Cirrus DESIGN SR22T Pilot Operating Handbook page 392

Section 9
Supplements
Section 5 - Performance
Airplane performance and stall speeds without ice accumulation are
essentially unchanged with the installation of the Ice Protection
System. Serials SR22T-0001 and subsequent: Performance of the
airplane with the Teledyne Continental TSIO-550-K turbocharged
engine installed is equal to or better than the performance described in
the following section.
Significant climb and cruise performance degradation, range
reduction, as well as buffet and stall speed increase can be expected if
ice accumulates on the airframe. Residual ice on the protected areas
and ice accumulation on the unprotected areas of the airplane can
cause noticeable performance losses and stall speed increases even
with the Anti-Ice System operating.
Stall Speeds with Ice Accumulation
Conditions:
• Weight ........................................................................................................ 3400 LB
• CG ..................................................................................................................Noted
• Power................................................................................................................. Idle
• Bank Angle .....................................................................................................Noted
Altitude loss during wings level stall may be 600 feet or more.
KIAS values may not be accurate at stall.
Weight Bank
Angle
LB Deg
0
3400
15
Most 30
FWD
45
CG
60
0
3400
15
Most 30
AFT
45
CG
60
26 of 48
• Note •
Flaps 0%
Full Up
KIAS KCAS
75 73
76 74
80 79
88 87
104 104
73 71
74 72
77 76
85 84
100 100
STALL SPEEDS
Flaps 50%
KIAS KCAS
70 68
72 69
75 73
81 81
97 97
69 67
71 68
74 72
80 80
95 95
Revision 04: 12-17-10
Cirrus Design
SR22 / SR22T
Flaps 100%
Full Down
KIAS KCAS
66 64
65 65
69 69
76 76
90 90
65 63
64 64
68 68
75 75
89 89
P/N 13772-134