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Cirrus SR22T User Manual

Cirrus SR22T
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Cirrus Design Section 9
SR22 / SR22T Supplements
P/N 13772-135 13 of 30
Temporary Interrupt of ESP (Optional)
Although ESP is only provided when AFCS Autopilot is disengaged,
the AFCS and its servos are the source of ESP guidance. When the
AP Disconnect button is pressed and held, the servos will provide no
ESP control force feedback. Upon release of the AP Disconnect
button, ESP will be restored.
1. AP Disconnect ..........PRESS and HOLD until maneuver complete
Section 5 - Performance
• WARNING •
The Autopilot may not be able to maintain all selectable
vertical speeds. Selecting a vertical speed that exceeds the
aircraft’s available performance may cause the aircraft to stall.
If AFCS Underspeed Protection function is not installed, the Autopilot
will disconnect if the Stall Warning System is activated.
Section 6 - Weight & Balance
Refer to Section 6 - Weight and Balance of the basic POH.
Revision 03: 12-14-10

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Cirrus SR22T Specifications

General IconGeneral
ManufacturerCirrus Aircraft
EngineContinental TSIO-550-K
Horsepower315 hp
Max Takeoff Weight3, 600 lbs
Service Ceiling25, 000 ft
Cabin Width49 in
Cabin Height50 in
Seating Capacity4
AvionicsCirrus Perspective+ by Garmin
CategorySingle-engine piston aircraft
PropellerHartzell 3-blade composite
Wingspan38 ft 4 in
Length26 ft
Height8 ft 11 in
Maximum Cruise Speed213 KTAS
Fuel Capacity92 gallons
Stall Speed64 knots
Safety FeaturesCirrus Airframe Parachute System (CAPS)
Cruise Speed183 knots

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