Tecnam P2010 - Page 493

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV 7-9
Ed. 1Rev 0
Section 7 – Airframe and Systems description -
INSTRUMENTAL PANEL
4 INSTRUMENT PANEL
The instrument panel is divided in three areas:
 The left area holds Garmin G1000 PFD, a chronometer and the pitch trim indicator;
 The Central area holds the standby unit for PFI parameters, MD 302 suite, and
the ELT button;
 The right area holds Garmin G1000 MFD with dedicated AP control buttons
and breaker panel;
 The lower-LH portion of the instrument 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 instrument panel holds:
 Pocket
Fig. 7-8. INSTRUMENT PANEL