Manual Extension - Beechcraft Baron G58 Pilot Operating Handbook

Section 7
Systems Description
The switches which activate the warning
horn and [GEAR UP] Warning Alert are
operated by the throttles, thus the horn and
[GEAR UP] Warning Alert will always acti-
vate at the same throttle position. The
resultant manifold pressure is dependent
on altitude and RPM.

MANUAL EXTENSION

The landing gear can be manually extended, but not retracted,
by operating the handcrank at the rear of the pilot's seat. Make
certain that the landing gear handle is in the down position and
pull the landing gear MOTOR circuit breaker before manually
extending the gear. When the electrical system is operative,
the landing gear may be checked for full down with the gear
position lights, provided the landing gear RELAY circuit
breaker is engaged. After the landing gear is down, disengage
the handcrank. For electrical retraction of the landing gear
after a practice manual extension use the procedures outlined
in Section 3A, ABNORMAL PROCEDURES.
If the landing gear was extended for emergency reasons, do
not move any landing gear controls or reset any switches or
circuit breakers until the airplane is on the ground and the mal-
function has been determined and corrected, to prevent a gear
retraction on the ground. These procedures are outlined in
Section 3A, ABNORMAL PROCEDURES.
7-18
NOTE
Model G58
May, 2015