G3-8 MA FM 3207 - R02
7
Airplane and Systems Description
Systeme 7 - 9
elevator control system
The control sticks are installed to a pivoting connection element
(stick bridge). Thereby a push/pull input stick is transferred from the
control stick through a bell crank and a push-pull tube towards the
elevator. An electrical operated elevator trim tab is installed on the
elevator.
The elevator control system is connected to the elevator by a quick
connector to allow the tailplane to be detached from the aircraft.
Checking this quick connector is part of the preflight check!
Insecurely connected, improper operation of control surfaces or inse-
curely locked fasteners will lead to loss of control of the aircraft!!
Checks inside the aircraft
Summary of Contents for GX eLITE
Page 21: ......
Page 23: ......
Page 24: ......
Page 135: ...POH Supplement Flight Training...
Page 149: ...POH Supplement Glider Towing...
Page 169: ...POH Supplement Banner Towing...