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03-03-08
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS MULTI-FUNCTION DISPLAYS (MFD)
MFD display systems information, synoptic diagrams, and CAS messages are usually displayed on the left MFD.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
03-04-01
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS (Cont) ANTI-ICE SYNOPTIC PAGE
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
03-04-02
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS (Cont) ECS SYNOPTIC PAGE
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
03-04-03
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS (Cont) ELECTRICAL SYNOPTIC PAGE
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
03-04-04
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS (Cont) FLIGHT CONTROLS SYNOPTIC PAGE
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
03-04-05
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS (Cont) FUEL SYNOPTIC PAGE
UP
UP UP
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
03-04-06
AURAL/VISUAL ALERTS
CONTROLS AND INDICATIONS (Cont) HYDRAULIC SYNOPTIC PAGE
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
03-04-07
EICAS MESSAGES
The engine indicating and crew alerting system messages are shown on the EICAS. In the table below, a brief explanation for each message is provided.
MESSAGE INHIBITS MEANING AURAL WARNING
EFIS COMPARATOR INOP TO/LAND EFIS comparator unable to compare one or more of the following parameters: altitude, air-speed, roll attitude, pitch attitude, heading, radio altitude, flight director, localizer or glideslope
EFIS MISCOMPARE There is a mismatch between the onside and cross-side data and accompanied by a PFD annunciation ALT, IAS, ROL, PIT, HDG, LOC, GS, RA, or FD
L (R) IAPS FAIL TO/LAND The respective Integrated Avionics Processing System has failed
PFD X-TALK FAIL TO/LAND Communication between the PFDs has failed. REFs menu pages 1, 2 and 3 are not synchro-nized. The EFIS comparator will be inoperative and is unable to compare one or more of the fol-lowing parameters: altitude, airspeed, roll atti-tude, pitch attitude, heading, radio altitude, flight director, localizer or glideslope
DCU FAULT TO/LAND Channel A or B in the DCU failed.The yaw damper may fail. The rudder travel limiter moni-toring may be inoperative
MFD X-TALK FAIL TO/LAND Communication between the MFDs has failed, and cross side tuning will not be available
RDC FAN FAIL TO/LAND Channel A or B of the remote data concentrator has failed
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