Introduction; Airframe; Flight Controls; Trim Systems - Cessna U206G STATIONAIR Pilot Operating Handbook

SOLOY TURBINE PAC SECTION 7
POHS CESSNA U/TU 206G AIRPLANE & SYSTEMS
DESCRIPTION

INTRODUCTION

This section provides description and operation of the airplane and its
systems. Some equipment described herein is optional and may not
be installed in the airplane. Refer to Section 9, Supplements, for
details of other optional systems and equipment.
– No Change

AIRFRAME

– No Change

FLIGHT CONTROLS

TRIM SYSTEMS – No Change Except:
The Soloy Turbine Pac system consists of a dual actuator trim tab.

INSTRUMENT PANEL

The instrument panel (refer to Figure 7-1) is designed around the basic
"T" configuration. The gyros are located immediately in front of the
pilot, and arranged vertically. The airspeed indicator and altimeter are
located to the left and right of the gyros respectively. The TOT, N
p
(propeller RPM), and torque indicators are located in a cluster gauge to
the right of the altimeter. Avionics equipment is stacked approximately
on the center line of the panel.. The right side of the panel contains
the annunciator panel, flight hour recorder, suction gauge, fuel
totalizer, engine cluster gauge (N , oil temperature, oil pressure),
1
transmission oil pressure, fuel quantity indicators, ammeter, and space
for additional instruments and avionics equipment. On serial numbers
U20606440 and on, the suction gauge and ammeter are located on the
left side of the panel. A switch and control panel at the lower edge of
the instrument panel contains most of the switches, controls, and
circuit breakers necessary to operate the airplane. The left side of the
panel contains the motor/start switch, generator/APU switch, battery
switch, auto-feather test button, light intensity controls, electrical
switches, avionics power switch and circuit breakers for installed
equipment. On serial numbers U20606440 and on, all circuit breakers
for general electrical equipment and avionics are mounted in a circuit
breaker panel located on the left cabin sidewall adjacent to the pilot's
seat. The center area contains the power control, propeller control,
and fuel cutoff control. The right side of the panel contains the wing
flap switch and indicator, cabin heater, cabin air, defroster, auxiliary
cabin air control knobs and the cigar lighter. A pedestal, extending
from the lower edge of the switch and control panel to the floorboard,
7-9
F.A.A. Approved October 4, 2005