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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
Original: 03-27-07
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 75.2 711 770
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
Original: 03-27-07
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
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 88 Knots
Rate of Climb .......................948 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 91 1326 1317 1300 1277 1304
2000 90 1214 1200 1179 1153 1189
4000 89 1100 1082 1057 1028 1074
6000 88 985 962 934 901 958
8000 88 869 842 809 774 843
10000 87 851 719 683 644 727
2900
SL 91 1646 1638 1621 1598 1626
2000 90 1518 1505 1484 1457 1494
4000 89 1389 1371 1346 1316 1363
6000 88 1259 1236 1207 1172 1232
8000 88 1128 1100 1066 1028 1101
10000 87 995 962 924 883 971
Original: 03-27-07
13772-130 29 of 58
Cirrus Design Section 9
SR22 Supplements
Enroute 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
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(144)
