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message or "CONFIG STAB TRIM"
warning message.
Position Pointer/digital readout
Moves vertically (in 0.1 units)
along the scale to indicate the trim
setting.
NU TRIMS
ND
STAB
NU TRIMS
ND
STAB
3.5
7.2
GF1010_028
NU
ND
VERTICAL SCALE LONG TICK MARKS SHORT TICK MARKS
Between 0 units (bottom) and
14 units (top)
0 and 14 unit positions 3.5, 7 and 10.5 units
GREEN BAND TAKEOFF
GREEN BAND −
Between 4.5 and 11 units Replaces the 7 and 10.5 marks
FLIGHT CONTROLS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
10−10−22
STABILIZER TRIM (CONT'D)
Stabilizer In Motion Aural Warning
The stabilizer in motion aural clacker signals operation of the horizontal stabilizer under the
following conditions:
· Operation of more than 3 seconds at a rate used for manual trim (0.2 degrees per second or
greater).
OR
· More than 6 seconds at a low rate above the mach trim rate (.08 degrees per second or
greater).
CONFIGURATION WARNING
Horizontal stabilizer trim position and condition is continuously monitored and any fault detected is
displayed on EICAS.
SPLRS/STAB In Test
An advisory message “SPLRS/STAB IN TEST” will be displayed when the spoilers and stab trim
systems are performing selftest
once hydraulics are applied. The horizontal stabilizer system is
inoperative through the duration (approximately 20 seconds) of the test. Refer to the EICAS
MESSAGES in the spoiler section of flight controls for the message display.
FLIGHT CONTROLS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
10−10−23
FLIGHT CONTROL INVALID DATA DISPLAYS
FLIGHT CONTROLS
AILERON
POSITION
INVALID
RUDDER/POSITION
INVALID
ELEVATOR POSITION
INVALID
Invalid data
SLAT INVALID
FLAP INVALID
SPOILER INVALID
AILERON SURFACE
HYDRAULIC PRESSURE
NOT AVAILABLE
Flight Control Synoptic Page
SPOILER POSITION
VECTOR
GF1010_010
SLAT
FLAP − −
− − −
ELEV
AIL
ELEV
AIL
Flight Control Primary Page
TRIM DISPLAYS:
AILERON
RUDDER
STABILIZER
Invalid data
CONTROL SURFACE
DISPLAYS:
FLAPS
SLATS
SPOILERS
GF1010_031
ND
STAB
NU
NL RUDDER
LWD RWD
NR
TRIMS
AIL
− −
− −
FLIGHT CONTROLS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
10−10−24
PRIMARY/SECONDARY FLIGHT CONTROL EICAS MESSAGES
CONFIG RUD TRIM
Displayed during
takeoff,
if rudder trim is
out of certified range
(green band).
CONFIG AIL TRIM
Displayed during
takeoff,
if rudder trim is
out of certified range
(green band).
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 switching
capability is lost. It may
be accompanied by an
additional rudder
authority caution
message.
LOW
Indicates that the rudder
authority available is low
(rudder limiter failed in
low authority position).
RUD AUTHORITY
RUD AUTHORITY SAFE
Indicates that rudder
authority is safe in current
configuration and speed.
RUD LIMITER FAULT
Indicates that one
channel of the rudder
limiter is inoperative.
ELEVATOR SPLIT
Displayed anytime elevator
split is:
At or greater than 4 degrees
above 250 knots, or
6 degrees below 250 knots.
STAB TRIM
Indicates both pitch trim
channels are inoperative.
Failure
Both STAB switches
May be result of:
MASTER DISC switch
selected OFF, or
pressed for more than 5
seconds.
"NO TAKEOFF"
"NO TAKEOFF"
"NO TAKEOFF"
CONFIG AIL TRIM
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
GF1010_032
FLIGHT CONTROLS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
　
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