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and no roll priority has been
selected within 30 seconds.
FLIGHT SPOILERS FAIL
Indicates two or more flight
spoilers have failed.
GND LIFT DUMP
Indicates when at least two
pairs of spoilers (MFS or GS)
are not available or degraded
for ground lift dumping, or
ground lift dumping is not
available.
SPLR LEVER FAIL
Indicates that the MFS
function for at least two
pairs of MFS is inoperative.
Ground lift dump and roll
assist are not affected.
For Training Purposes Only
Sept 04
10-69
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
Spoiler EICAS Messages (Cont)
789
FLT SPOILERS FAULT
GND LIFT DUMP
SPLRS/STAB IN TEST
NO TAKEOFF
GND LIFT DUMP OFF
GLD MANUAL ARM
PLT ROLL SPLRS
CPLT ROLL SPLRS
GX_10_067
FLIGHT SPOILERS FAULT
Indicates that a single pair of flight
spoilers is inoperative (may be
retracted or deployed).
GND LIFT DUMP
Indicates that the ground lift
dump function for one pair of
ground spoilers is inoperative,
or ground spoiler upfloat is
occurring in flight.
NO TAKEOFF
Indicates that the airplane is
not configured for takeoff
(example: trims, slats/flaps,
spoilers or parking brake on)
during taxi.
GLD MANUAL ARM
Displayed if the GND LIFT
DUMPING “MANUAL ARM”
switch is selected to manual.
CPLT ROLL SPLRS
Displayed if the copilot roll
spoilers switch is selected.
SPLRS/STAB IN TEST
Indicates that the spoilers
and stab trim systems are
performing self-test once
hydraulics are applied. Both
systems are inoperative
during the test (aproximately
20 seconds).
GND LIFT DUMP OFF
Displayed if the GND LIFT
DUMPING “OFF” switch is
selected off.
PLT ROLL SPLRS
Displayed if the pilot roll
spoilers switch is selected.
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
10-70 For Training Purposes Only
Sept 04
STALL PROTECTION EICAS MESSAGES
789
STALL PROTECT FAIL
STALL WARN ADVANCE
PITCH DISC FAULT
MACH XDUCER FAIL
SHAKER 1 (2) FAIL
STALL WARN BASIC
GX_10_068
STALL WARN ADVANCE
Indicates that the stall warning
advance has been activated. Can
occur automatically based on
airplane condition or manually
through the EMS CDU.
MACH XDUCER FAIL
Indicates that the mach
transducer has failed.
STALL PROTECT FAIL
Indicates either the pusher is
manually deactivated, pusher
switch is disabled, or one of the
following have failed:
• a SPC channel.
• AOA sensor, or
• the pusher.
PITCH DISC FAULT
Indicates that the pitch
disconnect solenoid has failed
in the locked or unlocked
position.
SHAKER 1 (2) FAIL
Indicates pilot or copilot’s
shaker has failed (actual
motor) or the commanding
SPC channel has failed.
STALL WARN BASIC
Indicates that the system is
incorrectly operating in a single
engine configuration (Basic
mode).
For Training Purposes Only
Sept 04
10-71
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
EMS CIRCUIT PROTECTION
M
M
M
M
CB - FLT CONTROLS SYSTEM 1/4
AILERON TRIM
FLT CTL 1 CH A
FLT CTL 1 CH B
FLT CTL 2 CH A
FLT CTL 2 CH B
MACH TRANSDUCER
DC 2
DC 1
DC 2
DC ESS
DC ESS
BATT
IN
IN
IN
IN
IN
IN
CB - FLT CONTROLS SYSTEM 3/4
DC ESS
AC 1
AC ESS
BATT
DC ESS
AC 1
CCBP
CCBP
ACPC
SLAT/FLAP CTLR 2
SLAT/FLAP PWR 1
SLAT/FLAP PWR 2
SPC CH A
SPC CH B
STAB TRIM CH 1
IN
IN
IN
IN
IN
IN
M
BRT
CIRCUIT BREAKER SYSTEM
STAT SYS BUS
PREV
PAGE
NEXT
PAGE
CNTL TEST
BUS
EMER
CONT
GX_10_069
CIRCUIT BREAKER - SYSTEM 1/2
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
2/4
P FEEL/RUD LIM 1
P FEEL/RUD LIM 2
PUSHER LOCK CH A
PUSHER LOCK CH B
RUDDER TRIM
SLAT/FLAP CTLR 1
IN
IN
IN
IN
IN
IN
DC 2
DC ESS
BATT
DC ESS
DC ESS
BATT
CB - FLT CONTROLS SYSTEM
STAB TRIM CH 2
STICK PUSHER PWR
STICK SHAKER 1
STICK SHAKER 2
　
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