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neutral position (to indicate a potential and unwanted control demand).
Note: If the aircraft is on the ground and commencing its takeoff run and one stick is
deactivated, this triggers the takeoff “CONFIG” warning.
GLARESHIELD
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-27-20-30 P 11/28
FCOM 19 AUG 10
(1) SIDE STICK PRIORITY lt
Red arrow light : ‐ comes on in front of the pilot losing authority.
‐ goes out if he has recovered his authority
• if the other pilot releases his TAKEOVER pushbutton prior the priority
condition is latched.
or
• If he has used his takeover push button to cancel a latched priority
situation.
Sidestick priority audio : A “PRIORITY LEFT” or “PRIORITY RIGHT”
audio voice message is given each time priority is taken.
Green CAPT and F/O lights :
When a pilot has taken priority by pressing the takeover pushbutton and the other pilot's
sidestick is not at neutral, the light in front of the pilot with priority lights up. It goes out when the
other pilot returns his stick to the neutral position.
GLARESHIELD
Applicable to:
,
,
MSN,,,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-27-20-30 P 12/28
FCOM 19 AUG 10
(1) SIDE STICK PRIORITY lt
Red arrow light : comes on in front ‐ of the pilot losing authority.
‐ goes out if he has recovered his authority
• if the other pilot releases his TAKEOVER pushbutton prior the priority
condition is latched.
or
• If he has used his takeover push button to cancel a latched priority
situation.
Sidestick priority audio : A “PRIORITY LEFT” or “PRIORITY RIGHT”
audio voice message is given each time priority is taken.
Green CAPT and F/O lights :
‐ Both lights flash when the pilots move both sidesticks simultaneously and neither takes
priority.
‐ When a pilot has taken priority by pressing the takeover pushbutton and the other pilot's
sidestick is not at neutral, the light in front of the pilot with priority lights up. It goes out when
the other pilot returns his stick to the neutral position.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-27-20-30 P 13/28
FCOM 19 AUG 10
OVERHEAD PANEL
Applicable to:
(1) ELAC 1(2) pushbutton
Controls the Elevator and Aileron Control (ELAC) Computer 1(2).
ON : ELAC 1(2) performs the following functions :
‐ Normal pitch and roll, normal LAF
‐ Alternate pitch, alternate LAF
‐ Direct pitch and roll
‐ Abnormal attitude
‐ Aileron droop
‐ Acquisition of autopilot orders.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-27-20-30 P 14/28
FCOM 19 AUG 10
OFF : The corresponding computer is not active. Switching it OFF, then ON, resets the
computer.
FAULT : Comes on amber, along with an ECAM caution :
‐ When a failure is detected
‐ During ELAC power-up test (eight seconds).
Note: The ELAC power-up test occurs when electrical power is turned on, or
after the occurrence of an electrical transient lasting longer than 25 ms.
The FAULT light goes off, when the pilot selects OFF, or at the end of the ELAC
power-up test, if its results are satisfactory.
(2) SEC 1(2)(3) pushbutton
Controls the spoiler and elevator (SEC) computers 1(2)(3).
ON : SEC 1(2)(3) performs the following functions :
‐ Normal roll (by controlling the spoilers)
‐ Speedbrakes and ground spoilers
‐ Alternate pitch (SEC 1 and SEC 2 only)
‐ Direct pitch (SEC 1 and SEC 2 only)
‐ Direct roll
‐ Alternate Load Alleviation Function (LAF)
‐ Abnormal attitude.
OFF : The corresponding computer is not active. Switching it OFF, then on, resets the
computer.
FAULT : Comes on amber, along with an ECAM caution, when a failure is detected.
The FAULT light goes off, when the pilot selects OFF.
(3) FAC 1(2) pb sw
Controls the flight augmentation computer (FAC) 1(2).
ON : Both FACs perform the following functions :
Normal roll (coordinating ‐ turns and damping dutch roll)
‐ Rudder trim
‐ Rudder travel limit
‐ Alternate yaw
　
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