AEROPRAKT-22LS Pilot Operating Handbook
A22LS-POH-04
8.7.2 Elevator trim tab control system
Elevator trim tab is used for controlling the force on control yokes in pitch. The trim tab
control lever is accessible from both pilot seats.
Fig. 5 Elevator trim tab control system
The trim tab control lever 1 ( Fig. 5 ) is placed on the central console. It is retained in place
by friction adjusted using the wheel 2.
The trim tab control lever is connected with a cable 3 to the trim tab control arm 4. The
cable is running through the flexible conduits 5 (in the central console) and 6 (in stabilizer)
and cable fairleads 7 and 8 inside the tail boom. The trim tab is hinged to the elevator
trailing edge on a wire serving also as a torsion spring.
The trim tab angles of deflection are: upward 21±1°, downward 22±1°.
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Summary of Contents for 22LS
Page 8: ...AEROPRAKT 22LS Pilot Operating Handbook A22LS POH 04 Approved fuel types see paragraph 3 6 8...
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