Cirrus SR22T, Pilot Operating Handbook

Page: 189 / 506

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-31 P/N 13772-005 5-31
Balked Landing 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 ...................................................................................................... 100% (DN)
• Climb Airspeed.................................................................................................V
REF
Weight
LB
Press Alt
FT
Climb
Speed
(V
REF
)
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile
Temperature ~°C
-20 0 20 40 50 ISA
3600
SL
79 1111 921 751 596 524 792
2000
79 1015 835 674 528 459 744
4000
79 924 754 602 463 398 699
6000
79 838 678 534 402 341 655
8000
79 758 606 470 346 287 613
10000
79 682 539 410 293 237 573
2900
SL
79 1519 1274 1057 861 771 1109
2000
79 1394 1164 959 775 689 1049
4000
79 1277 1061 868 694 612 991
6000
79 1168 965 783 618 541 936
8000
79 1066 874 703 547 474 883
10000
79 970 790 628 481 412 832
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