曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
CONTROLS AND INDICATIONS (Cont)
ENGINE START CONTROLS
AIR COND/BLEED CONTROL PANEL
EICAS DISPLAY
CFO1801002_015
CRANK START
OFF
CRANK START
OFF
R ENGINE
OFF
RUN
L ENGINE
OFF
RUN
CFO1801002_003 AIR SOURCE
NORM
OFF PACK ONLY
TRIM AIR
ONLY
RAM AIR
ON
XBLEED R BLEED
OFF
APU
ON
L BLEED
OFF
T
600 600
85.0 MCT 85.0 MCT
93.0 61.0
NI
MACH
HOLD
VIB VIB
ITT
IGN IGN
N2
OIL PRESS
OIL TEMP
FF PPH
84.7
46
115
7300
84.7
46
115
7300
APU RPM 300
APU EGT 250
S
T
A
R
T
S
T
A
R
T
O V
CFO1801002_017
2
POWERPLANT
Sep 14/2005 Flight Crew Operating Manual Volume 2
REV 4 CSP 100-6 18-01-25
EICAS MESSAGES
The powerplant messages are shown on the EICAS. In the table below are the powerplant messages, meanings, inhibits,
and aural warnings along with a brief explanation of each message.
MESSAGE INHIBITS MEANING
AURAL
WARNING
L (R) ENGINE
EXCEEDANCE
The respective engine has exceeded a speed or
temperature limit
L (R) ENGINE FIRE
The L (R) ENGINE FIRE CAS, FIRE EI in the
N1 indicator, FIRE indication in the L(R) ENG
FIRE switch, or “LEFT (RIGHT) ENGINE FIRE’
voice message indicates that the engine fire
detection loop has activated. An engine fire is
usually accompanied by other indications, such
as: excessive ITT, erratic or rough engine operation,
fluctuating engine indications, or smoke in
the cabin.
“Left (Right)
Engine Fire”
L (R) ENG OIL
PRESS LOW TO/LAND The respective engine oil pressure is low
L (R) REVERSER
UNSAFE
Illumination of either the L or R REVERSER
UNSAFE CAS, or a REV EI indicates an unsafe
thrust reverser condition. The affected engine
should automatically decelerate to idle. The
autostow function will attempt to stow the
reverser doors
L (R) ENGINE
FLAMEOUT The respective engine has had a flameout
ENGINES FUEL
BYPASS TO/LAND Both engine fuel filters are impending bypass
L (R) ENG OIL TEMP
HIGH TO/LAND The respective engine oil temperature is high
L (R) ENG ANTI-ICE
FAIL TO/LAND The respective engine anti-ice has failed
L (R) ENG
DSPL MISCOMP TO/LAND
The respective engine N1 or ITT display does
not agree with the other N1 or ITT display
L (R) ENG FUEL SOV
FAIL TO/LAND
The respective engine fuel shutoff valve has
failed to close when commanded
L (R) ENG OIL TEMP
HIGH TO/LAND The respective engine oil pressure is low
L (R) ENG OIL PRESS
HIGH TO/LAND The respective engine oil pressure is high
L (R) ENGINE
VIBRATION TO/LAND
A higher than normal level of vibration has been
sensed REV 4 in the respective engine
POWERPLANT
Volume 2 Flight Crew Operating Manual Sep 14/2005
18-01-26 CSP 100-6 REV 4
L (R) FADEC FAIL TO
Major control system failure affecting both channels
of the respective FADEC. The engine may
shutdown or got to idle, or engine operation may
be degraded. Failure of the control system may
cause control effect, performance degradation
or a loss of a protective system
L (R) REVERSER FAIL TO The respective thrust reverser has failed
L (R) START
ABORTED TO/LAND
The ground engine start on the respective
engine has been aborted
L (R) STARTER FAIL TO/LAND The respective engine starter has failed
L (R) STARTER FAIL
ON TO/LAND The respective engine starter has failed ON
DOWNLOAD FADEC TO/LAND
The FADEC maintenance data should be downloaded
ENG SYNC/M-HOLD
FAIL TO/LAND Engine SYNC and Mach hold are not available
L (R) ENG A/ICE FAIL
ON TO/LAND The respective nacelle anti-ice has failed ON
L (R) ENG FUEL TEMP
LOW TO/LAND
The fuel temperature in the respective engine
filter is low
L (R) ENG IGN FAUL TO/LAND
A fault has been detected in the respective
engine ignition
L (R) ENG THRUST
FAULT TO/LAND
A fault has been detected in the respective
engine thrust
L (r) ENGINE FAULT TO/LAND
A fault has been detected in the respective
engine
L (R) ENGINE FUEL
BYPASS TO/LAND
The respective engine fuel filter is impending
bypass
ENG MACH HOLD
FAIL TO/LAND The Mach hold function has run out of authority
L (R) ENGINE MINOR
FAULT TO/LAND The engine has detected a minor engine fault
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Bombardier_Challenger_Global_00-Powerplant(13)
