AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGRATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 3-7
3. G500 SYSTEM FAILURES
3.1 LOSS 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
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
Section 3 – Emergency procedures
AVIONIC SUITE FAILURES
Ed. 1, Rev.0
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