Takeoff Climb Gradient - Cirrus SR22 Pilot Operating Handbook

S 5: P
ECTION ERFORMANCE
T D
AKEOFF ISTANCE

Takeoff Climb Gradient

Conditions:
• Power ........................................................................................Full Throttle
• Mixture.....................................................Set to very top of GREEN ARC
• 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
Cruise climbs or short duration climbs are permissible at best
power as long as altitudes and temperatures remain within those
For operation in air colder than this table provides, use coldest
data shown. For operation in air warmer than this table provides,
Weight Press Alt
LB FT
3600 SL
2000
4000
6000
8000
10000
5-22
D
ATA
• N
specified in the table.
use caution.
CLIMB GRADIENT - Feet per Nautical Mile
Climb
Speed
KIAS -20
97 888
95 777
94 669
92 564
90 463
89 365
•
OTE
climbs.
TEMPERATURE ~°C
0 20
822 760
713 654
608 552
507 453
408 357
313 264
C
IRRUS
40 50
702 674
599 573
499 474
403 379
310 287
219 198
P/N 13772-006
Reissue A
D
ESIGN
SR22
ISA
775
680
588
498
411
325