Tecnam P2010, Flight Manual, Page: 331 / 587

AFMS N°D03 FOR ALTERNATIVE AVIONICS CONFIGURATION
Page 3G-7
Section 3 – Emergency procedures
AVIONIC SUITE FAILURES
Ed. 1, Rev.0
3. G500 S
YSTEM
F
AILURES
3.1 L
OSS OF INFORMATION DISPLAYED
When a LRU or a LRU function fails, a large red „X‟ is typically displayed on
the display field associated with the failed data.
In most of cases, the red “X” annunciation is accompanied by a
message advisory alert issuing a flashing ADVISORY Softkey
annunciation which, once selected, acknowledges the presence
of the message advisory alert and displays the alert text message
in the Alerts Window.
3.2 L
OSS OF AIRSPEED INFORMATION
AIRSPEED FAIL
(
RED
X
ON DISPLAY FIELD
)
Display system is not receiving airspeed input
from Air Data Computer.
INSTRUCTION : revert to standby instrument
NOTE