Malibu Boats PA-46-310P, Руководство по эксплуатации для пилотов

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SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-46-310P, MALIBU
REPORT: VB-1300 ISSUED: JULY 1, 1986
4-28 REVISED: AUGUST 20, 1993
The engine power setting table defines the cruise power at the desired
mixture setting of 50° lean of peak. Operation at the same manifold pressure
and a richer mixture setting will produce a higher horsepower, increased
engine temperatures and in the case of 75% power will exceed the approved
horsepower for leaning the engine. Do not operate the aircraft in cruise with
a mixture setting other than 50° lean of peak T.I.T.
For maximum service life, cylinder head temperature should be
maintained below 420°F during cruise operation. If cylinder head
temperatures become too high during flight, reduce them by decreasing
power.
Following level-off for cruise, the pressurization system should be
checked.
The pilot should monitor weather conditions while flying, and be alert
for meteorological conditions which might lead to icing. Even aircraft
equipped with a complete deicing option are not approved for flight in heavy
icing, heavy snow, or freezing rain. (See Section 9.) Immediate steps shall be
taken to exit any area where such icing conditions are inadvertently
encountered. Saturated air accelerating through the induction system filter
can form ice although ambient temperatures are above freezing. If induction
system icing is suspected, place the induction air control in the
ALTERNATE position. Alternate air should also be selected before
entering clouds. Manifold pressure may decrease when alternate air is
selected depending on altitude, power setting, and other factors. If ice is
forming on the filter, manifold pressure could continue to deteriorate after
selecting alternate air. When manifold pressure stabilizes reestablish cruise
configuration. The primary filter may retain ice after leaving icing
conditions, making the selection of PRIMARY induction air impractical
until ice melts or sublimates.
During flight, keep account of time and fuel used in connection with
power settings to determine how the fuel flow and fuel quantity gauging
systems are operating.
There are no mechanical uplocks in the landing gear system. In the event
of a hydraulic system malfunction, check valves should prevent the gear from
extending. However, some hydraulic system malfunctions may cause the gear
to free-fall to the gear down position. The true airspeed with gear down is
approximately 70% of the gear retracted airspeed for any given power
setting. Allowances for the reduction in airspeed and range should be made
when planning extended flight between remote airfields or flight over water.
In order to keep the airplane in best lateral trim during cruise flight, the
fuel should be used alternately from each tank at one hour intervals or less.
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-46-310P, MALIBU
REPORT: VB-1300 ISSUED: JULY 1, 1986
4-28 REVISED: AUGUST 20, 1993
The engine power setting table defines the cruise power at the desired
mixture setting of 50° lean of peak. Operation at the same manifold pressure
and a richer mixture setting will produce a higher horsepower, increased
engine temperatures and in the case of 75% power will exceed the approved
horsepower for leaning the engine. Do not operate the aircraft in cruise with
a mixture setting other than 50° lean of peak T.I.T.
For maximum service life, cylinder head temperature should be
maintained below 420°F during cruise operation. If cylinder head
temperatures become too high during flight, reduce them by decreasing
power.
Following level-off for cruise, the pressurization system should be
checked.
The pilot should monitor weather conditions while flying, and be alert
for meteorological conditions which might lead to icing. Even aircraft
equipped with a complete deicing option are not approved for flight in heavy
icing, heavy snow, or freezing rain. (See Section 9.) Immediate steps shall be
taken to exit any area where such icing conditions are inadvertently
encountered. Saturated air accelerating through the induction system filter
can form ice although ambient temperatures are above freezing. If induction
system icing is suspected, place the induction air control in the
ALTERNATE position. Alternate air should also be selected before
entering clouds. Manifold pressure may decrease when alternate air is
selected depending on altitude, power setting, and other factors. If ice is
forming on the filter, manifold pressure could continue to deteriorate after
selecting alternate air. When manifold pressure stabilizes reestablish cruise
configuration. The primary filter may retain ice after leaving icing
conditions, making the selection of PRIMARY induction air impractical
until ice melts or sublimates.
During flight, keep account of time and fuel used in connection with
power settings to determine how the fuel flow and fuel quantity gauging
systems are operating.
There are no mechanical uplocks in the landing gear system. In the event
of a hydraulic system malfunction, check valves should prevent the gear from
extending. However, some hydraulic system malfunctions may cause the gear
to free-fall to the gear down position. The true airspeed with gear down is
approximately 70% of the gear retracted airspeed for any given power
setting. Allowances for the reduction in airspeed and range should be made
when planning extended flight between remote airfields or flight over water.
In order to keep the airplane in best lateral trim during cruise flight, the
fuel should be used alternately from each tank at one hour intervals or less.
FOR REFERENCE ONLY
NOT FOR FLIGHT