Sharp R-360ES Especificaciones descargar pdf (Pagina 55)

P/N 13999-002 Info Manual 3-13

Cirrus Design Section 3

SR20 Emergency Procedures

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 – Refer to Low Oil Pressure procedure 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.

(Continued on following page)

September 2011

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Sharp R-360ES Especificaciones Pagina 55