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ACA Citabria Explorer 7ECA - Flaps System (7 GCBC Only)

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Citabria 6-7
An elevator trim tab is mounted on the left elevator. The trim control is located on the left side of
the cabin between the two seats. Take-off position is indicated by a white dot on the control
quadrant.
Rudder trim is provided by ground adjustable tab located on the rudder control surface.
FLAPS (7GCBC ONLY)
Wing flaps are mechanically operated by cables and interconnected by a torque tube. The flap
handle is located to the left of the pilot. Flap settings of 0°, 7°, 14°, 21°, 27° and 35° are
available by pulling the handle for retraction. No UP lock is provided.

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