Cessna 402C - Page 212

SECTION 7
AIRPLANE &. SYSTEMS DESCRIPTIONS
AILERON SYSTEM
~~l402C
Each aileron, see Figure 7-4, is attached to the rear main wing spar at
two points. The aileron is actuated by a bellcrank which is attached to a
wheel in the wing. The wheel is actuated by cables attached to the pilot's
control wheel. When the rudder is actuated, a spring assembly, intercon-
nected to the aileron system, causes the ailerons to automatically
assist
the turn.
AILERON SYSTEM
DETAIL B
DETAIL C
DETAIL A
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