Cirrus SR22T User Manual

8 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Section 3 - Emergency Procedures
A failure of the Anti-Ice System is any condition, observed or
suspected, in which the system fails to remove ice from protected
surfaces including the propeller, in addition to any Anti-Ice System
CAS failure annunciations. An unobserved failure may be indicated by
a decrease in airspeed, anomalous handling characteristics, or
airframe vibrations.
• Note •
Significant loss in cruise or climb performance may be an
indication of propeller ice accretions that are not visible to the
naked eye. Operation of the engine at 2500 RPM will help
shed ice in severe icing conditions.
• Caution •
Continuous ice accumulations on protected areas are
abnormal.
• WARNING •
With ice accumulations on the horizontal stabilizer leading
edge, flaps should remain retracted for landing and the
landing speed increased accordingly.
With asymmetrical ice accumulations on large portions of the
wing or horizontal stabilizer, avoid flight at speeds less than 95
KIAS.
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