Cessna 402C Pilot Operating Handbook page 216

SECTION 7
AIRPLANE & SYSTEMS DESCRIPTIONS
RU DOER SYSTEM
~~L402C
The rudder, see Figure 7-8, is attached to the vertical stabilizer rear
main spar at three points. The rudder is actuated by a bellcrank attached
to the bottom of the rudder. The bellcrank is actuated by cables attached
to the cockpit rudder pedals. When the rudder is actuated, a cable and ~
spring assembly that is
connected to
the aileron system causes the ailerons
to automatically assist the turn.
RUDDER SYSTEM
7-12
DETAIL
A
Fi gure 7-8
B
DETAIL
B
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A.851611045
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