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TAT 2 FAIL
ICE DETECTOR FAULT
L COWL A/ICE FAULT
ICE
YD HEAT 1 FAIL
YD HEAT 2 FAIL
TAT 1−2−3 FAIL
Indicates that the respective
TAT has failed.
ICE AND RAIN PROTECTION
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
14−10−20
ICE AND RAIN EICAS MESSAGES (CONT'D)
L−R COWL A/ICE ON
Indicates that the respective cowl
anti-ice has been selected ON.
L−R WSHLD HEAT OFF
Indicates that the respective
temperature controller
selector is selected to
OFF/RESET.
WING XBLEED FROM L − R
Indicates that wing anti-ice is
being supplied from the
selected side.
WING A/ICE AUTO
Indicates that wing anti-ice
has been selected to AUTO.
WING A/ICE ON
Indicates that wing anti-ice
has been selected ON.
L−R COWL A/ICE AUTO
Indicates that the
respective cowl anti-ice
has been selected to AUTO.
GF1410_031
L COWL A/ICE AUTO
R COWL A/ICE AUTO
L COWL A/ICE ON
R COWL A/ICE ON
L WSHLD HEAT OFF
R WSHLD HEAT OFF
WING A/ICE AUTO
WING A/ICE ON
WING XBLEED FROM L
WING XBLEED FROM R
ICE AND RAIN PROTECTION
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
14−10−21
ICE AND RAIN PROTECTION
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
14−10−22
THIS PAGE INTENTIONALLY LEFT BLANK
CB - ICE SYSTEM
GF1420_001
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 2/2
CIRCUIT BREAKER SYSTEM
HYD
ICE
IND/RECORD
LDG GEAR
LIGHTS
NAV
OIL
OXYGEN
THRUST REV
BRT
BATT
HBMU 2
L AOA HEAT
L WINDOW HEAT
HBMU 1 IN
IN
IN
IN
IN
BATT
DC ESS
AC ESS
L COWL A/ICE VLV
AC ESS
AC ESS
IN
AC 1
L WIING A/ICE CTL
L WISHLD HEAT 1
PITOT 1 HT A
PITOT 1 HT B
L WINDOW HEAT CTL IN
IN
IN
IN
IN
DC ESS
DC ESS
AC 1
L WSHLD HEAT 2
AC 1
AC ESS
IN
PITOT 3 HT
R AOA HEAT A
R COWL A/ICE VLV
R ICE DETECTOR
PITOT 2 HT IN
IN
IN
IN
IN
AC 2
AC ESS
AC 1
R AOA HEAT B AC ESS
BATT
AC 1
IN
L ICE DETECTOR
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CB − ICE SYSTEM 1/5
CB − ICE SYSTEM 2/5
CB − ICE SYSTEM 3/5
R WINDOW HEAT CTL
R WING A/ICE CTL
R WSHLD HEAT 1
R WSHLD HEAT 2
STBY PITOT HT
R WINDOW HEAT IN
IN
IN
IN
IN
AC 2
DC 1
DC ESS
AC 3
AC 3
AC ESS IN
TAT HT 2
TAT HT 3
WAI XBLEED CTL
WAI XBLEED VLV
TAT HT 1 IN
IN
IN
IN
IN
AC ESS
AC ESS
AC 3
DC ESS
DC ESS
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CCBP
CB − ICE SYSTEM 4/5
CB − ICE SYSTEM 5/5
ICE AND RAIN PROTECTION
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
14−20−1
ICE AND RAIN PROTECTION
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
14−20−2
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION
General 15−10−1
Main Landing Gear Assembly 15−10−1
Main Landing Gear Schematic 15−10−2
Wheel Assemblies 15−10−3
Main Gear/Door Downlock Safety Pins 15−10−4
Main Landing Gear Overheat Detection 15−10−4
Landing Gear Bay Overheat Schematic 15−10−5
Nose Landing Gear Assembly 15−10−6
Nose Landing Gear Schematic 15−10−7
Nose Gear Downlock Safety Pin 15−10−8
Landing Gear Electronic Control Unit (LGECU) 15−10−9
LGECU System Schematic 15−10−9
LGECU Control 15−10−10
LGECU Control Schematic 15−10−11
Landing Gear Control System 15−10−12
Landing Gear Control Panel 15−10−12
Landing Gear Indication 15−10−12
Landing Gear Position and Warning System 15−10−13
Landing Configuration Warning 15−10−14
　
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