Airplane and Systems Description 2 - 12
Rev. 01 – 07-01-2008
2
Airplane and Systems Description
2.13 Dual Throttle, Oil Temperature Control, Additional Terminals
Two extension panels are located to the left and to right of the cockpit frame
which are used as follows:
Left Panel (illustrated to the right)
At the upper position the oil temperature control is installed. Push – to
increase temperature, Pull – to decrease temperature.
At the lower position the dual trottle control is located. The dual throttle lever
does not feature a friction lock.
Right Panel (not illustrated)
At the upper position the 12V receptacle for external use (i.e. portable GPS) is
installed. Beneath you will find two audio-in connectors (if fitted).
This panel is also prepared to add 2 Sub-D 9-pin connectors, to be used as
PC interface for connecting installed devices to a personal computer.
Summary of Contents for G 2008 Series
Page 1: ...i...
Page 7: ...vii Rev 01 07 01 2008 Views The REMOS GX is designed as full composite carbon fiber aircraft...
Page 15: ...Airplane and Systems Description 2 5 Rev 01 07 01 2008 2 Airplane and Systems Description...
Page 47: ...Performance 5 5 Rev 01 07 01 2008 5 Performance 5 5 Pressure Altitude Diagramm...
