Cessna 162 SKYLANE, Руководство по эксплуатации для пилотов и дополнение к учебнику по летной подготовке

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SECTION 2 CESSNA
AIRPLANE AND SYSTEM DESCRIPTION MODEL 162
GARMIN G300
U.S.
FLIGHT CONTROLS
(Continued)
Dual under panel control sticks are used for aileron and elevator
control. The under panel control sticks mimic the control movement of a
floor mounted control stick while providing ease of entry to the cabin.
The control stick location is designed so that the pilot's hand naturally
falls on the control stick with the outboard arm on the door arm rest.
Rudder pedals with toe brakes provide rudder control through forward
and aft individually adjustable pilot and copilot pedal assemblies.
Rudder pedals should be adjusted so that it is possible to have full
brake pedal deflection when the same side rudder is fully deflected.
Wing flaps are manually operated down by a flap handle located
between the seats and returned to faired UP position by air load and
return spring assist. Flap detent position UP, 10º, 25º, or FULL may be
selected only after depressing the release button in the end of the flap
handle.
A control gust lock is provided. The control lock pins the left control
stick through a bracket to immobilize the ailerons and elevator. Rudder
is held centered by the springs used for increasing rudder pedal force.
During the preflight walk-around inspection it is possible to move the
ailerons into an over-centered position by moving the aileron down
from the centered or faired with the flaps UP flaps position. The down-
deflected aileron may appear to be stuck or difficult to move up. This is
normal characteristic of the Cessna 162 ailerons system that only
occurs when the ailerons are moved down from outside the airplane. It
is recommended that the aileron movement be checked by moving the
ailerons up from the flaps UP faired position then returned to this
position. However if an aileron is externally moved down and becomes
over-centered, simply re-center the cockpit control stick and continue
the walk-around inspection.
CAUTION
AILERON OVER CENTERING ONLY OCCURS WHEN
AILERONS ARE MOVED FROM OUTSIDE THE
AIRPLANE. CONTROL STICK STIFFNESS OR STICKING
IN ANY DIRECTION OF ANY CONTROL SURFACE THIS
IS NOT NORMAL AND SHOULD BE INSPECTED BY
MAINTENANCE PERSONNEL PRIOR TO FLIGHT.
162PHUS-01
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