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Cirrus DESIGN SR22T User Manual

Cirrus DESIGN SR22T
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Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-003 3-19
Selecting HIGH BOOST/PRIME may clear the problem if vapor in the
injection lines is the problem or if the engine-driven fuel pump has
partially failed. The electric fuel pump will not provide sufficient fuel
pressure to supply the engine if the engine-driven fuel pump
completely fails.
Selecting the opposite fuel tank may resolve the problem if fuel
starvation or contamination in one tank was the problem.
Cycling the ignition switch momentarily from BOTH to L and then to R
may help identify the problem. An obvious power loss in single ignition
operation indicates magneto or spark plug trouble. Lean the mixture to
the recommended cruise setting. If engine does not smooth out in
several minutes, try a richer mixture setting. Return ignition switch to
the BOTH position unless extreme roughness dictates the use of a
single magneto.
If a partial engine failure permits level flight, land at a suitable airfield
as soon as conditions permit. If conditions do not permit safe level
flight, use partial power as necessary to set up a forced landing
pattern over a suitable landing field. Always be prepared for a
complete engine failure and consider CAPS deployment if a suitable
landing site is not available. Refer to Section 10, Safety Information,
for CAPS deployment scenarios and landing considerations.
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Cirrus DESIGN SR22T Specifications

General IconGeneral
ManufacturerCirrus Aircraft
ModelSR22T
Seating Capacity5
EngineContinental TSIO-550-K
Horsepower315 hp
AvionicsCirrus Perspective+ by Garmin
TypeSingle-engine piston aircraft
Maximum Speed213 knots
Cruise Speed183 knots
Service Ceiling25, 000 feet
Maximum Takeoff Weight3, 600 lbs
Wingspan38 feet 4 inches
Length26 ft
Height8 feet 11 inches
Safety FeaturesCirrus Airframe Parachute System (CAPS)
Cabin Width49 inches
Cabin Height50 inches

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