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Original: 03-27-07
13772-130 35 of 58
Cirrus Design Section 9
SR22 Supplements
Balked Landing Climb Gradient
• Note •
• Balked Landing Climb Gradients shown are the gain in altitude for the horizontal
distance traversed expressed as Feet per Nautical Mile.
• 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 Best Rate of Climb speeds shown with
flaps down or following the Go-Around / Balked Landing procedure in Section 4.
Conditions: Example:
• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ...................... Set per Placard Weight .................................. 3400 LB
• Flaps ................................ 100% (DN) Pressure Altitude .................. 4000 FT
• Climb Airspeed...........................VREF
Climb Airspeed .....................77 Knots
Rate of Climb....................633 FT/NM
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
Original: 03-27-07
36 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
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: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 20° C
• Mixture.......................Set per Placard Weight...................................3400 LB
• Flaps.................................100% (DN) Pressure Altitude...................4000 FT
• Climb Airspeed .......................... VREF
Climb Airspeed..................... 77 Knots
Rate of Climb ................... 878 FT/NM
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
Original: 03-27-07
13772-130 37 of 58
Cirrus Design Section 9
SR22 Supplements
Landing Distance
Factors:
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.
• Caution •
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
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(147)
