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when submerged under water.
TRI-AXIAL ACCELEROMETER
The tri-axial accelerometer is used for acceleration measurements. It contains three separate seismic sensors that measure
vertical, lateral, and longitudinal acceleration near the center of gravity of the aircraft. This data is sent to the DCUs where
it is formatted for the FDR.
COMMUNICATIONS
Volume 2 Flight Crew Operating Manual Sep 13/2004
06-01-18 CSP 100-6 REV 1
EICAS MESSAGES
Communication messages are shown on the EICAS. In the table below is a list of communication system messages. A brief
explanation of each message is provided.
MESSAGE INHIBITS MEANING
AURAL
WARNING
CVR FAIL TO/LAND The cockpit voice recorder has failed
FDR FAIL TO/LAND The flight data recorder has failed
FDR FAULT TO/LAND
The longitudinal, lateral or normal accelerations
parameters in the flight data recorder are inoperative.
It may be possible to clear this message
SELCAL HF 1
SELCAL HF 2 TO/LAND
The SELCAL code has been received on HF 1 or
HF 2
“SELCAL”
SELCAL VHF 1
SELCAL VHF 2
SELCAL VHF 3
TO/LAND
The SELCAL code has been received on VHF 1,
2, or 3
“SELCAL”
SELCAL DATALINK TO/LAND
The SELCAL code has been received on
DATALINK
“SELCAL”
ELT ON Pilot status that ELT is transmitting
EV 1

　
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