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Enroute Rate of Climb with Ice Accumulation
• 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 top of green arc 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.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .................................................................................................As Required
• Flaps .......................................................................................................... 0% (UP)
• Airspeed.....................................................................................Best Rate of Climb
Negative climb data shown in heavier table borders.
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~°C
-20 -10 0 5 ISA
3400
SL 101 817 803 787 779 1398
2000 100 686 670 652 643 1279
4000 98 553 535 516 506 1160
6000 97 420 399 378 367 1041
8000 96 285 262 239 227 241
10000 95 148 124 99 86 111
12000 95 10 -16 -43 -57 -19
14000 95 -129 -157 -186 -201 -150
16000 95 -270 -300 -331 -347 -280
2900
SL 101 1045 1030 1014 1005 986
2000 100 895 878 859 849 837
4000 98 744 725 704 693 688
6000 97 593 571 548 536 540
8000 96 439 415 390 377 392
10000 95 285 258 231 217 244
12000 95 129 100 71 56 97
14000 95 -28 -59 -91 -107 -51
16000 95 -187 -220 -254 -271 -198
Revision 02: 11-17-09
28 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Cruise Performance with Ice Accumulation
• Note •
Aircraft with optional Air Conditioning System - Cruise performance is
reduced by 2 knots. For maximum performance, the air-conditioner should be
off.
Conditions:
• Cruise Weight .............................................................................................2900 LB
• Winds................................................................................................................Zero
2000 Feet Pressure Altitude
ISA -30°C (-19°C) ISA (11°C) ISA + 30°C (41°C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 27.4 103% 160 24.6
2600 27.4 99% 157 23.5
2500 27.4 93% 153 22.1
2500 26.4 89% 150 21.1
2500 25.4 84% 146 20.0
2500 24.4 80% 142 19.0
2500 23.4 76% 137 18.0
4000 Feet Pressure Altitude
ISA -30°C (-23°C) ISA (7°C) ISA + 30°C (37°C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 25.4 96% 158 22.9
2600 25.4 92% 155 21.9
2500 25.4 87% 150 20.6
2500 24.4 82% 146 19.5
2500 23.4 78% 141 18.5
2500 22.4 73% 136 17.4
2500 21.4 69% 130 16.4
Revision 02: 11-17-09
P/N 13772-134 29 of 44
Cirrus Design Section 9
SR22 Supplements
Cruise Performance (Continued)
6000 Feet Pressure Altitude
ISA -30°C (-27°C) ISA (3°C) ISA + 30°C (33°C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 23.5 89% 155 21.2 85% 155 20.1
2600 23.5 85% 151 20.3 81% 151 19.2
2500 23.5 80% 146 19.1 76% 146 18.1
2500 22.5 76% 140 18.1 72% 140 17.1
2500 21.5 72% 134 17.0 68% 134 16.1
2500 20.5 67% 128 15.9 64% 128 15.1
2500 19.5 63% 120 14.9 59% 120 14.1
8000 Feet Pressure Altitude
ISA -30°C (-31°C) ISA (-1°C) ISA + 30°C (29°C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 21.7 83% 150 19.7 78% 150 18.6
2600 21.7 79% 146 18.8 75% 146 17.8
2500 21.7 75% 140 17.7 71% 140 16.8
2500 20.7 70% 133 16.7 66% 133 15.8
2500 19.7 66% 126 15.6 62% 126 14.8
2500 18.7 61% 117 14.5 58% 117 13.8
2500 17.7 57% 108 13.5 54% 108 12.8
10,000 Feet Pressure Altitude
ISA -30°C (-35°C) ISA (-5°C) ISA + 30°C (25°C)
RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH
2700 20.0 77% 144 18.2 73% 144 17.3
2600 20.0 71% 136 17.0 68% 136 16.1
2500 20.0 67% 129 16.0 64% 129 15.1
2500 19.0 63% 120 14.9 59% 120 14.1
2500 18.0 58% 111 13.8 55% 111 13.1
2500 17.0 54% 100 12.8 51% 100 12.1
Revision 02: 11-17-09
30 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Range / Endurance Profile with Ice Accumulation
• Note •
Range is decreased by a approximately 10% with ice accretion on the aircraft.
　
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