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CONFIG RUD TRIM
CONFIG STAB TRIM
MACH TRIM FAIL
STAB TRIM
RUD LIMITER FAIL
RUD AUTHORITY HIGH
RUD AUTHORITY LOW
ELEVATOR SPLIT
RUD AUTHORITY SAFE
RUD LIMITER FAULT
STAB TRIM
Indicates both pitch trim
channels are inoperative.
May be result of:
• failure
• both STAB switches
selected OFF
• MASTER DISC switch
pressed for more than 5
RUD AUTHORITY HIGH
Indicates that the rudder
authority available is too high
for the indicated airspeed.
RUD AUTHORITY SAFE
Indicates that rudder authority
is safe in current configuration
and speed.
CONFIG STAB TRIM
Displayed during takeoff, if
stabilizer trim is out of certified
range (green band).
MACH TRIM FAIL
Indicates the mach trim
function has failed due to loss
of mach data information.
RUD LIMITER FAIL
Indicates that the rudder
limiter capability is lost. It may
be accompanied by an
additional rudder authority
caution message.
RUD AUTHORITY LOW
Indicates that the rudder
authority available is low
(rudder limiter failed in low
authority position).
RUD LIMITER FAULT
Indicates that one channel of
the rudder limiter is
inoperative.
“NO TAKEOFF”
CONFIG RUD TRIM
Display during take-off, if
rudder trim is out of certified
range (green band)
“NO TAKEOFF”
CONFIG AIL TRIM
Displayed during take-off, if
aileron trim is out of certified
range (green band).
“NO TAKEOFF”
GX_10_063
ELEVATOR SPLIT
Displayed anytime elevator
split is:
• at or greater than 4 degrees
above 250 knots, or
• 6 degrees below 250 knots.
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
10-66 For Training Purposes Only
Sept 04
PRIMARY/SECONDARY FLIGHT CONTROL EICAS MESSAGES (Cont)
789
STAB CH 1 FAIL
PITCH FEEL FAULT
FCU FAULT
STAB CH 2 FAIL
STAB CH 1 OFF
STAB CH 2 OFF
STAB CH 1 FAIL
STAB CH 2 FAIL
Indicates that channel 1or 2
failed.
FCU FAULT
Indicates that a fault has been
recognized by the flight
control unit (maintenance
action before the next scheduled
check). This message
appears only on the ground.
PITCH FEEL FAULT
Indicates that either pitch feel
is inoperative, or degraded
(force gradient not nominal)
on one or both channels.
STAB CH 1 (2) OFF
Indicates that the affected
pitch trim off switch (center
pedestal) has been selected
to the OFF position.
GX_10_064
For Training Purposes Only
Sept 04
10-67
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
SLAT/FLAP EICAS MESSAGES
GX_10_065
“NO TAKEOFF”
CONFIG SLAT/FLAP
Indicates that the slats are not
out, or flaps are not at the
correct takeoff configuration.
SLAT DRIVE OVHT
FLAP DRIVE OVHT
Indicates that one slat/flap
motor has overheated and
shut down.
SLAT-FLAP BIT
Indicates (on ground only)
that maintenance action is
required prior to the 500-hour
scheduled interval.
SLAT FAIL
FLAP FAIL
Indicates that the affected
actuating system is
inoperative.
SLAT HALFSPD
FLAP
Indicates that the affected
actuating system is operating
at half speed.
HALFSPD
789
CONFIG SLAT/FLAP
SLAT FAULT
FLAP FAULT
SLAT FAIL
FLAP FAIL
SLAT HALFSPD
FLAP
SLAT DRIVE OVHT
FLAP DRIVE OVHT
SLAT-FLAP BIT
HALFSPD
SLAT FAULT
FLAP FAULT
Indicates that the affected
system has shut down and
may be out of the selected
position due to a jam, loss of
power, overheat,etc.
P I LOT T R A I N I N G GU I D E
FLIGHT CONTROLS
10-68 For Training Purposes Only
Sept 04
Spoiler EICAS Messages
789
CONFIG SPOILERS
FLT SPOILERS FAIL
ROLL SPOILERS FAIL
GND LIFT DUMP
FLT SPLR DEPLOYED
SPLR LEVER FAIL
ROLL SELECT
“NO TAKEOFF”
GX_10_066
CONFIG SPOILERS
Displayed during takeoff, if
a spoiler is deployed for
other than roll assistance.
ROLL SPOILERS FAIL
Indicates that roll function for
at least two pairs of MFS is
inoperative.
FLT SPLR DEPLOYED
Indicates flight spoilers
deployed at low altitude,
(below 300 ft. AGL, or when
the throttle quadrant angle is
at high power).
ROLL SELECT
Indicates roll disconnect
　
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