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GF1010_073
After takeoff the amount of rudder travel will be limited as a function of flap retraction or airspeed increasing above 155 knots.
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
RUDDER CONTROL (CONT'D)
Rudder Surface Position Indication
Left and right rudder surface position is displayed by a moving pointer on the EICAS FLIGHT CONTROLS page. A single pointer indicates left and right rudder surface positions.
Scale Pointer Rudder Limit Bug
Filled rudder cross.section directed toward the centre of the scale. It will change color, (green or amber) based on hydraulic pressure availability.
Scale
Arc represents the left and right rudder travel paths.
Indicates the position and status of the rudder limiter.
Control active . bug color is white.
Control inactive . bug color is amber.
Invalid . bug is
removed.
GF1010_013
Rudder Trim
Rudder trim is available by rotating the RUD TRIM control switch on the trim control panel (centre pedestal), in the desired direction. The control provides signals to a trim actuator that repositions the rudder neutral point.
Hydraulic power is necessary to set rudder trim. Rudder trim position is displayed on PRIMARY page, along with the allowable take-off green band.
A“CONFIG RUD TRIM”red warning message is accompanied by a “NO TAKE-OFF”aural warning. It is displayed during the take-off roll if the rudder trim is set outside the allowable take-off range.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
RUDDER CONTROL (CONT'D)
Rudder Trim (Cont’d)
Rudder Trim Switch
Located on the trim control panel (pedestal). Switch must be rotated full left or right to activate the trim. Spring loaded to the centre position.
Pointer
Trim Scales
Rudder trim range for nose left centre and nose
Green Band (take-off)
right indications.
Replaces the centre tick mark. White when not in the green take-off position.
NL . Nose left.
NR . Nose right.
GF1010_015
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
RUDDER CONTROL (CONT'D)
Rudder Control Schematic
RUDDER
PEDALS
ARTIFICAL
FEEL
NO TAKE-OFF
TRIMS RUD
NL NR
NU
AIL
7.2
LWD RWD
ND
STAB RUDDERNL NR
CRS 2
LEGEND
ELEV ELEV
Electrical input Mechanical input Cable input
RUDDER
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
ELEVATOR CONTROL
Longitudinal control is provided by elevators operating in relation to control column displacement and supplemented by a moveable horizontal stabilizer for maintaining longitudinal (pitch) trim. Pilot inputs to the elevator circuit are from the dual control columns which are normally connected through an automatic disconnect mechanism.
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