DESCRIPTION
General 03−10−1
Engine Indication and Crew Alerting System 03−10−1
General Description 03−10−1
Components 03−10−2
EICAS Presentation 03−10−9
Crew Alerting System 03−10−18
Aural Alerts 03−10−25
Reversionary Control 03−10−27
Maintenance Diagnostic Computer 03−10−30
Flight Data Recorder 03−10−31
EICAS Messages 03−10−32
SUMMARY
Power Supply and Circuit Breaker Summary 03−20−1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 03−10−1 Aural/Visual Warnings 03−10−1
Figure 03−10−2 Aural/Visual Warning Control Panels 03−10−3
Figure 03−10−3 Adaptive Flight Displays 03−10−4
Figure 03−10−4 Cursor Control Panel 03−10−6
Figure 03−10−5 Reversionary Control Panel 03−10−7
Figure 03−10−6 MASTER WARNING/CAUTION Switch/Lights 03−10−8
Figure 03−10−7 AUDIO WARNING Panel 03−10−8
Figure 03−10−8 Miscellaneous Test Panel 03−10−9
Figure 03−10−9 EICAS Page 03−10−10
Figure 03−10−10 EICAS Page − Compressed 03−10−11
Figure 03−10−11 Synoptic Page Selection (1 of 3) 03−10−13
Figure 03−10−12 Synoptic Pages (2 of 3) 03−10−14
Figure 03−10−13 Synoptic Pages (3 of 3) 03−10−15
Figure 03−10−14 SUMMARY Page Layout (1 of 2) 03−10−16
AURAL/VISUAL WARNING SYSTEM
Table of Contents
Vol. 2 03−00−1
Oct 05/06
CHAPTER 3 - AURAL/VISUAL WARNING SYSTEM
03−00−1
CL−605 Flight Crew Operating Manual
PSP 605−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 03−10−15 SUMMARY Page Layout (2 of 2) 03−10−17
Figure 03−10−16 Crew Alerting Messages 03−10−18
Figure 03−10−17 Warning Messages 03−10−19
Figure 03−10−18 Caution Messages 03−10−20
Figure 03−10−19 Advisory/Status Messages 03−10−21
Figure 03−10−20 Crew Alerting Message Pagination 03−10−21
Figure 03−10−21 Crew Alerting Message De-Clutter 03−10−22
Figure 03−10−22 Miscellaneous Panel 03−10−27
Figure 03−10−23 AUDIO WARNING Panel 03−10−27
Figure 03−10−24 EICAS Selector moved to Right MFD 03−10−28
Figure 03−10−25 EICAS Selector moved to BOTH PFD’s 03−10−29
Figure 03−10−26 Displays Selector − PFD REV Selected 03−10−30
Figure 03−10−27 Displays Selector − MFD REV Selected 03−10−30
Figure 03−10−28 Maintenance Diagnostic Computer Switch 03−10−31
Figure 03−10−29 FDR EVENT Switch 03−10−32
AURAL/VISUAL WARNING SYSTEM
Table of Contents
Vol. 2 03−00−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
Page
GENERAL
Aural and visual warnings include those components that integrate information into an independent
display system. This provides the crew with flight and operational information as well as visual and
aural alerts of malfunctions and/or operational changes. Additionally, data is provided to the flight
data recorder (FDR) and the maintenance diagnostic computer (MDC). This chapter provides details
on the following:
• Engine indication and crew alerting system (EICAS);
• Flight data recording; and
• Maintenance diagnostics.
Aural/Visual Warnings
Figure 03−10−1
ENGINE INDICATION AND CREW ALERTING SYSTEM
General Description
The engine indication and crew alerting system (EICAS) processes inputs from aircraft systems to
provide visual information and aural alerts to the crew.
In general terms, the function of EICAS is to:
• Process and display engine parameters and related information;
• Process and display system parameters and related information;
• Provide a graphical depiction of certain airframe systems for the purpose of in-flight health
monitoring;
• Process and provide visual and aural alerts to the crew;
• Provide aural warning when the aircraft is not in proper takeoff configuration; and
• Process information for the flight data recorder.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：庞巴迪挑战者605机组操作手册 CL605-AURAL_and_VISUAL_WARNING_S
