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by the “CONFIGURATION” voice warning.
“Configuration”
PITCH DISCONNECT Pitch disconnect has occurred on the ground
with throttles at or above CLB
ROLL DISCONNECT Roll disconnect has occurred on the ground
with throttles at or above CLB
ELEVATOR SPLIT
The elevator has a split of greater than 7.5°.
The split may be caused by maneuvering with
the elevator disconnected
FLAPS FAIL TO
The flap system has shutdown due to a failure.
The flaps are not resettable
FLAPS FAULT TO
The flaps are operating in a degraded mode.
The fault may be resettable in some conditions,
by movement of the flap selector handle
FLAPS NORM
PRESS LOW TO/LAND
The flaps normal hydraulic pressure is low.
This will be accompanied by a FLAPS FAULT
CAS. Alternate pressure may be available
FLT SPOILERS
DEPLOY
The flight spoilers are deployed below 500 feet
(FAA), {800 ft JAA} or the flight spoilers are
deployed and the throttles are at CLB or above
FLT SPOILERS FAIL All flight spoilers have failed
FLT SPOILERS
FAULT TO
Either the inboard or outboard spoilers have
failed
GND SPLRS NOT
ARMED
The ground spoilers are not armed and not
selected OFF
FLIGHT CONTROLS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 10-02-19
EICAS MESSAGES (Cont)
MESSAGE INHIBITS MEANING
AURAL
WARNING
GND SPOILERS FAIL The ground spoilers have failed
MACH TRIM FAIL TO/LAND The Mach trim has failed
PRI STAB TRIM FAIL The stabilizer trim has failed. Mach trim, flap
and spoiler config trim inoperative
ROLL SPOILERS
FAIL
Roll assist function has failed but flight and
ground spoilers have not. Roll control forces
will be higher
ROLL SPOILERS
FAULT
Either the inboard or outboard roll spoilers
have failed. Roll control forces will be higher
ROLL SPOILERS
OFF
The roll spoilers have been turned off with the
ROLL DISC not activated
RUDDER LIMITER
FAIL The rudder limiter has failed
SEC STAB TRIM
FAIL
The secondary stabilizer trim has failed. This
message should not be displayed unless the
primary stabilizer trim has already failed
SPOILERS FAIL
The spoilers have failed. If the spoilers were
deployed, they will retract down to a float position.
The spoilers will not float up.
SPOILERS FAULT
One or more of the spoiler panels have failed
or one or more of the ground spoilers is up prior
to touchdown
STALL PROTECT
FAIL
The stall protection has a failure in either channel
A or B, or the pusher or AOA sensor has
failed, or a miscompare has been detected
between essential inputs or essential inputs are
unavailable
STALL PUSHER OFF
The control wheel master switch button has
been depressed for at least ten seconds or a
stall protection system failure has occurred that
has inhibited operation of the stall pusher
FLAPS FAULT TO
There is a fault in the flap system. The flaps
should operate normally
FLAPS RATE LOW TO/LAND
The flap extension and retraction rates are
slower than normal. This message will illuminate
when the right engine is shutdown, or if
the engine driven pump is shutdown
FLIGHT CONTROLS
Volume 2 Flight Crew Operating Manual Sep 13/2004
10-02-20 CSP 100-6 REV 1
EICAS MESSAGES (Cont)
MESSAGE INHIBITS MEANING
AURAL
WARNING
RUDDER LIMITER
FAULT TO/LAND
A minor failure resulting in the loss of redundancy
has occurred in the rudder limiter system
The rudder travel limiter will continue to function
SPOILERS FAULT TO/LAND
There is a fault in the spoiler system that does
not affect spoiler operation. Selecting the roll
disconnect on the ground and moving the control
wheel(s) separately will result in a SPOILERS
FAULT message. If this occurs, removing
all power from the aircraft and re-powering will
cause the message to clear
STAB TRIM FAULT TO/LAND
A minor failure has occurred causing a loss of
redundancy in the horizontal stabilizer trim system.
The stabilizer trim will continue to function
STALL PROTECT
FAULT TO/LAND
The Stall Protection Computer has automatically
reverted to settings for flaps 30
L (R) STALL
SHAKER FAIL TO/LAND The respective stall shaker has failed
GND SPOILERS OFF The ground spoilers are selected OFF
PITCH DISCONNECT
The pitch disconnect has been selected. The
pilots control column moves the left elevator.
The copilot’s control column moves the right
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