Circuit Breakers And Fuses; Ground Service Plug Receptacles; Lighting Systems; Pitot Static System And Instruments - Cessna U206G STATIONAIR Pilot Operating Handbook

SOLOY TURBINE PAC
POHS CESSNA U/TU 206G

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

CABIN HEATING, VENTILATING AND DEFROSTING
– No Change except No Heater Installed.
SYSTEM
PITOT STATIC SYSTEM AND INSTRUMENTS –
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

OUTSIDE AIR TEMPERATURE (OAT) GAUGE

Change
F.A.A. Approved
AIRPLANE & SYSTEMS
– No Change
7-28
SECTION 7
DESCRIPTION
No
– No Change
– No
October 4, 2005