Takeoff Rate Of Climb - Cirrus DESIGN SR22 Pilot Operating Handbook

Section 5
Performance Data

Takeoff Rate of Climb

Conditions:
• Power.................................................................................................... Full Throttle
• Mixture....................................................................................................... Full Rich
• 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.
Aircraft with optional Air Conditioning System - Maximum rate of climb
performance is reduced by approximately 50 feet per minute. For maximum
climb performance the air-conditioner should be off.
Weight Press
Altitude
LB FT
SL
2000
4000
3400
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
5-18
• 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
Cirrus Design
40 50
1277 1265
1153 1139
1028 1012
901 884
774 755
644 624
1598 1585
1457 1442
1316 1299
1172 1154
1028 1008
883 861
P/N 13772-002
Reissue A
SR22
ISA
1304
1189
1074
958
843
727
1626
1494
1363
1232
1101
971