Cirrus SR22T User Manual

Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-005 3-23P/N 13772-005 3-23
High Cylinder Head Temperature
CHT Caution and Warning
On-Ground
1. Power Lever .....................................................................REDUCE
2. Annunciations and Engine Temperatures ...................... MONITOR
If Caution or Warning annunciation is still illuminated:
3. Power Lever ................................................MINIMUM REQUIRED
4. Flight ......................................................................... PROHIBITED
In-Flight
1. Power Lever .....................................................................REDUCE
2. Mixture ..................................ADJUST fuel flow to top of green arc
3. Airspeed .......................................................................INCREASE
4. Annunciations and Engine Temperatures ...................... MONITOR
If Caution or Warning annunciation is still illuminated:
5. Power Lever ............................................... MINIMUM REQUIRED
6. Engine Instruments ....................................................... MONITOR
If Caution annunciation only remains illuminated:
a. Land as soon as practical.
If Warning annunciation remains illuminated:
a. Land as soon as possible.
CHT
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