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SECTION 3
EMERG PROCEDURES
3.19 LOSS OF FUEL FLOW (3.3h) (Continued)
If power is restored, turn OFF the emergency (EMERG) fuel pump (except
in the case of an engine driven fuel pump failure). Adjust the mixture control
as necessary.
If power is not restored, turn the emergency (EMERG) fuel pump and
the fuel selector OFF, and proceed with Power Off Landing procedure (refer
to paragraph 3.13).
3.21 ENGINE DRIVEN FUEL PUMP FAILURE (FUEL PRESS light il-
luminated - annunciator panel) (3.3i)
If an engine driven fuel pump failure is indicated, retard the throttle and
turn the emergency (EMERG) fuel pump ON. The throttle and mixture
should then be reset as required. A landing should be made at the nearest
appropriate airport as soon as possible and the cause of the failure
investigated.
If normal engine operation and fuel flow are
not reestablished, the emergency (EMERG)
fuel pump should be turned OFF. The lack of a
fuel flow indication could indicate a leak in the
fuel system. If fuel system leak is verified,
switch fuel selector to OFF.
3.23 HIGH OIL TEMPERATURE (3.3j)
An abnormally high oil temperature indication may be caused by a low
oil level, an obstruction in the oil cooler, damaged or improper baffle seals, a
defective gauge, or other causes. Reduce power and/or enrich the mixture,
and increase airspeed if practical. If condition is not corrected, land as soon
as practical at an appropriate airport and have the cause investigated.
A steady rapid rise in oil temperature is a sign of trouble. Land at the
nearest airport and let a mechanic investigate the problem. Watch the oil
pressure gauge for an accompanying loss of pressure.
3.24 TURBINE INLET TEMP (TIT) INDICATOR FAILURE (3.3k)
In the event the Turbine Inlet Temperature (TIT) indicator or sensor fails
during flight, continued flight is possible using conservative mixture/TIT
settings. If TIT failure occurs during takeoff, climb, descent, or landing,
maintain a full rich mixture to assure adequate fuel flow for engine cooling.
During cruise climb operations, a fuel flow of 32 gph may be used.
REPORT: VB-1710
3-28
CAUTION
ISSUED: FEBRUARY 23, 1999
REVISED: SEPTEMBER 10, 2001
PA-46-350P, MALIBU
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