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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.
(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.
(D) NORM CTL message
It appears in amber, when the normal rudder command is lost.
The rudder is then controlled by the Backup Control Module.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 20/22
FCOM 19 AUG 10
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.
(2) Hydraulic system pressure indication
It is normally in green. It becomes amber in case of hydraulic system low pressure
(downstream the leak valves).
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 21/22
FCOM 19 AUG 10
(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.
(7) Pitch trim position indication
PITCH TRIM
label
: It is normally in white.
It becomes amber in case of THS electrical control loss.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-27-20-30 P 22/22
FCOM 19 AUG 10
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.
(C) Rudder trim position
It is normally in blue.
The position varies from -29.2 ° to +29.2 °.
It becomes amber, if the rudder trim systems 1 and 2 are inoperative.
(D) NORM CTL message
It appears in amber, when the normal rudder command is lost.
The rudder is then controlled by the Backup Control Module.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-27-20-40 P 1/10
FCOM 19 AUG 10
WARNINGS AND CAUTIONS
Applicable to:
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
CONFIG.
• SPD BRK NOT RETRACTED or
• PITCH TRIM NOT IN TO RANGE (-7 °, -1 °)
• RUD TRIM NOT IN TO RANGE (± 3 °)
aircraft not in TO configuration when thrust levers
are set at TO or Flex TO, or when pressing TO
CONFIG. pb.
CRC MASTER
WARN 5, 6, 7, 8
PITCH TRIM/MCDU/CG DISAGREE
Disagreement between the real pitch trim value
　
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