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Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
9.2. AVIONICS
The avionic system installed on P2010 is mainly based on the integrated avionic
suite Garmin G1000. The installed configuration is based on a two-screen layout.
Primary flight information are displayed on the LH screen, namely PFD (Primary
Flight Display).
Primary Engine and moving map information are displayed on the RH display,
namely MFD (Multi-Function Display).
Both communication and navigation means, including the ones provided by third
party units (i.e. ADF and DME), are integrated within the suite and their related
information are displayed on both PFD and MFD.
In the event of a PFD or MFD failure the “reversionary mode” is automatically
enabled.
In the event of a failure of the automatic reversion logic, the pilot can force rever-
sionary mode by pressing “reversionary mode” button marked in red and located
on the audio-panel.
When reversionary mode is activated primary flight and engine information are
presented together on the remaining display.
In order to provide the pilot with main flight information in the event of a dual
display failure of both PFD and MFD, or in the event of an AHRS and ADC units
combined failure, an integrated digital stand-by instrument, Mid-Continent MD-
302, featuring airspeed, altitude, attitude and slip information is installed.
A dedicated analogue indicator is provided for pitch trim position.
The installed equipment is such that the aircraft is able to fly under day/night VFR
and day/night IFR rules and to perform ILS CAT I approaches with ILS.
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