SOLOY TURBINE PAC
SECTION 7
POHS CESSNA U/TU 206G
AIRPLANE & SYSTEMS
DESCRIPTION
7-28
F.A.A. Approved
October 4, 2005
CIRCUIT BREAKERS AND FUSES
The circuit breakers and fuses remains the same with the
following exceptions:
The APU circuit fuse and clock circuit fuse are mounted adjacent
to the electrical component housing on the left side of the firewall.
The three circuit breakers added during the turbine conversion
(auto-feather and annunciator lights, generator field, and engine
start) can be pulled off to disable the applicable circuit(s). These
additional circuit breakers are mounted on the lower left side of
the instrument panel.
GROUND SERVICE PLUG RECEPTACLES
– No Change
LIGHTING SYSTEMS
– No Change
CABIN HEATING, VENTILATING AND DEFROSTING
SYSTEM
– No Change except No Heater Installed.
PITOT STATIC SYSTEM AND INSTRUMENTS
–
No
Change.
AIRSPEED INDICATOR
The airspeed indicator is calibrated in knots. Limitation and range
markings include the white arc (40 to 96 knots), with a step at (49
knots), and a red line (149 knots).
RATE-OF-CLIMB INDICATOR
– No Change
ALTIMETER
– No Change
VACUUM SYSTEM AND INSTRUMENTS
– No Change
OUTSIDE AIR TEMPERATURE (OAT) GAUGE
– No
Change
UNCONTROLLED
COPY
