Turbine Inlet Temperature (Tit) Indicator Failure; Electrical Failures - Piper Malibu PA-46-310P Pilot Operating Handbook

SECTION 3
EMERG PROCEDURES
PIPER AIRCRAFf CORPORATION
PA-46-310P, MALIBU
filGH CYLINDER HEAD TEMPERATURE
Power .......................................................................................................... reduce
Mixture ...................................................................................... enrich if practical
Land at nearest airport and investigate problem.
TURBINE INLET TEMPERATURE (TIT) INDICATOR FAILURE
CAUTION
Aircraft POH range and endurance data
presented in Section 5 will no longer be
applicable. Less range/endurance will result due
to higher fuel flow/fuel consumption.
If
failure occurs during takeoff, climb, descent, or landing:
Mixture ............................................................................................. FULL RICH
If
failure occurs after setting cruise power:
Mixture ............................................................... 6 GPH fuel flow above value in
section 5 Power Setting Table
Cylinder Head and Oil Temperatures ................................................. MONITOR
NOTE
Repair TIT indicator as soon as possible.
ELECTRICAL FAILURES
CAUTION
The alternator output circuit breakers should
never be opened manually when the alternators
are functioning properly, as voltage regulator
damage may occur.
ALTERNATOR annunciator light illuminated
Ammeter ........................................................................................ check to verify
inop. alt.
Reduce electrical loads to minimum
ALTNR circuit breakers ............................................................... check and reset
as required
If
ammeter shows zero
ALTR switch(es) ...................................................................... OFF for 1 second,
REPORT: VB-1200
3-6
then ON
ISSUED: JANUARY 11, 1984
REVISED: MARCH 19, 1999