Cirrus SR22 Pilot Operating Handbook page 450

Plane
Table of Contents

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Section 9
Supplements
Conditions:
• Power...............................Full Throttle
• Mixture............................As Required
• Flaps..................................... 0% (UP)
• Airspeed ...............Best Rate of Climb
• 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.
Weight
Press
Alt
LB
FT
SL
2000
4000
6000
3400
8000
10000
12000
14000
16000
SL
2000
4000
6000
2900
8000
10000
12000
14000
16000
26 of 48
Enroute Rate of Climb
• Note •
Climb
Speed
KIAS
-20
101
1428
100
1311
99
1193
98
1074
97
953
96
830
95
706
94
581
93
454
101
1761
100
1629
99
1494
98
1359
97
1222
95
1084
95
945
93
804
92
662
Example:
Outside Air Temp ...................... 10° C
Weight................................... 3400 LB
Pressure Altitude................... 6000 FT
Climb Airspeed..................... 97 Knots
Rate of Climb .....................1030 FPM
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
0
20
1414
1392
1292
1267
1170
1141
1046
1013
921
884
794
754
666
623
537
490
406
355
1748
1726
1610
1584
1471
1441
1331
1296
1189
1151
1046
1004
902
855
757
706
610
556
Cirrus Design
SR22
40
ISA
1366
1398
1238
1279
1108
1160
977
1041
845
922
712
803
577
684
441
565
303
446
1698
1732
1552
1596
1405
1461
1257
1326
1108
1191
958
1056
806
921
653
787
499
653
13772-130
Revision 03: 05-09-11

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