5-20 P/N 13772-002
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.
Aircraft with optional Air Conditioning System: Maximum rate of climb
performance is reduced by approximately 50 feet per minute if system is ON.
For maximum climb performance the air-conditioner should be off.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture................................................................................................. As Required
• Flaps...........................................................................................................0% (UP)
• 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
3400
SL 101 1428 1414 1392 1366 1351 1398
2000 100 1311 1292 1267 1238 1221
1279
4000 99 1193 1170 1141 1108 1090
1160
6000 98 1074 1046 1013 977 958
1041
8000 97 953 921 884 845 824
922
10000 96 830 794 754 712 689
803
12000 95 706 666 623 577 553
684
14000 94 581 537 490 441 416
565
16000 93 454 406 355 303 277
446
2900
SL 101 1761 1748 1726 1698 1683
1732
2000 100 1629 1610 1584 1552 1535
1596
4000 99 1494 1471 1441 1405 1386
1461
6000 98 1359 1331 1296 1257 1237
1326
8000 97 1222 1189 1151 1108 1086
1191
10000 95 1084 1046 1004 958 934
1056
12000 95 945 902 855 806 781
921
14000 93 804 757 706 653 626
787
16000 92 662 610 556 499 471
653
Reissue A