5-18 P/N 13772-004
Section 5 Cirrus Design
Performance Data SR22
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.
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.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture....................................................................................................... Full Rich
• Flaps................................................................................................................. 50%
• Airspeed .................................................................................... Best Rate of Climb
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~°C
-20 0 20 40 50 ISA
3600
SL 97 1361 1310 1256 1200 1172
1270
2000 95 1215 1161 1104 1045 1015
1129
4000 94 1068 1010 950 889 858 989
6000 92 920 859 796 732 700
849
8000 90 770 706 640 574 541
709
10000 89 620 552 483 415 380 568
2900
SL 91 1646 1638 1621 1598 1585
1626
2000 90 1518 1505 1484 1457 1442
1494
4000 89 1389 1371 1346 1316 1299 1363
6000 88 1259 1236 1207 1172 1154
1232
8000 88 1128 1100 1066 1028 1008
1101
10000 87 995 962 924 883 861 971
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