Cirrus DESIGN SR22T User Manual

3-28 P/N 13772-003
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 able
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 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