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ENGINE COWL ANTI-ICE SYSTEM 15--40
Engine Cowl Anti--Ice System 15--40--1
System Circuit Breakers 15--40--5
AIR DATA ANTI-ICE SYSTEM 15--50
Air Data Anti--Ice System 15--50--1
System Circuit Breakers 15--50--4
WINDSHIELD AND SIDE WINDOW ANTI-ICE SYSTEM 15--60
Windshield and Side Window Anti--Ice System 15--60--1
System Circuit Breakers 15--60--5
WINDSHIELD WIPER SYSTEM 15--70
Windshield Wiper System 15--70--1
System Circuit Breakers 15--70--2
LIST OF ILLUSTRATIONS
INTRODUCTION
Figure 15--10--1 Anti--Iced Areas 15--10--2
ICE DETECTION SYSTEM
Figure 15--20--1 Ice Detection System -- Schematic 15--20--2
Figure 15--20--2 Ice Detection System 15--20--3
Figure 15--20--3 Anti--Ice System EICAS Indications 15--20--4
Vol. 1 15--00--2
ICE AND RAIN PROTECTION SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
WING ANTI-ICE SYSTEM
Figure 15--30--1 Wing Anti--Ice System Schematic 15--30--2
Figure 15--30--2 Wing Anti--Ice Controls 15--30--3
Figure 15--30--3 Anti--Ice Synoptic Page 15--30--4
Figure 15--30--4 Wing Anti--Ice System EICAS Indications 15--30--5
ENGINE COWL ANTI-ICE SYSTEM
Figure 15--40--1 Engine Cowl Anti--Ice System -- General 15--40--2
Figure 15--40--2 Anti--Ice Synoptic Page 15--40--3
Figure 15--40--3 Engine Cowl -- Anti--Ice EICAS Indications 15--40--4
AIR DATA ANTI-ICE SYSTEM
Figure 15--50--1 Air Data Sensor Anti--Ice System 15--50--2
Figure 15--50--2 Air Data Sensor Anti--Ice EICAS Indications 15--50--3
WINDSHIELD AND SIDE WINDOW ANTI-ICE SYSTEM
Figure 15--60--1 Windshield Temperature Control 15--60--2
Figure 15--60--2 Windshield and Side Window Anti--Ice Controls 15--60--3
Figure 15--60--3 Windshield and Side Window Anti--Ice EICAS Indications 15--60--4
WINDSHIELD WIPER SYSTEM
Figure 15--70--1 Windshield Wiper Control Panel 15--70--1
Vol. 1 15--10--1
ICE AND RAIN PROTECTION SYSTEM
Introduction REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. INTRODUCTION
Ice and rain protection is provided for the wing leading edges, engine intake cowl,
windshields, side windows and the air data probes and sensors. An ice detection system
alerts the flight crew of impending icing conditions.
Hot bleed air from the engine compressors is used to anti-ice the wing leading edges and
engine intake cowl. Electrical power is used to anti-ice the windshields, side windows, air
data probes and sensors. Electrical windshield wipers provide rain removal for the pilot and
copilot’s windshields.
A bleed air leak detection system monitors the bleed air ducting for leaks and
overtemperature (refer to Chapter 19).
Ice and rain protection system warnings and cautions are displayed on the EICAS primary
page. Status and advisory messages are displayed on the EICAS status page. A general
view of the pneumatic anti-icing system is presented as a diagram on the EICAS A--ICE
synoptic page.
Vol. 1 15--10--2
ICE AND RAIN PROTECTION SYSTEM
Introduction REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Anti---iced Areas
Figure 15---10---1
WINDSHIELDS
SIDE
WINDOW
TAT PROBE
(RH SIDE ONLY)
PITOT
STATIC
PROBE
ICE
DETECTORS
STANDBY PITOT
(LH SIDE ONLY)
AOA
VANES
WING
LEADING
EDGES
ENGINE
AIR INLET
(COWLS)
STATIC PORTS
WINDSHIELD
WIPERS
Pneumatic anti--ice.
Electrical heaters.
LEGEND
SIDE
WINDOW
Vol. 1 15--20--1
ICE AND RAIN PROTECTION SYSTEM
Ice Detection System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. ICE DETECTION SYSTEM
The aircraft is equipped with an ice detection system that alerts the flight crew of impending
icing condition. The ice detection system consists of two independent ice detector
assemblies located on each side of the forward fuselage. Each detector assembly includes
a detector unit and a probe that extends into the airstream. The ice detection system is
operational whenever AC power is available on the aircraft.
The ice detectors interface with the data concentrator units (DCU) to provide visual
indications of icing conditions. When the probes detect an ice build up, a signal is sent by
the unit to the EICAS and at the same time electrical power is used to de--ice the probe.
When the probe is de--iced, it is then ready to detect ice formation again.
Vol. 1 15--20--2
ICE AND RAIN PROTECTION SYSTEM
Ice Detection System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
　
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