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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.
POWER PLANT
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
18−10−69
POWER PLANT EICAS MESSAGES (CONT'D)
GF1810_102 A/T
ADC MISCMP
A/T IRS MISCMP
A/T 1 FAIL
A/T 1 FAIL
ENG SYNC FAIL
ENG SYNC LIMITED
L BLEED ON
R BLEED ON
L BLEED OFF
R BLEED OFF
L−R 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 and R IGNITION ON
Indicates that the IGNITION
switch has been selected and
the EEC is activating all igniters.
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 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 BLEED OFF
Indicates that the selected bleed
has been selected OFF.
POWER PLANT
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
18−10−70
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 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
18−20−1
CB - OIL SYSTEM
GF1820_002A
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
L ENG LUBE
LUBE PUMP
R ENG LUBE
APU LUBE IN
IN
IN
IN
BATT
BATT
BATT
BATT
CB − OIL SYSTEM 1/1
OIL TANK PROBE DC 2 IN
BRT
NOTE
The OIL TANK PROBE power source is tied to the MAP LTS circuit breaker, therefore, the
OIL TANK PROBE circuit breaker is OUT for airplanes incorporating SB 700−79−005.
POWER PLANT
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
18−20−2
CB - OIL SYSTEM (CONT'D)
Effectivity:
· Airplanes 9002 thru 9122 not incorporating Service Bulletin:
· SB 700−24−045, AC and DC Power Distribution − Unit Change and Activation of Build 4
Electrical System.
GF1820_003
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
L ENG LUBE
LUBE PUMP
R ENG LUBE
APU LUBE IN
IN
IN
IN
BATT
BATT
BATT
BATT
CB − OIL SYSTEM 1/1
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庞巴迪挑战者手册7(155)
