Introduction
This Supplement contains supplemental information to operate the aircraft in a safe and efficient
manner when equipped with Garmin G3X Touch and analogical engine instruments.
Section 1 - General
1.1. Instrument Panel
The aircraft is equipped with a Garmin G3X Touch screen (GDU 460) which provides the information
and parameters of the flight. The system obtains the necessary data through the GSU 25 ADHARS,
the GMU 11 or GMU 22 Magnetometer and the OAT probe, GTP 59. The G3X system also
incorporates a GPS receiver.
Engine information is provided to the pilot through conventional instruments. These provide
information on RPM, flap angle, voltimeter, coolant temperature, oil temperature and pressure, and
fuel quantity indicators for each tank, left and right.
A pair of instrument lights (if installed) are fixed on the sides of the instrument panel, equipped with
flexible struts, they can be adapted to illuminate the instrument panel, according to the needs of the
pilot. A dimming device, if installed, is located in the upper area of the central instrument panel,
allowing the brightness of the instrument lights to be adjusted.
In addition, a map light (dimmable) and two hazard lights are provided on the roof of the cabin.
A magnetic compass is installed for additional heading information.
The left area holds:
- (Pitch) Trim switch
- PFD Garmin GDU 460
- Fuel Pump switch
- AP Master switch (if installed)
- Ignition key
- Master and Generator switches
- Autopilot control panel (if installed).
- Choke Push
The central area holds:
- Audio panel (if installed)
- Radio VHF/COM/NAV
- Fuel selector
- Flap control switch
- Day/ Night switch (if installed)
- Instrument dimmer (if installed)
- Throttle friction knob.
- Backup instruments (if installed)
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