Piper SARATOGA II HP PA-32R-301 Pilot Operating Handbook page 436

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PA-32R-301, SARATOGA II HP
SECTION9
SUPPLEMENT 23
SECTION 3 - EMERGENCY PROCEDURES (continued)
Complete Electrical Failure
Standby Attitude Gyro .......................... SELECT Standby (STBY) power button
CAUTION
The STBY PWR annunciator will rapidly flash for
approximately one minute when aircraft power is lost.
STBY PWR must be selected, otherwise the gyro will auto
shutdown after approximately one minute.
Standby Attitude Gyro .............................................................. VERIFY ON and
flag is pulled on gyro
Maintain aircraft control with reference to the standby airspeed, altimeter, and
attitude gyro indicators.
Battery Switch ................................................................................................ OFF
Ground Clearance Switch
(if
installed) .......................................................... ON
Land as soon as possible.
WARNING
Compass error may exceed 10 degrees with alternator
inoperative.
NOTE
Turning ON the ground clearance switch will activate the
No. 1 nav/com/GPS radio.
NOTE
If
the battery is depleted, the landing gear must be lowered
using the emergency extension procedure. The gear position
lights will be inoperative. The flaps will also be inoperative
and a flaps up landing will be required.
ISSUED: JUNE 30,1997
REVISED: OCTOBER 17,2005
REPORT: VB-1669
17 of 34,
9-193

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