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• 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 101 1428 1414 1392 1366 1398
2000 100 1311 1292 1267 1238 1279
4000 99 1193 1170 1141 1108 1160
6000 98 1074 1046 1013 977 1041
8000 97 953 921 884 845 922
10000 96 830 794 754 712 803
12000 95 706 666 623 577 684
14000 94 581 537 490 441 565
16000 93 454 406 355 303 446
2900
SL 101 1761 1748 1726 1698 1732
2000 100 1629 1610 1584 1552 1596
4000 99 1494 1471 1441 1405 1461
6000 98 1359 1331 1296 1257 1326
8000 97 1222 1189 1151 1108 1191
10000 95 1084 1046 1004 958 1056
12000 95 945 902 855 806 921
14000 93 804 757 706 653 787
16000 92 662 610 556 499 653
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-19
Enroute Rate of Climb Vs Density Altitude
Conditions:
• Power ....................................................................................................Full Throttle
• Flaps .......................................................................................................... 0% (UP)
• Airspeed.....................................................................................Best Rate of Climb
1,000
2,000
3,000
4,000
5,000
6,000
7,000
8,000
9,000
10,000
11,000
12,000
13,000
14,000
15,000
16,000
17,000
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
3400 LB
2900 LB
Rate of Climb ~ Feet Per Minute Density Altitude ~
Feet
March 2010
5-20 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Time, Fuel and Distance to Climb
• Note •
Taxi Fuel - Add 1.5 gallon for start, taxi, and takeoff.
Temperature - Add 10% to computed values for each 10º C above standard.
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.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture...............................................................................Per Schedule, Section 4
• Fuel Density...........................................................................................6.0 LB/GAL
• Weight ........................................................................................................3400 LB
• Winds................................................................................................................Zero
• Climb Airspeed ...............................................................................................Noted
Press
Alt
FT
OAT
(ISA)
°C
Climb
Speed
KIAS
Rate Of
Climb
FPM
TIME, FUEL, DISTANCE ~ From Sea Level
Time
Minutes
Fuel
U.S. Gal
Distance
NM
SL 15 101 1398 0.0 0.0 0.0
1000 13 100 1339 0.7 0.3 1.0
2000 11 100 1279 1.5 0.7 2.5
3000 9 99 1220 2.5 1.0 4.0
4000 7 99 1160 3.0 1.3 5.5
5000 5 97 1101 4.0 1.7 7.0
6000 3 98 1041 5.0 2.0 8.5
7000 1 96 982 6.0 2.4 10.5
8000 -1 97 922 7.0 2.7 12.0
9000 -3 95 863 8.0 3.1 14.5
10000 -5 95 803 9.5 3.5 16.5
11000 -7 94 744 10.5 3.9 19.0
12000 -9 95 684 12.0 4.4 21.5
13000 -11 93 625 13.5 4.8 24.5
14000 -13 93 565 15.0 5.3 28.0
15000 -15 92 506 17.0 5.8 31.5
16000 -17 92 446 19.0 6.4 35.5
17000 -19 91 387 21.5 7.1 40.0
17500 -20 91 357 24.0 7.8 45.5
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-21
Cruise Performance
• Note •
Subtract 10 KTAS if nose wheel pant and fairing removed. Lower KTAS by
10% if nose and main wheel pants & fairings are removed.
Aircraft with optional Air Conditioning System - Cruise performance is
reduced by 2 knots. For maximum performance, the air-conditioner should be
off.
Shaded data cells: Cruise Power above 85% not recommended.
Conditions:
• Cruise Weight............................................................................................. 2900 LB
　
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