3-20 P/N 11934-004
Section 3 Cirrus Design
Emergency Procedures SR20
Engine Partial Power Loss
Indications of a partial power loss include fluctuating RPM, reduced or
fluctuating manifold pressure, low oil pressure, high oil temperature,
and a rough-sounding or rough-running engine. Mild engine
roughness in flight may be caused by one or more spark plugs
becoming fouled. A sudden engine roughness or misfiring is usually
evidence of a magneto malfunction.
• Note •
Low oil pressure may be indicative of an imminent engine
failure. See Oil Pressure Out of Range - OIL PRESS Warning
in this section for special procedures with low oil pressure.
• Note •
A damaged (out-of-balance) propeller may cause extremely
rough operation. If an out-of-balance propeller is suspected,
immediately shut down engine and perform Forced Landing
checklist.
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.
If the power loss is due to a fuel leak in the injector system, fuel
sprayed over the engine may be cooled by the slipstream airflow which
may prevent a fire at altitude. However, as the Power Lever is reduced
during descent and approach to landing the cooling air may not be
sufficient to prevent an engine fire.
• WARNING •
If there is a strong smell of fuel in the cockpit, divert to the
nearest suitable landing field. Fly a forced landing pattern and
shut down the engine fuel supply once a safe landing is
assured.
The following procedure provides guidance to isolate and correct
some of the conditions contributing to a rough running engine or a
partial power loss:
Original Issue
To Next Page
Loading...
