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Position Pointer/digital readout
Moves vertically (in 0.1 units) along the scale to indicate the trim setting.
The pointer/digital readout will turn white with a "STAB TRIM" caution message or "CONFIG STAB TRIM"
warning message.
GF1010_028
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 TAKE-OFF GREEN BAND .
Between 4.5 and 11 units Replaces the 7 and 10.5 marks
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.
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
STABILIZER TRIM (CONT'D)
SPLRS/STAB In Test
An advisory message “SPLRS/STAB IN TEST”will be displayed when the spoilers and stab trim systems are performing self-test 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.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
FLIGHT CONTROL INVALID DATA DISPLAYS
Flight Control Synoptic Page
INVALID SLAT INVALID
SPOILER POSITION
VECTOR
AILERON SURFACE HYDRAULIC PRESSURE NOT AVAILABLE
ELEVATOR POSITION INVALID
Invalid data Flight Control Primary Page
CONTROL SURFACE DISPLAYS:
FLAPS
SLATS
SPOILERS TRIM DISPLAYS:
AILERON
RUDDER
STABILIZER
Invalid data
GF1010_031 GF1010_010
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
PRIMARY/SECONDARY FLIGHT CONTROL EICAS MESSAGES
"NO TAKE-OFF"
"NO TAKE-OFF"
CONFIG RUD TRIM CONFIG AIL TRIM
Displayed during Displayed during
take-off, if rudder trim is take-off, if rudder trim is out of certified range out of certified range (green band). (green band).
CONFIG STAB TRIM
STAB TRIM
Displayed during take-off, 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
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