Cirrus SR22T User Manual

3-28 P/N 13772-005
Section 3 Cirrus Design
Emergency Procedures SR22T
EGT, TIT or CHT Temperature Sensor Failure
1. Similar gages ................................................................. MONITOR
2. Flight ............................................................................ CONTINUE
using remaining gages as representative.
Amplification
Isolated red X presentation of an EGT, TIT or CHT indicates that
sensor has failed. Continued flight is permitted, using the remaining
gages as representative of the failed gage; control airspeed or mixture
in a normal manner to maintain the other cylinders or TIT within their
normal operating ranges.
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