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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 90 834 793 752 711
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
Revision 02: 08-26-09
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