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50 ft 2320 2493 2673 2858 3051 2407
6000 Grnd Roll 1676 1810 1950 2095 2245 1717
50 ft 2564 2755 2953 3159 3371 2622
7000 Grnd Roll 1861 2009 2164 2325 2492 1877
50 ft 2837 3048 3267 3494 3729 2859
8000 Grnd Roll 2068 2233 2405 2584 2770 2054
50 ft 3142 3376 3619 3871 4131 3122
9000 Grnd Roll 2302 2485 2677 2875 3082 2250
50 ft 3485 3744 4014 4293 4581 3412
10000 Grnd Roll 2564 2769 2982 3204 3434 2468
50 ft 3870 4158 4457 4767 5088 3733
Revision 02: 08-26-09
26 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Takeoff Distance - 2900 Lb
WEIGHT = 2900 LB
Speed at Liftoff = 70 KIAS
Speed over 50 Ft Obstacle = 74 KIAS
Flaps - 50% · Takeoff Pwr · Dry Paved
Headwind: Subtract 10% for each 12
knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 ISA
SL Grnd Roll 610 659 710 763 818 684
50 ft 971 1043 1118 1195 1275 1080
1000 Grnd Roll 673 727 783 841 902 743
50 ft 1066 1146 1228 1313 1401 1170
2000 Grnd Roll 743 802 864 929 995 809
50 ft 1173 1260 1351 1444 1541 1269
3000 Grnd Roll 821 887 955 1026 1100 880
50 ft 1292 1388 1487 1590 1697 1378
4000 Grnd Roll 908 981 1057 1135 1217 959
50 ft 1424 1530 1639 1753 1871 1498
5000 Grnd Roll 1006 1086 1170 1257 1348 1046
50 ft 1571 1688 1809 1935 2065 1630
6000 Grnd Roll 1116 1205 1298 1394 1494 1143
50 ft 1736 1865 1999 2138 2281 1775
7000 Grnd Roll 1238 1337 1440 1547 1659 1249
50 ft 1920 2063 2211 2365 2523 1936
8000 Grnd Roll 1376 1486 1601 1720 1843 1367
50 ft 2127 2285 2449 2619 2795 2113
9000 Grnd Roll 1532 1654 1781 1914 2051 1498
50 ft 2359 2534 2716 2904 3099 2309
10000 Grnd Roll 1707 1843 1985 2132 2285 1643
50 ft 2619 2814 3016 3225 3441 2527
Revision 02: 08-26-09
13772-130 27 of 58
Cirrus Design Section 9
SR22 Supplements
Takeoff Climb Gradient
• Note •
• Climb Gradients shown are the gain in altitude for the horizontal distance traversed
expressed as Feet per Nautical Mile.
• 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.
• 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.
Conditions: Example:
• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ...................... Set per Placard Weight .................................. 3400 LB
• Flaps ...........................................50% Pressure Altitude .................. 4000 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................89 Knots
Gradient............................654 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 91 939 896 853 811 864
2000 90 834 793 752 711 770
4000 89 734 694 654 615 680
6000 88 638 600 561 524 594
8000 88 546 509 472 436 510
10000 87 458 422 387 353 431
2900
SL 91 1172 1122 1070 1019 1083
2000 90 1049 1000 950 902 972
4000 89 931 884 836 790 867
6000 88 818 773 727 683 766
8000 88 711 667 623 581 669
10000 87 608 566 524 484 576
Revision 02: 08-26-09
28 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Takeoff Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude for unit time expended
expressed in Feet per Minute.
• 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.
• 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.
Conditions: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 10° C
• Mixture.......................Set per Placard Weight...................................3400 LB
• Flaps........................................... 50% Pressure Altitude...................6000 FT
　
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