Cirrus SR22T User Manual

Cirrus Design Section 4
SR22T Normal Procedures
P/N 13772-005 4-15P/N 13772-005 4-15
indicate faulty grounding of one side of the ignition system or magneto
timing set in advance of the specified setting.
Maximum Power Fuel Flow
For maximum power operations (Power Lever full forward - 2500 RPM,
36.0 in.Hg manifold pressure) fuel flow should be in the green arc.
For any power setting greater than 30.5 in.Hg (cruise power) fuel flow
is indicated by a dynamically calculated green arc displayed on the
fuel gage. Fuel flow should be maintained within this arc by use of the
mixture lever.
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