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OFF : Turbulence Damping function commands are inhibited.
SIDE STICK INDICATIONS ON PFD
Applicable to: ALL
On ground, after first engine start, side stick position indications appear white on both PFDs.
The indication disappears when the aircraft passes from ground to flight.
ECAM F / CTL PAGE
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 15/22
FCOM 19 AUG 10
(1) Spoilers / speed brakes indication
▹􀀃:􀀃Spoiler􀀃not􀀃retracted􀀃(green)􀀃
— : Spoiler retracted (green)
▹􀀃:􀀃Spoiler􀀃fault􀀃deflected􀀃(amber)􀀃
1 : Spoiler fault retracted (amber)
Note: Same indications are displayed on WHEEL page.
(2) Hydraulic system pressure indication
It is normally in green. It becomes amber in case of hydraulic system low pressure
(downstream the leak valves).
(3) PRIM / SEC indication
PRIM and ‐ SEC labels are always displayed in white.
‐ The computer number is normally in green and boxed in grey. The number and box become
amber, in the event of a computer failure.
(4) Ailerons position indication
White scale and green indexes.
The index becomes amber when both (associated) servojacks are not available
(5) Aileron / Elevator actuators indication
G, B and Y are normally displayed in green.
They become amber in case of a hydraulic system low pressure.
It is partially boxed amber in case of electrical failure detected by the PRIM .
(6) Elevator position indication
White scale and green index.
The index becomes amber, when both associated actuators are not available.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 16/22
FCOM 19 AUG 10
(7) Pitch trim position indication
PITCH TRIM
label
: It is normally in white.
It becomes amber in case of THS electrical control loss.
Position
indication
: Varies from 2 ° down to 14 ° up.
It is normally in green.
It becomes amber in case of a B + Y system low pressure.
(8) Yaw control indications
(A) Rudder position indication
It is normally in green.
The rudder symbol becomes amber, in the case of a B + G + Y hydraulic low pressure.
(B) Rudder travel limiter or PTLU indication
It is normally in green.
It becomes amber, when travel Limiters 1 and 2 are faulty.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 17/22
FCOM 19 AUG 10
(C) Rudder trim position
It is normally in blue.
The position varies from -25 to +25 °.
It becomes amber, if the rudder trim systems 1 and 2 are inoperative.
ECAM F / CTL PAGE
Applicable to:
(1) Spoilers / speed brakes indication
▹􀀃:􀀃Spoiler􀀃not􀀃retracted􀀃(green)􀀃
— : Spoiler retracted (green)
▹􀀃:􀀃Spoiler􀀃fault􀀃deflected􀀃(amber)􀀃
1 : Spoiler fault retracted (amber)
Note: Same indications are displayed on WHEEL page.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 18/22
FCOM 19 AUG 10
(2) Hydraulic system pressure indication
It is normally in green. It becomes amber in case of hydraulic system low pressure
(downstream the leak valves).
(3) PRIM / SEC indication
PRIM and ‐ SEC labels are always displayed in white.
‐ The computer number is normally in green and boxed in grey. The number and box become
amber, in the event of a computer failure.
(4) Ailerons position indication
White scale and green indexes.
The index becomes amber when both (associated) servojacks are not available
(5) Aileron / Elevator actuators indication
G, B and Y are normally displayed in green.
They become amber in case of a hydraulic system low pressure.
It is partially boxed amber in case of electrical failure detected by the PRIM .
(6) Elevator position indication
White scale and green index.
The index becomes amber when both associated actuators are not available.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 19/22
　
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