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AILERON CONTROL (CONT'D)
Aileron Surface Position Indication
Left and right aileron positions are displayed by a moving pointer on the EICAS flight controls page. Separate pointers indicate the aileron surface position on each wing.
Scale Pointer
Unfilled triangle moves vertically
Surface Outline
The surface outline has no movement. It will change color, (magenta, green or amber) based on electrical power (ie: battery only or all busses powered) and hydraulic pressure availability.
Scale
Indicates the full range available for aileron up and down travel.
GF1010_007a
SCALE LONG TICK MARKS SHORT TICK MARKS
Left side .25° (top) at top and bottom at 0°
+21.5° (bottom)
Right side +25° (top) at top and bottom at 0°
.21.5° (bottom)
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
AILERON CONTROL (CONT'D)
Aileron Trim
Aileron trim is accomplished by selecting the AIL TRIM switches on the trim control panel (pedestal) in the desired direction. Actuating both switches provides arming and direction signals to reposition the ailerons through the use of a trim actuator. Hydraulic power is necessary to set aileron trim. Aileron trim position is displayed on PRIMARY page, along with the allowable take-off green band.
A“CONFIG AIL TRIM”red warning message is accompanied by a “NO TAKE-OFF”aural warning. It is displayed during the take-off roll if the aileron trim is set outside the allowable take-off range.
Aileron Trim Switch
Located on the trim control panel (centre pedestal). Spring loaded split switches requires both to be selected in the same direction. Push both switches full left or right to activate the trim.
Trim Scales
Aileron trim range for left wing down, centre and right wing down indications.
LWD . Left wing down.RWD
Pointer
Pivots about the centre dot and indicates the trim setting.
Green Band (take-off)
Replaces the centre tick mark. White if it is not in the green band.
GF1010_009
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
AILERON CONTROL (CONT'D)
Aileron Control Schematic
ROLL DISCONNECT SWITCH
Electrical input Mechanical input Cable input
GF1010_011
Trim motor
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
RUDDER CONTROL
Directional control about the yaw axis is provided by the rudder control system. The rudder is hydraulically powered through displacement of either pilot’s rudder pedals and controlled via control rods, cable runs and quadrants.
Rudder Control General Arrangement
RUDDER
POWER CONTROL UNIT (PCU)PEDAL
RUDDER TRAVEL LIMITER ACTUATOR
FORWARD
QUADRANT SUMMING
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