Systems Description
Section 7
Model G58
7-19
BRAKES
The brakes on the main landing gear wheels are operated by
applying toe pressure to the top of the rudder pedals.
The parking brake control is located on the pilot’s subpanel just
left of the elevator trim control. To set the parking brakes, pull
the control out and pump each toe pedal until solid resistance
is felt. Push the control in to release the brakes.
The parking brake should be left off and
wheel chocks installed if the airplane is to
be left unattended. Changes in ambient
temperature can cause the brakes to
release or exert excessive pressures.
The brake hydraulic fluid reservoir is accessible through the
nose baggage door. Fluid level is checked with the dipstick
attached to the reservoir cap. The brakes require no adjust-
ments, since the pistons move outward to compensate for lin-
ing wear.
BAGGAGE COMPARTMENTS
AFT BAGGAGE COMPARTMENT
The aft baggage compartment is accessible through the utility
doors on the right side of the fuselage. This area extends aft of
the pilot’s seats to the rear bulkhead. Because of structural lim-
itations, this area is divided into three sub-compartments, each
having a different weight limitation. Loading within the baggage
compartment must be in accordance with the data in Section 6,
WEIGHT AND BALANCE/EQUIPMENT LIST. All baggage
must be secured with the approved cargo retention systems.
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