Arion Aircraft LS-1 Lightning, Pilot Operating Handbook, Page: 144 / 164

Section 9 Lightning LS-1
Flight Training Supplement Pilot’s Operating Handbook
Page FTS-4 Issue B
Figure S11-3: Throttle
SECONDARY CONTROLS
The secondary controls are the elevator (pitch) trim,
wing flap actuation, and braking controls. Pitch trim
and wing flap switches are located above the engine
controls in a GRT system (See Figure S11-4) or below
the engine controls in a Dynon system.
The angle of the wing flaps is changed by a linear
actuator mounted in the center console below and
between the seats. The wing flap control rocker
switch is located on the instrument panel, either
above or below the engine controls (see Item 1,
Figure S11-4). Pushing the bottom of the switch
lowers the flaps and pushing the top raises the flaps.
The elevator trim is actuated using the rocker trim
switch (Item 2, Figure S11-4). Pushing the top of the