Electrical Overload; Spin Recovery - Piper WARRIOR III PA-28-161 Pilot Operating Handbook

SECTION 3
EMERGENCY PROCEDURES
ELECTRICAL OVERLOAD (Alternator over 20 amps above known
electrical load)
ALT switch .....................................................................................................ON
Battery Master switch ....................................................................................OFF
If alternator loads are reduced:
Electrical load .....................................................................Reduce to Minimum
Land as soon as practical.
Due to increased system voltage and radio
frequency noise, operation with ALT switch ON
and BATT switch OFF should be made only
when required by an electrical system failure.
If alternator loads are not reduced:
ALT switch ....................................................................................................OFF
BATT switch ......................................................................................As required
Land as soon as possible. Anticipate complete electrical failure.

SPIN RECOVERY

Rudder...........................................................................................full opposite to
Control wheel...........................................................................full forward while
Throttle............................................................................................................idle
Rudder.....................................................................neutral (when rotation stops)
Control wheel ..................................................................as required to smoothly
REPORT: VB-1565
3-6
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR III
NOTE
direction of rotation
neutralizing ailerons
regain level flight attitude
ISSUED: JULY 1, 1994