Cirrus SR22T User Manual

P/N 13772-151 13 of 52
Cirrus Design Section 9
SR22T Supplements
4. ICE PROTECT Mode Switch ................................................. HIGH
If warning annunciation extinguishes:
a. Anti-Ice System ....................................................... MONITOR
If warning annunciation does not extinguishes or intermittent:
a. PUMP BKUP Switch............................................................ON
b. Icing Conditions.................................................. AVOID / EXIT
Lift Transducer Overheat Warning
PFD Alerts Window: “AOA probe is overheated”
• Note •
Operation of Pitot Heat on hot days may annunciate the AOA
OVERHEAT Warning when flying at slow speeds. When air
temperatures are greater than 41°F (5°C), operation of Pitot
Heat is at discretion of the pilot. If overheat warning is
annunciated, Pitot Heat should remain OFF.
1. PITOT HEAT Switch.................................................................OFF
2. Icing Conditions .......................................................... AVOID/EXIT
Tank Control Failure Warning
PFD Alerts Window: “Tank valves cannot be controlled (closed) (TKS)”
Tank selection is inoperative and both left and right are open, typical
with GIA failure.
1. Icing Conditions ........................................................ AVOID / EXIT
AOA OVERHEAT
ANTI ICE CTL
Original Issue: 02-01-13

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots