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• Power................................................................................................................. Idle
• Bank Angle .....................................................................................................Noted
Weight
LB
Bank
Angle
Deg
STALL SPEEDS
Flaps 0%
Full Up Flaps 50%
Flaps 100%
Full Down
KIAS KCAS KIAS KCAS KIAS KCAS
3400
Most
FWD
CG
0 73 70 66 64 62 60
15 74 71 67 65 64 61
30 76 75 71 69 66 64
45 83 83 77 76 72 71
60 99 99 90 90 84 84
3400
Most
AFT
CG
0 72 69 65 63 60 58
15 73 70 66 64 61 59
30 76 74 69 67 63 62
45 82 82 76 75 69 69
60 98 98 89 89 82 82
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-11
Wind Components
• Note •
The max demonstrated crosswind is 20 knots. Value not considered limiting.
Example:
• Runway Heading................................................................................................ 10°
• Wind Direction.................................................................................................... 60°
• Wind Velocity..............................................................................................15 Knots
10°
Tailwind Headwind
0°
ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
140° 130° 120°
150°
160°
170°
180°
VELOCITY ~ KNOTS WIND
40
10 20 30 40
WIND COMPONENTS ~ KNOTS CROSSWIND COMPONENT ~
KNOTS
-20
-10
0
10
20
40
30
SR22_FM05_1014
10
20
30
50
March 2010
5-12 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Takeoff Distance
• Note •
The following factors are to be applied to the computed takeoff distance for
the noted condition:
• Headwind - Subtract 10% from computed distance for each 12 knots headwind.
• Tailwind - Add 10% for each 2 knots tailwind up to 10 knots.
• Grass Runway, Dry - Add 20% to ground roll distance.
• Grass Runway, Wet - Add 30% to ground roll distance.
• Sloped Runway - Increase table distances by 22% of the ground roll distance at Sea
Level, 30% of the ground roll distance at 5000 ft, 43% of the ground roll distance at
10,000 ft for each 1% of upslope. Decrease table distances by 7% of the ground roll
distance at Sea Level, 10% of the ground roll distance at 5000 ft, and 14% of the
ground roll distance at 10,000 ft for each 1% of downslope.
• Note •
The above corrections for runway slope are required to be included herein.
These corrections should be used with caution since published runway slope
data is usually the net slope from one end of the runway to the other. Many
runways will have portions of their length at greater or lesser slopes than the
published slope, lengthening (or shortening) takeoff ground roll estimated
from the table.
• If brakes are not held while applying power, distances apply from point where full
throttle and mixture setting is complete.
• For operation in outside air temperatures colder than this table provides, use coldest
data shown.
• For operation in outside air temperatures warmer than this table provides, use
extreme caution.
• Aircraft with optional Air Conditioning System - Add 100 feet to ground roll and 150
feet to distance over 50 foot obstacle.
Conditions:
• Winds................................................................................................................Zero
• Runway.........................................................................................Dry, Level, Paved
• Flaps................................................................................................................. 50%
• Power.................................................................................................... Full Throttle
• Mixture............................................................................................ Set per Placard
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-13
Takeoff Distance - 3400 LB
Weight: 3400 LB
Speed at Liftoff: 73 KIAS
Speed over 50 Ft. Obstacle: 78 KIAS
Flaps: 50%
Power: Takeoff
Runway: Dry, Paved, Level
Headwind: Subtract 10% for each 12
　
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