1189
1028
1074
901
958
774
843
644
727
1598
1626
1457
1494
1316
1363
1172
1232
1028
1101
883
971
13772-130

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