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Both sidesticks are
moved simultaneously Every 5 s One sidestick deactivated
(1) All aural warnings may be cancelled by pressing either :
The EMER CANC pushbutton on the ‐ ECAM control panel, or
‐ The MASTER WARN light, except for some warnings like OVERSPEED, or L/G NOT DOWN, or CAVALRY
CHARGE, if AP disconnection is due to a VMO/MMO warning.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
ECAM DESCRIPTION
Intentionally left blank
A330/A340 FLEET DSC-31-10 P 10/10
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON E/WD
A330/A340 FLEET DSC-31-15 P 1/8
FCOM 19 AUG 10
GENERAL
Applicable to:
The E/WD appears on the upper ECAM Display Unit (DU).
The upper ‐ part of this DU displays :
• Engine parameters (Refer to DSC-70-92-A ECAM - PRIMARY PARAMETER),
• Fuel on board (FOB) (Refer to DSC-28-20 ECAM UPPER DISPLAY),
• Position of slats and flaps (Refer to DSC-27-20-30 ECAM F / CTL PAGE).
‐ The lower part of this DU displays messages generated by the FWC :
• Warning and caution messages when a failure occurs,
• Memos when there is no failure.
The lower part, which is dedicated to ECAM messages, is divided into two parts of several lines
each.
Left part : ‐ Primary or independent warnings and cautions, or
‐ Memo information.
Right part : ‐ Title of system affected by a primary or independent warning or caution in case
of overflow on the left part, or
‐ Secondary failure, or
‐ Memo, or
‐ Special lines (such as “AP OFF”, “LAND ASAP”).
As soon as the FWC detects a failure, and if no flight phase inhibition is active, the E/WD displays
the title of the failure and the actions to be taken.
The action line automatically clears when the flight crew has executed the required action.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON E/WD
A330/A340 FLEET DSC-31-15 P 2/8
FCOM 19 AUG 10
Note: Certain actions will not disappear after execution.
GENERAL
Applicable to: ,
The E/WD appears on the upper ECAM Display Unit (DU).
The upper ‐ part of this DU displays :
• Engine parameters (Refer to DSC-70-91-A PRIMARY PARAMETER),
• Fuel on board (FOB) (Refer to DSC-28-20 ECAM UPPER DISPLAY),
• Position of slats and flaps (Refer to DSC-27-20-30 ECAM F / CTL PAGE).
‐ The lower part of this DU displays messages generated by the FWC :
• Warning and caution messages when a failure occurs,
• Memos when there is no failure.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON E/WD
A330/A340 FLEET DSC-31-15 P 3/8
FCOM 19 AUG 10
The lower part, which is dedicated to ECAM messages, is divided into two parts of several lines
each.
Left part : ‐ Primary or independent warnings and cautions, or
‐ Memo information.
Right part : ‐ Title of system affected by a primary or independent warning or caution in case
of overflow on the left part, or
‐ Secondary failure, or
‐ Memo, or
‐ Special lines (such as “AP OFF”, “LAND ASAP”).
As soon as the FWC detects a failure, and if no flight phase inhibition is active, the E/WD displays
the title of the failure and the actions to be taken.
The action line automatically clears when the flight crew has executed the required action.
Note: Certain actions will not disappear after execution.
INDEPENDENT FAILURE
Applicable to: ALL
If there are too many ECAM messages for the amount of space available in the lower part of
the E/WD, a green arrow appears at the bottom of the display, pointing down to show that the
information has overflowed off the screen. The pilot can scroll down to view additional messages
by pushing the CLR pushbutton on the ECAM control panel (on the pedestal, just below the lower
ECAM DU).
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON E/WD
A330/A340 FLEET DSC-31-15 P 4/8
FCOM 19 AUG 10
PRIMARY AND SECONDARY FAILURES
Applicable to: ALL
The ECAM DU displays a primary failure as a boxed title.
It identifies a secondary failure by putting a star in front of the title of the affected system.
Note: The DU displays the overflow symbol, if primary or secondary failures overflow. In case of
ECAM SINGLE DISPLAY, the secondary failures are inhibited.
FLIGHT PHASES
Applicable to:
The FWC divides its functions according to these ten flight phases :
　
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