Piper ARCHER III - Electrical Overload; Spin Recovery

SECTION 3
EMERGENCY PROCEDURES PA-28-181, ARCHER III
SECTION 3
EMERGENCY PROCEDURES PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
3-6
REPORT: VB-1611 ISSUED: JULY 12, 1995
3-6
ELECTRICAL OVERLOAD (Alternator over 20 amps above known
electrical load)
ALT switch ......................................................................................................ON
BAT switch.....................................................................................................OFF
If alternator loads are reduced:
Electrical load ......................................................................Reduce to Minimum
Land as soon as practical.
NOTE
Due to increased system voltage and radio
frequency noise, operation with ALT switch
ON and BAT switch OFF should be made
only when required by an electrical system
failure.
If alternator loads are not reduced:
ALT switch.....................................................................................................OFF
BAT switch .........................................................................................As required
Land as soon as possible. Anticipate complete electrical failure.
SPIN RECOVERY
Rudder...........................................................................................full opposite to
direction of rotation
Control wheel...........................................................................full forward while
neutralizing ailerons
Throttle............................................................................................................idle
Rudder.....................................................................neutral (when rotation stops)
Control wheel ..................................................................as required to smoothly
regain level flight attitude
ELECTRICAL OVERLOAD (Alternator over 20 amps above known
electrical load)
ALT switch ......................................................................................................ON
BAT switch.....................................................................................................OFF
If alternator loads are reduced:
Electrical load ......................................................................Reduce to Minimum
Land as soon as practical.
NOTE
Due to increased system voltage and radio
frequency noise, operation with ALT switch
ON and BAT switch OFF should be made
only when required by an electrical system
failure.
If alternator loads are not reduced:
ALT switch.....................................................................................................OFF
BAT switch .........................................................................................As required
Land as soon as possible. Anticipate complete electrical failure.
SPIN RECOVERY
Rudder...........................................................................................full opposite to
direction of rotation
Control wheel...........................................................................full forward while
neutralizing ailerons
Throttle............................................................................................................idle
Rudder.....................................................................neutral (when rotation stops)
Control wheel ..................................................................as required to smoothly
regain level flight attitude