SOLOY TURBINE PAC
SECTION 7
POHS CESSNA T206H/206H
AIRPLANE & SYSTEMS
DESCRIPTION
7-19
F.A.A. Approved
November 14, 2014
FUEL RETURN SYSTEM
– Deleted
FUEL VENTING
-- No Change
FUEL SELECTOR VALVE
-- No Change
FUEL DRAIN VALVES
-- No Change
BRAKE SYSTEM
– No Change
ELECTRICAL SYSTEM
Electrical power for the aircraft is supplied by a 28 volt direct current
negative ground electrical system (see Figure 7-4). A single 19 amp
hour, 24 volt lead acid battery, or an optional 25 amp hour, 24V lead
acid battery, supplies power for starting and furnishes a reserve source
of power in the event of a generator system failure. An engine driven
starter/generator, controlled by a solid state generator control unit,
provides power for the aircraft electrical system and charges the
battery during operation. An APU plug is installed to permit an external
power source to supplement the battery system for starting and ground
operation.
CAUTION
PRIOR TO TURNING THE BATTERY SWITCH
ON OR OFF, STARTING THE ENGINE, OR
APPLYING AN EXTERNAL POWER SOURCE,
THE AVIONICS POWER SWITCH, LABELED
AVIONICS POWER, SHOULD BE TURNED OFF
TO PREVENT ANY HARMFUL TRANSIENT
VOLTAGE FROM DAMAGING THE AVIONICS
EQUIPMENT.
ANNUNCIATOR PANELS
In addition to the existing Cessna annunciator panel there is the
turbine installation related annunciator panel located on the right
hand instrument panel. Both panels provide caution (amber) and
warning (red) messages for selected portions of the airframe
systems.
The original annunciator panel located in the upper center panel
is retained with its original functions. This annunciator is
designed to flash messages for approximately 10 seconds to gain
the attention of the pilot before changing to steady on. The
annunciator cannot be turned off by the pilot.
UNCONTROLLED
COPY
