Takeoff Climb Gradient - Cirrus SR22 Pilot's Operating Handbook And Flight Manual

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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
3600
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
P/N 13772-004
P/N 13772-004
Original Issue
• Note •
CLIMB GRADIENT ~ Feet per Nautical Mile
Climb
Speed
KIAS
-20
97
888
95
777
94
669
92
564
90
463
89
365
91
1172
90
1049
89
931
88
818
88
711
87
608
Temperature ~°C
0
20
822
760
713
654
608
552
507
453
408
357
313
264
1122
1070
1000
950
884
836
773
727
667
623
566
524
Section 5
Performance Data
40
50
702
674
599
573
499
474
403
379
310
287
219
198
1019
994
902
878
790
767
683
662
581
561
484
465
ISA
775
680
588
498
411
325
1083
972
867
766
669
576
5-17
5-17

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