MAINTENANCE MANUAL
Effectivity: All
Page 31-17
Edition 2 | Rev. 1
CENTRAL WARNING SYSTEM
1. DESCRIPTION AND OPERATION
The airplane is equipped with optical and acoustic signalization, which informs the crew about unusual
situations.
A. Optical signalization
The upper left section of the instrument panel includes signaling lights. Red signaling lights with
the highest priority display failure states of the airplane systems. Orange signaling light displays
the emergency system activation, green and blue signaling light informs the crew about the
system state.
The combination of signaling lights depends on the airplane equipment. Fig. 31-7 displays the
maximum number of signaling lights for basic versions of the instrumental equipment.
Meaning of the individual signaling lights:
AUX. CHARG.
red Auxiliary generator failure.
Applies only to the
airplanes with an
CANOPY
red Unsecured cockpit canopy.
Applies only to the
airplanes with analog
EMS
red
Exceeding of the engine limit
Applies to the airplanes
PARK BRAKE
LEVER UP
orange Park brake is activated.
Applies to the airplanes
with the park brake
FLAPS
orange Flaps are in take-off or landing
position.
Applies only to the
airplanes with analog
EXT. POWER
blue External power source is connected.
Applies only to the
airplanes with a socket
of the external power
PITOT HEAT.
green Heating of the pitot-static tube is
activated.
Applies only to the
airplanes with analog
devices and pitot-static
NOTE
Signalization of the unsecured cockpit canopy, extended flaps
and activated Pitot-static tube heating of the airplane with the
Dynon SkyView system is indicated on the EMS display.
Signalization of the unsecured cockpit canopy, extended flaps
and activated Pitot-static tube heating of the airplane with the
Garmin G3X system is indicated on the MFD.
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