BOMBARDIER BD-100-1A10, Operating Manual

Page: 302 / 544

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 redun-
dancy has occurred in the rudder limiter system
The rudder travel limiter will continue to func-
tion
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 con-
trol wheel(s) separately will result in a SPOIL-
ERS 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 sys-
tem. The stabilizer trim will continue to function
STALL PROTECT
FAULT
TO/LAND
The Stall Protection Computer has automati-
cally 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
elevator. Autopilot will disengage and not re-
engage
ROLL DISCONNECT
The roll disconnect has been selected. The
pilot’s control wheel moves the aileron. The
autopilot will disengage and not re-engage
ROLL SPOILERS
OFF
The roll spoilers have been turned off and the
roll disconnect has been activated
RUD LIMITER IN
TEST
The rudder travel limiter system is conducting
the manually activated system test
SEC STAB TRIM ON
The secondary channel of the horizontal stabi-
lizer trim system is selected. The autopilot will
be inoperative
STAB TRIM OFF
The STAB TRIM switch is in the off position.
The autopilot will be inoperative
STALL PUSHER OFF
The stall pusher has been manually deacti-
vated