Aircraft Type: CTSW
FLIGHT DESIGN
Aircraft Operating Instructions
Page: 7-2
AU 010 01000
Rev. No: 7
Original Issue Date: 28-Feb-2005
Revision Date: 29-Apr-2008
Failure of the Dynon EMS
Failure of the Dynon EMS (if equipped) does not directly endanger continuation of flight.
With a completely failed EMS system the engine data can no more be surveyed by the
pilot. To avoid damages to the engine the flight can be continued, but operation should
be limited to moderate RPMs (equalling maximum 185 km/h / 100 kts cruise speed at
flaps fully negative). Aerotow or banner tow shall not be done with this failure. Ongoing
flights to a qualified service station are allowed with the limitations named before.
Before such a flight due care has to be given to oil and coolant quantity checks before
the flight.
Flap control failure
If failure of the flap control occurred, proceed a suitable landing area and perform a
precautionary landing. Use instruction for the flap manual operation.
Instruction for the flap manual operation
1) To activate the manual operation of the flap control printed circuit board (PCB), do as
follows.
a) Turn the flap control switch by 180° with reference to 15° position to illuminate the
LED display VD1 and central segments of the automatic operation indicator (provided
the processor is in proper working condition).
This is to notify that the manual operation is switched on and the automatic operation
is switched off. The control system is in the stand-by mode.
VD1
b) When the flap control switch is turned by 180°
with reference to 30° position, the
flaps start to retract (flaps move up)
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