Cirrus SR22T, Pilot Operating Handbook

Page: 175 / 506

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-17 P/N 13772-005 5-17
Takeoff Climb Gradient
• Note •
Climb Gradient values 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 the coldest (left-most)
data shown.
For operation in air warmer than this table provides, use extreme caution.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps .................................................................................................................50%
• Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~°C
-20 0 20 40 50 ISA
3600
SL
91 1020 879 752 634 579 782
2000
91 958 823 701 589 537 755
4000
91 898 770 654 547 496 728
6000
91 841 719 608 506 458 702
8000
91 787 671 565 468 422 676
10000
91 735 625 524 431 387 651
2900
SL
94 1303 1148 1002 864 797 1038
2000
94 1251 1097 952 815 750 1016
4000
93 1196 1043 900 765 701 991
6000
93 1137 986 845 713 650 964
8000
92 1077 928 790 660 599 935
10000
92 1015 869 733 607 546 904
Original Issue