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(2) ECAM/ND transfer selector switch
Transfers the system/status display to either the captain's or the first officer's NDU.
Note: If both ECAM DUs (E/WD and SD) fail, the flight crew can use this switch to
transfer the E/W display to either navigation display.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
ECAM CONTROLS
A330/A340 FLEET DSC-31-30 P 4/4
FCOM 19 AUG 10
ATTENTION GETTERS
Applicable to: ALL
(1) MASTER WARN lights
‐ Flash red for level 3 warning.
‐ Accompanied by an aural warning (continuous repetitive chime, specific sounds or synthetic
voice).
(2) MASTER CAUT lights
‐ Light up steady amber for a level 2 caution.
‐ Accompanied by a single chime.
These lights go out when :
‐ One pilot presses the light (except for some red warnings, such as the overspeed and stall
warnings).
‐ The warning/caution situation is over.
‐ The pilot presses the CLR pushbutton on the ECAM control panel (except for some red
warnings, such as the overspeed and stall warnings).
‐ The pilot presses the EMER CANC pushbutton on the ECAM control panel.
The aural warnings cease when :
‐ One pilot presses the MASTER WARN light (except for some red warnings, such as the
overspeed and stall warnings).
‐ The warning situation is over.
‐ The pilot presses the EMER CANC pushbutton on the ECAM control panel.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON PFD
A330/A340 FLEET DSC-31-40 P 1/48
FCOM 19 AUG 10
TAIL STRIKE PITCH LIMIT INDICATOR
Applicable to: ALL
(1) Tail Strike Pitch Limit
The pitch limit indicates the maximum pitch attitude to avoid the tail strike risk at takeoff and
landing. During takeoff, the indication progresses from the pitch limit value with main landing
gear compressed, to the pitch limit value with main landing gear extended. The indication is
removed when the tail strike risk disappears.
During landing, the indication is a fixed value corresponding to the main landing gear
compressed. The indication appears at 400 ft radio height.
GENERAL
Applicable to:
The Primary Flight Display (PFD) provides the following information to the flight crew :
• Attitude and Guidance
• Airspeed
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON PFD
A330/A340 FLEET DSC-31-40 P 2/48
FCOM 19 AUG 10
• Altitude (baro and radio) and vertical speed
• Heading and Track
• FMGS modes (Flight Mode Annunciator)
• Vertical and Lateral Deviations
• Radio navigation information (ILS, DME).
The FWC monitors such main parameters as : Attitude, heading, and altitude. Also Refer to
DSC-31-40 FLAGS AND MESSAGES DISPLAYED ON PFD.
Note: A grey background appears on the speed, the heading vertical speed, and the altitude
speed scales of the PFD. If the Primary Flight Display (PFD) Unit temperature exceeds a
defined threshold, the grey background disappears, in order to limit power consumption and
prevent a DU overheat. Any additional increase in temperature will lead to a complete cut
off of the power supply to this display unit.
GENERAL
Applicable to: ,
The Primary Flight Display (PFD) provides the following information to the flight crew :
• Attitude and Guidance
• Airspeed
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON PFD
A330/A340 FLEET DSC-31-40 P 3/48
FCOM 19 AUG 10
• Altitude (baro and radio) and vertical speed
• Heading and Track
• FMGS modes (Flight Mode Annunciator)
• Vertical and Lateral Deviations
• Radio navigation information (ILS, DME).
The FWC monitors such main parameters as : Attitude, heading, and altitude. Also Refer to
DSC-31-40 FLAGS AND MESSAGES DISPLAYED ON PFD.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON PFD
A330/A340 FLEET DSC-31-40 P 4/48
FCOM 19 AUG 10
SPECIFIC GROUND INDICATIONS
Applicable to: ALL
(1) Sidestick order indication (white)
This is displayed, as soon as one engine is started.
It indicates the total of the pilot's and copilot's sidestick orders (shown here as left wing down,
pitch up).
(2) Max Sidestick Deflection (white)
This is displayed, as soon as one engine is started.
(3) Ground Roll Guidance Command Bar (green)
This symbol is displayed when the aircraft is on the ground, or below 30 ft radio altitude,
　
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