Cirrus DESIGN SR22T User Manual

Cirrus Design Section 4
SR22T Normal Procedures
P/N 13772-003 4-19
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 DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches