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Revision 02: 11-17-09
24 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
After Landing and Shutdown
1. PITOT HEAT Switch .................................................................OFF
2. ICE PROTECT System Switch.................................................OFF
3. PUMP BKUP Switch ................................................................OFF
4. Ice-Inspection Lights ................................................................OFF
• Note •
When the Anti-Ice System has been used, avoid touching the
airframe structure or windshield as they will be partially
covered with anti-ice fluid. Clean the anti-ice fluid from the
windshield and the porous panels as described in Section 8,
Handling, Service, and Maintenance.
Revision 02: 11-17-09
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Cirrus Design Section 9
SR22 Supplements
Section 5 - Performance
Airplane performance and stall speeds without ice accumulation are
essentially unchanged with the installation of the Ice Protection
System.
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
• Note •
Altitude loss during wings level stall may be 600 feet or more.
KIAS values may not be accurate at stall.
Conditions:
• Weight ........................................................................................................ 3400 LB
• CG..................................................................................................................Noted
• Power ................................................................................................................. Idle
• Bank Angle..................................................................................................... Noted
Weight
LB
Bank
Angle
Deg
STALL SPEEDS
Flaps 0%
Full Up Flaps 50%
Flaps 100%
Full Down
KIAS KCAS KIAS KCAS KIAS KCAS
3400
Most
FWD
CG
0 75 73 70 68 66 64
15 76 74 72 69 65 65
30 80 79 75 73 69 69
45 88 87 81 81 76 76
60 104 104 97 97 90 90
3400
Most
AFT
CG
0 73 71 69 67 65 63
15 74 72 71 68 64 64
30 77 76 74 72 68 68
45 85 84 80 80 75 75
60 100 100 95 95 89 89
Revision 02: 11-17-09
26 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Enroute Climb Gradient with Ice Accumulation
• 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 top of green arc 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.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture............................................................................................ Set Per Placard
• Flaps...........................................................................................................0% (UP)
• Airspeed .................................................................................... Best Rate of Climb
Negative climb data shown in heavier table borders.
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet / Nautical Mile
Temperature ~°C
-20 -10 0 5 ISA
3400
SL 101 517 498 480 470 452
2000 100 423 405 387 378 367
4000 98 332 315 298 289 286
6000 97 245 229 213 204 207
8000 96 162 146 131 123 132
10000 95 82 67 52 45 60
12000 95 6 -9 -22 -29 -10
14000 95 -67 -79 -92 -98 -75
16000 95 -137 -145 -157 -163 -137
2900
SL 101 663 641 619 608 585
2000 100 553 532 510 500 487
4000 98 447 427 407 397 393
6000 97 346 327 308 299 302
8000 96 250 232 213 204 215
10000 95 158 140 123 114 131
12000 95 68 52 37 28 50
14000 95 -15 -29 -45 -52 -25
16000 95 -92 -107 -120 -127 -97
Revision 02: 11-17-09
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Cirrus Design Section 9
SR22 Supplements
　
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