Cirrus SR22T User Manual

3-30 P/N 13772-005
Section 3 Cirrus Design
Emergency Procedures SR22T
Propeller Governor Failure
1. Power Lever .... Reduce to minimum necessary for sustained flight
2. Airspeed...................................................... Reduce to 85-90 KIAS
3. Oil Pressure ................................................................... MONITOR
4. Land as soon as possible.
Amplification
An in-flight governor failure will likely result in a large exceedance
(3000 RPM or more), as propeller blade angle will be go to fine pitch.
Failure may evidence of engine oil pressure of volume loss, typically
accompanied by OIL PRESSURE warning.
Propeller becomes a fixed pitch propeller; reducing speed to 85-90
KIAS and using only power necessary for sustained flight at that speed
will minimize the overspeed.
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