Tecnam P2008 JC, Flight Manual

Page: 257 / 264

AFMS for VFR NIGHT equipped airplanes
Page N7 - 13
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
Ed. 1, Rev 0
9.2. A
VIONICS
The avionic system installed P2008 JC is based on five analogue indicators, an air-
speed indicator, an attitude indicator, an altimeter, a magnetic compass and a slip in-
dicator, which provide primary flight information on the left side of the instrument
panel.
On the right side of the instrument panel three analogue indicators provides primary
information of engine parameters, an RPM indicator, oil temperature indicator and a
CHT indicator.
A dedicated analogue voltmeter is installed, located below engine instruments, which
provides primary information of the electrical power supplied.
The fuel quantity information is provided by two dedicated analogue indicators lo-
cated in the bottom central instruments panel.
Garmin G3X integrated avionic suite in a dual screen configuration is installed. It
provides flight and engine information intended for the pilot’s situational awareness
only.
G3X also embodies a GPS WAAS receiver whose information, intended for situ-
ational awareness only, are presented on RH display moving map.
Two dedicated indicators provide the pilot with information about the flaps and pitch
trim position.
Stand-alone external COM/NAV and transponder sources (Garmin GNC 255A and
GTX 328) are installed. Garmin GNC 255A navigation information is presented on
the display (course and direction) along with the information related to active/standby
frequency. This information is supplemented by an HSI indicator on G3X LH dis-
play.
GTX 328 transponder provides SSR (Secondary Surveillance Radar) responses; this
unit is capable of both mode “S” and mode “C”. An external altitude encoder (ACK
A-30) allows altitude reporting, this information is also presented on GTX 328 dis-
play.
An automatic reversion mode is integrated within the system in order to continue
providing the pilot with the flight and engine information in the event of a LH or RH
display failure.
Seven warning lights located on the top centre area of the instrument panel are avail-
able:

Electric fuel pump ON (GREEN)

Low Oil Pressure (RED)

Low Fuel Pressure (RED)

Alternator Fail (AMBER)

High Oil Pressure (RED)

Pitot heat ON (GREEN)

Pitot heat fail (AMBER)