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Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile Best
Rate
of
Climb
KIAS
Temperature ~°C
-20 0 20 40 ISA
3400
SL 77 834 835 823 803 827 80
2000 77 750 744 728 704 736 80
4000 77 666 654 633 604 648 79
6000 77 581 564 537 504 560 78
8000 77 496 472 440 402 473 77
10000 77 409 379 341 296 387 77
2900
SL 77 1069 1070 1056 1032 1060
2000 77 969 962 942 914 953
4000 77 869 855 829 796 847
6000 77 789 747 716 677 743
8000 77 668 639 602 556 641
10000 77 565 529 484 432 639
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-27
Balked Landing Rate of Climb
• Note •
Balked Landing Rate of Climb values shown are the full flaps change in
altitude for unit time expended expressed in Feet per Minute.
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.
This chart is required data for certification. However, significantly better
performance can be achieved by climbing at the Best Rate of Climb speeds
shown with flaps down or following the Go-Around / Balked Landing
procedure in Section 4.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................Set per Placard
• Flaps ......................................................................................................100% (DN)
• Climb Airspeed............................................................................................... VREF
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB - Feet per Minute Best
Rate
of
Climb
KIAS
Temperature ~°C
-20 0 20 40 ISA
3400
SL 77 996 1035 1057 1067 1053 80
2000 77 930 959 972 971 966 80
4000 77 858 876 878 867 878 79
6000 77 779 784 775 752 784 78
8000 77 691 683 660 623 684 77
10000 77 593 571 532 478 578 77
2900
SL 77 1268 1318 1348 1363 1342
2000 77 1195 1233 1252 1255 1245
4000 77 1115 1140 1146 1137 1144
6000 77 1026 1037 1030 1007 1037
8000 77 927 923 900 861 923
10000 77 817 796 755 696 803
March 2010
5-28 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Landing Distance
• Note •
The following factors are to be applied to the computed landing distance for
the noted condition:
• Headwind - Subtract 10% from table distances for each 13 knots headwind.
• Tailwind - Add 10% to table distances for each 2 knots tailwind up to 10 knots.
• Grass Runway, Dry - Add 20% to ground roll distance.
• Grass Runway, Wet - Add 60% to ground roll distance.
• Sloped Runway - Increase table distances by 27% of the ground roll distance for each
1% of downslope. Decrease table distances by 9% of the ground roll distance for
each 1% of upslope.
• 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) landing ground roll estimated
from the table.
• 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.
Conditions:
• Winds................................................................................................................Zero
• Runway.........................................................................................Dry, Level, Paved
• Flaps............................................................................................................... 100%
• Power.........................................................................................3° Power Approach
to 50 FT obstacle, then reduce power passing the estimated 50 foot point and
smoothly continue power reduction to reach idle just prior to touchdown.
March 2010
Cirrus Design Section 5
SR22 Performance Data
Information Manual 5-29
Landing Distance
WEIGHT: 3400 LB
Speed over 50 Ft Obstacle: 77 KIAS
　
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