Cirrus Design Section 5
SR22 Performance Data
P/N 13772-004 5-17P/N 13772-004 5-17
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:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................Set per Placard
• 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 97 888 822 760 702 674
775
2000 95 777 713 654 599 573
680
4000 94 669 608 552 499 474 588
6000 92 564 507 453 403 379
498
8000 90 463 408 357 310 287
411
10000 89 365 313 264 219 198 325
2900
SL 91 1172 1122 1070 1019 994
1083
2000 90 1049 1000 950 902 878
972
4000 89 931 884 836 790 767 867
6000 88 818 773 727 683 662
766
8000 88 711 667 623 581 561
669
10000 87 608 566 524 484 465 576
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