Cirrus SR22T User Manual

Cirrus Design Section 4
SR22T Normal Procedures
P/N 13772-005 4-19P/N 13772-005 4-19
HIGH BOOST /PRIME position and reset the mixture as required to
maintain adequate stable fuel flow. Vapor lock is most often indicated
by any or a combination of the following:
•Fluctuations in normal fuel flow possibly coupled with abnormal
engine operation;
•Rising EGTs and TIT coupled with falling fuel flow
•Rising CHTs (late in the process)
After the aircraft is in cruise flight for 30 minutes or more, the fuel
pump should be returned to the BOOST position or OFF, as conditions
permit.
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