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Figure 11---20---1 COPILOT
CONTROL COLUMN
ROLL DISCONNECT
MECHANISM
UP
ROLL DISCONNECT
HANDLE
PILOT CONTROL
COLUMN
AILERON FORWARD
QUADRANTS
UP
UP
UP
AILERON
FLUTTER
DAMPER
AILERON
PCUs
AILERON
AILERON REAR
QUADRANTS
ARTIFICIAL FEELAND
CENTERING UNIT
TRIM ACTUATOR
AUTOPILOT
SERVO ACTUATOR
AILERON POSITION
TRANSMITTER
AILERON
AILERON
FLUTTER
DAMPER
Vol. 1 11--20--3
FLIGHT CONTROLS
Ailerons REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Ailerons --- Emergency Control
Figure 11---20---2
ROLL DISC
PULL &
TURN
Roll Disconnect Handle
Center Pedestal
Ailerons Glareshield Emergency Control
Figure 11---20---3
ROLL SEL
ROLL SEL (amber) light
comes on to indicate that roll
priority selection is required.
PLT ROLL or CPLT ROLL
Used to select roll priority.
PLT ROLL or CPLT ROLL (green) light
indicates which side has been selected
manually or automatically, for spoileron
control.
Left Glareshield
PLT
ROLL
ROLL SEL
Right Glareshield
CPLT
ROLL
ROLL SEL
Vol. 1 11--20--4
FLIGHT CONTROLS
Ailerons REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
EICAS Flight Control --- Synoptic Page
Figure 11---20---4
Flutter Damper Outlines (white)
Displayed if low fluid is detected in
respective damper.
Flight Controls Page
YAW DAMPER (amber)
Indicates failure of both yaw dampers.
Aileron Position Indicator (white)
Indicates relative position of
respective aileron.
Vol. 1 11--20--5
FLIGHT CONTROLS
Ailerons REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Aileron trim is electrically operated and manually controlled using the trim selector on the
center pedestal. Operation of the aileron trim will cause control wheel rotation.
Aileron Trim Controls
Figure 11---20---5
AIL TRIM
Used to control aileron trim.
Spring loaded to center position.
LWD -- Trims left wing down.
RWD -- Trims right wing down.
Aileron / Rudder Trim Panel
Center Pedestal
NR
TRIM
NL
RUD
L
W
D
R
W
D
AIL TRIM
Aileron Mistrim Flag <1015>
Figure 11---20---6
A
Aileron Mistrim Indicator (yellow)
Indicates that the ailerons are in a
mistrim condition, when the autopilot
is engaged.
Primary Flight Display
Pilot’s and Copilot’s Instrument Panels
Vol. 1 11--20--6
FLIGHT CONTROLS
Ailerons REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Aileron Trim EICAS Indications
Figure 11---20---7
Aileron Trim Pointers (white)
Indicates trim actuator position.
Turns green when in neutral
position on the ground.
Aileron Trim Scale (white)
LWD mark -- Aileron at
maximum left wing down.
RWD mark -- Aileron at
maximum right wing down.
Status Page
AIL
LWD RWD BRT
Flight Controls Page
Vol. 1 11--20--7
FLIGHT CONTROLS
Ailerons REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Spoilerons and Roll Selection --- EICAS Indications <1001>
Figure 11---20---8
SPOILERONS ROLL caution (amber)
Indicates that roll disconnect has been
selected and either no roll priority has
been selected or both roll priorities have
been selected.
PLT or CPLT ROLL CMD advisory (green)
Indicates that pilot or copilot roll authority has
been selected.
SPOILERONS ROLL
Primary Page
Status Page
FLUTTER DAMPER status (white)
Indicates that low fluid level is detected in a
flutter damper. (Refer to the flight controls
synoptic page for the affected flutter damper.)
Vol. 1 11--20--8
FLIGHT CONTROLS
Ailerons REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Trim AIL TRIM DC BUS 2 2 F3
Ailerons
Trim Indication AIL/RUD TRIM
IND
BATTERY
BUS 1 L7
Vol. 1 11--30--1
FLIGHT CONTROLS
Rudder REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. RUDDER
Directional (yaw) control is provided by the rudder and assisted by yaw dampers.
The rudder is hydraulically powered by three power control units (PCUs). The PCUs receive
　
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