Cirrus Design Section 5
SR22 Performance Data
P/N 13772-002 5-17P/N 13772-002 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
3400
SL 91 939 896 853 811 790
864
2000 90 834 793 752 711 691
770
4000 89 734 694 654 615 596 680
6000 88 638 600 561 524 506
594
8000 88 546 509 472 436 419
510
10000 87 458 422 387 353 336 431
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
Reissue A
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