Tecnam P2008 JC, Flight Manual

Page: 250 / 264

AFMS for VFR NIGHT equipped airplanes
Page N7 - 6
Section 7 – Airframe and Systems description
INSTRUMENT PANEL
Ed. 1, Rev 0
4. INSTRUMENT PANEL
The instrument panel is divided in four areas:

The left area holds primary (analogue) and pilot’s situational awareness (G3X LH
display) flight instruments, a chronometer, a pitch trim indicator and a holds
Day/night switch (selecting between two brightness levels for warning lights in the
annunciator panel);

The right area holds thus a voltmeter, the breaker panel and primary analogue
engine instruments:

Oil Temperature indicator

RPM indicator

CHT indicator

The central area holds the stabilator trim cut out switch and LH/RH selector
switch, the dimming devices (for G3X, for flexible support mounted panel lights
and for instruments), Nav/Com instrument (Garmin GNC 255A) , the GTX 328
transponder and the annunciator panel,,

Electric fuel pump ON (GREEN)

Low Oil Pressure (RED)

Low Fuel Pressure (RED)

Alternator Fail (AMBER)

Pitot heat operation lights (GREEN/AMBER)

High Oil Pressure warning light (RED)

The lower-LH portion of the instrument panel holds:

Ignition key;

Master and Generator switches;

Emergency fuel pump;

Avionic Master switch;

Pitot heat switch;

Emergency light switch;

Carburetor heat knob;

The lower-Central portion of the instrument panel holds:

Throttle;

Two analogue fuel quantity indicators;

Fuel selector valve;

The lower-RH portion of the instrument panel holds:

Flap indicator and toggle switch;

Cabin heating knob;

NAV, land and strobe switches.