Cirrus DESIGN SR22T User Manual

Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-003 3-23
2. A significant leak in the exhaust system.
a. An exhaust leak may present a possible fire hazard. Reducing
power and adjusting the mixture as described reduces the
possibility of an engine compartment fire.
3. A loss of oil pressure to the wastegate actuator due to a general
loss of engine oil pressure.
a. Potentially caused by a failed oil line, oil line fitting, or oil pump
b. Failure to maintain normal full manifold pressure at altitude
may be an early indication of an oil leak and impending further
loss of oil pressure.
c. Monitor for reduction in oil pressure; if observed continue for
diversion airfield, but prepare for forced landing.
4. A failure of an internal component in the turbocharger.
a. If the pilot experiences a sudden loss of manifold pressure
and later observes declining oil pressure, it is may be due to a
failure of an internal turbocharger component. If there is a loss
of oil pressure due to a failure of the turbocharger, engine oil
may be vented through the tail pipe overboard.
b. Monitor for reduction in oil pressure; if observed continue for
diversion airfield, but prepare for forced landing.
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