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• 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............................................................................................ Set per Placard
• 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 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 88 869 842 809 774 843
10000 87 851 719 683 644 727
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 88 1128 1100 1066 1028 1101
10000 87 995 962 924 883 971
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-17
Enroute Climb Gradient
• Note •
Climb Gradients shown are the gain in altitude for the horizontal distance
traversed expressed as Feet per Nautical Mile.
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:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps .......................................................................................................... 0% (UP)
• Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~°C
-20 0 20 40 ISA
3400
SL 101 911 867 823 781 834
2000 100 813 771 729 689 748
4000 99 720 679 639 600 665
6000 98 630 590 552 515 584
8000 97 544 505 468 433 507
10000 96 461 424 388 354 433
12000 95 381 346 312 279 361
14000 94 304 271 238 207 292
16000 93 231 199 168 139 226
2900
SL 101 1130 1078 1026 975 1039
2000 100 1015 965 915 867 937
4000 99 905 857 809 763 840
6000 98 800 753 708 664 746
8000 97 699 654 611 569 656
10000 96 603 560 518 478 570
12000 95 610 469 429 391 487
14000 94 422 382 344 308 407
16000 93 337 299 263 229 331
March 2010
5-18 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Enroute Rate of Climb
• Note •
Rate-of-Climb values shown are change in altitude in feet per unit time
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:
• Power.................................................................................................... Full Throttle
• Mixture................................................................................................. As Required
• Flaps...........................................................................................................0% (UP)
　
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