continues to increase, turn battery switch OFF.
Battery switch OFF.
The battery may be turned back ON
only for gear and flap extension and
approach to landing. Battery may be
usable after a 15 20 minute cool
Battery switch (landing gear/flap extension
Avionics Master Power Switch Failure. If
the Avionics Master Power Switch fails to operate in the
ON position, perform the following:
The avionics power relay is normally
hot. Pulling the AVIONICS MASTER
CONTR circuit breaker will remove
power to the relay, thus allowing
electrical power to the associated
9-28. EMERGENCY DESCENT.
The following procedure assumes the structural integrity
of the aircraft and smooth flight conditions. If structural
integrity is in doubt, limit speed as much as possible,
reduce rate of descent if necessary, and avoid high
maneuvering loads. For emergency descent, perform
Power levers IDLE.
Propeller levers HIGH RPM.
Airspeed 178 KIAS maximum.
Windshield defogging may be
9-29. FLIGHT CONTROLS MALFUNCTION.
Use the following procedures, as applicable, for flight
Disconnection. The autopilot can be disengaged by any
of the following methods:
Pressing the DISC TRIM AP YD disconnect
switch (control wheels).
Pressing the AP ENGAGE pushbutton on
the autopilot mode selector control panel.
Pressing the go-around switch (left power
lever), (yaw damper will remain on).
Pulling the AP CONTR and AFCS DIRECT
circuit breakers (overhead control panel).
switch (overhead control panel) to the off position.
Setting aircraft MASTER switch (overhead
control panel) to the OFF position.
Rudder boost operation without a large variation of
power between engines indicates a failure of the
system. Perform the following:
Control wheel disconnect switch Disconnect
and hold (hold to first level).
Rudder boost control switch OFF.
Rudder boost circuit breaker Pull (Provided
that rudder boost does not deactivate).
Control wheel disconnect Release.
Yaw damper Reengage.
Unscheduled Electric Trim. In the event of
Electric trim switch OFF.
Elevator trim circuit breaker Pull.
9-30. LANDING EMERGENCIES.
Structural damage may exist after
landing with brake, tire, or landing
circumstances shall an attempt be
made to inspect the aircraft until
jacks have been installed.
Landing Gear Unsafe Indication.
Landing gear control switch Check DN.
Landing gear control and gear indicator
circuit breakers Check in.