Tecnam P2010 2015 - 4. Instrument Panel

AFMS N" D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV 7-9
4 IN S TRU MEN T P AN EL
The insb1Jment panel is divided in three areas:
The left area holds Garmin G I OOO PFD, a chronometer and the pitch trim indicator;
The Central area holds the standby unit for PFI parameters, MD 302 suite, and
the EL T button;
The right area holds Garmin GIOOO MFD with dedicated AP control buttons
and breaker panel;
The lower-LH portion of the insb1Jment panel holds:
};;> Ignition key;
};;> Master and Generator switches;
};;> Emergency fuel pump;
};;> Avionic Master switch;
};;> AP Master switch
};;> Trim Disconnect switch
The lower-Central portion of the instrument panel holds :
};;> Fuel selector valve.
};;> Flap Control
The lower-RH portion of the insb1Jment panel holds:
};;> Pocket
Fig. 7-8. INSTRUMENT PANEL
Section 7 - Airframe and Systems description
INSTRUMENTAL PANEL
Ed. 2. Rev.O