Takeoff Climb Gradient - Cirrus SR22 Pilot Operating Handbook

Cirrus Design
SR22

Takeoff Climb Gradient

Conditions:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................ Set per Placard
• Flaps .................................................................................................................50%
• Airspeed .....................................................................................Best Rate of Climb
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.
Weight Press
Altitude
LB FT
SL
2000
4000
3400
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
P/N 13772-001
Revision A10
• Note •
CLIMB GRADIENT ~ Feet per Nautical Mile
Climb
Speed
KIAS
-20
91
939
90
834
89 734
88
638
88
546
87 458
91
1172
90
1049
89
931
88 818
88
711
87
608
Figure 5-10
Temperature ~°C
0 20
896 853
793 752
694 654
600 561
509 472
422 387
1122 1070
1000 950
884 836
773 727
667 623
566 524
Section 5
Performance Data
40 ISA
811 864
711 770
615 680
524 594
436 510
353 431
1019 1083
902 972
790 867
683 766
581 669
484 576
5-15