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R AIR COND
CONT
DC BUS 2
F9
Cabin Temperature
Control
CABIN TEMP
CONT LO LIM
E13
CABIN TEMP
CONT MAN
E14
CABIN TEMP
CONT AUTO
E15
CABIN FAN AC BUS 2 C9
Cockpit Temperature
Control
CKPT TEMP CONT
LO LIMIT
DC ESS 4
C9
CKPT TEMP CONT
MAN
C10
CKPT TEMP CONT
AUTO DC BUS 1
1
E15
CKPT HTR CONT F8
CKPT HTR
AC BUS 1
A8
CKPT FAN C9
Avionics Cooling
System
Display Fans
DISP FAN D5
DISP FAN CONT DC BUS 1 F1
AIR CONDITIONING AND PRESSURIZATION
Summary
Vol. 2 02−20−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
AIR CONDITIONING AND PRESSURIZATION
Summary
Vol. 2 02−20−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION
General 03−10−1
Engine Indicating and Crew Alerting System (EICAS) 03−10−2
Description 03−10−2
Components and Operation 03−10−2
Controls and Indicators 03−10−3
Master Warning Switch/Lights 03−10−3
Master Caution Switch/Lights 03−10−3
Aural Warning Testing 03−10−4
Aural Alert Disable 03−10−5
EICAS Control Panel 03−10−5
EICAS Primary Page 03−10−6
EICAS Status Page 03−10−10
EICAS Messages 03−10−11
Takeoff Configuration Warning 03−10−13
Inhibited EICAS Caution Messages 03−10−13
Display Reversionary Control 03−10−14
Maintenance Diagnostic Computer 03−10−17
Description 03−10−17
Operation 03−10−17
Flight Data Recorder 03−10−18
Description 03−10−18
Components and Operation 03−10−18
FDR EVENT Switch 03−10−18
Hard Landing Indication System 03−10−19
Description 03−10−19
Operation 03−10−19
EICAS Messages 03−10−20
SUMMARY
Power Supply and Circuit Breaker Summary 03−20−1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 03−10−1 EICAS Displays Location 03−10−1
AURAL/VISUAL WARNING SYSTEM
Table of Contents
Vol. 2 03−00−1
REV 75, Feb 17/09
CHAPTER 3 - AURAL/VISUAL WARNING SYSTEM
03−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 03−10−2 EICAS Control Panel (ECP) 03−10−1
Figure 03−10−3 Master Warning and Caution Lights 03−10−4
Figure 03−10−4 AURAL WARN/LAMP TEST Panel 03−10−4
Figure 03−10−5 DCU Disable Controls 03−10−5
Figure 03−10−6 EICAS Control Panel (ECP) 03−10−6
Figure 03−10−7 EICAS Primary Page 03−10−8
Figure 03−10−8 EICAS Status Page Displays 03−10−9
Figure 03−10−9 Display Reversionary Control Panel 03−10−16
Figure 03−10−10 Maintenance Diagnostic Computer Switch 03−10−17
Figure 03−10−11 FDR EVENT Switch 03−10−18
Figure 03−10−12 Hard Landing Indication System Panel 03−10−19
AURAL/VISUAL WARNING SYSTEM
Table of Contents
Vol. 2 03−00−2
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
Page
GENERAL
The aural and visual warning system components provide the flight crew with aural, visual and tactile
indications of potentially unsafe conditions, as well as information about airplane configuration and
engine data. The system also warns of airplane system malfunctions and non-normal situations.
EICAS Displays Location
Figure 03−10−1
EICAS Control Panel (ECP)
Figure 03−10−2
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS)
Description
The function of the EICAS is to display the engine instruments and to provide visual and aural
crew-alert messages and real-time interpretation of aircraft system operation.
Two EICAS displays present the data on different selectable display pages. Some display pages
are shown by default, others are available through crew selection. The EICAS control panel (ECP),
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庞巴迪挑战者604操作手册 Operating Manual 3(28)
