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that the airplane is within the starter
assisted engine relight envelope.
L (R) FADEC FAULT
Indicates that there is a
minor fault in the affected
should not be affected.
L (R) FUEL FILTER
Indicates that the affected fuel
L (R) OIL FILTER
Indicates that the affected oil
filter is impending bypass.
L (R) REVERSER FAULT
Indicates that there is a minor fault in
the affected thrust reverser system.
Engine operation should be normal.
L (R) REV LOCK FAULT
Indicates that one of two primary
stow switches, on affected thrust
reverser, is indicating not stowed,
with the thrust lever in the forward
OIL RES LO QTY
Indicates that the oil reservoir
has < 1.5 quarts of oil remaining. WINDMILL ENVELOPE
Indicates that FADEC has
determined that the airplane is
within the windmill start envelope.
A/T ADC MISCOMP
A/T 2 FAIL
A/T 1 FAIL
A/T IRS MISCOMP
ENG SYNC FAIL
ENG SYNC LIMITED
A/T 1 (2) FAIL
Indicates that the A/T is invalid,
or reporting a hardware or servo
failure.
A/T ADC MISCOMP
Indicates that the A/T is
is available due to an
ADC data miscompare.
A/T IRS MISCOMP
Indicates that the A/T is not
available due to an IRS data
miscompare.
ENG SYNC FAIL
Indicates that the affected
ENG SYNC LIMITED SYNC system has failed.
Indicates that the selected
SYNC system is unable to
function due to authority
limit or engine split greater
than SYNC authority.
filter is impending bypass.
FADEC. Engine operation
range.
POWER PLANT
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
18−10−71
POWER PLANT EICAS MESSAGES (CONT'D)
GF1810_102a A/T
ADC MISCMP
A/T IRS MISCMP
A/T 1 FAIL
A/T 1 FAIL
ENG SYNC FAIL
ENG SYNC LIMITED
L ENG BLEED ON
R ENG BLEED ON
L ENG BLEED OFF
R ENG BLEED OFF
L IGNITION ON
L FADEC N1 CTL
R FADEC N1 CTL
L ENG SHUTDOWN
R ENG SHUTDOWN
A/T 1 (2) FAIL
Indicates that the A/T is invalid, or
reporting a hardware or servo failure.
L (R) FADEC N1 CTL
Indicates that the affected engine is
in N1 control, by switch selection on
the engine control panel.
L (R) ENG SHUTDOWN
Indicates that the crew has initiated
shutdown on the affected engine.
A/T ADC MISCMP
Indicates that the A/T is not available
due to an ADC data miscompare.
L (R) ENG BLEED ON
Indicates that the selected bleed
has been selected ON.
ENG SYNC FAIL
Indicates that the affected
SYNC system has failed.
A/T IRS MISCMP
Indicates that the A/T is not available
due to an IRS data miscompare.
ENG SYNC LIMITED
Indicates that the selected SYNC
system is unable to function due
authority limit or engine split greater
than SYNC authority.
L (R) ENG BLEED OFF
Indicates that the selected bleed
has been selected OFF.
L (R) IGNITION ON
Indicates that the
IGNITION switch
has been selected and
the EEC is activating all
igniters.
R IGNITION ON
POWER PLANT
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
18−10−72
CB - ENGINE SYSTEM
GF1820_001
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
L ENG FUEL HPSOV
L ENG IGN 1
L ENG IGN 2
L ENG START A
L ENG START B
IN
IN
IN
IN
BATT
BATT
BATT
BATT
BATT
CB − ENGINE SYSTEM
IN
1/3
L FADEC CH B
R ENG FUEL HPSOV
R ENG IGN 1
R ENG IGN 2
R ENG START A
L FADEC CH A IN
IN
IN
IN
IN
BATT
BATT
BATT
BATT
BATT
BATT
CB − ENGINE SYSTEM
IN
2/3
R FADEC CH A
R FADEC CH B
R ENG START B IN
IN
IN
BATT
BATT
BATT
CB − ENGINE SYSTEM 3/3
VIBE MONITOR DC 1 IN
BRT
POWER PLANT
EMS CIRCUIT PROTECTION
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
18−20−1
CB - OIL SYSTEM
FGF1820_001
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
　
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