Cirrus SR22T User Manual

3A-18 P/N 13772-005
Section 3A Cirrus Design
Abnormal Procedures SR22T
Pitot Heat Current Sensor Annunciation
PITOT HEAT FAIL Caution
1. Pitot Heat Circuit Breaker....................................................CYCLE
2. Pitot Heat .............................................................CYCLE OFF, ON
If inadvertent icing encountered, perform Inadvertent Icing
Encounter Checklist and:
a. Airspeed .......................EXPECT NO RELIABLE INDICATION
b. Exit icing conditions using attitude, altitude, and power
instruments.
Amplification
Pitot heat failure. Displayed when Pitot heat switch is ON and Pitot
heat current is not detected.
Pitot Heat Required Annunciation
PITOT HEAT REQUIRED Caution
1. Pitot Heat .................................................................................. ON
Amplification
Displayed 20 seconds after system detects OAT is less than 41°F
(5°C) and Pitot Heat Switch is OFF.
PITOT HEAT FAIL
PITOT HEAT REQD
Original Issue

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