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‐ or the STATUS page.
SYSTEM PAGES
Applicable to:
The lower ECAM DU can display 14 system pages (For description see relevant FCOM chapter) :
‐ ENGINE (Secondary engine parameters)
‐ BLEED (Air bleed)
‐ CAB PRESS (Cabin pressurization)
‐ ELEC AC (AC Electrical power)
‐ ELEC DC (DC Electrical power)
‐ HYD (Hydraulic)
‐ C/B (Circuit Breakers)
‐ APU (Auxiliary Power Unit)
‐ COND (Air conditioning)
‐ DOOR/OXY (Doors/oxygen)
‐ WHEEL (Landing Gear, Braking, ground spoilers, ...)
‐ F/CTL (Flight Controls)
‐ FUEL (Fuel)
‐ CRUISE (Cruise)
The pilot may manually call up a system page for display on the lower ECAM DU, or the system may
automatically display a page.
‐ Manual :
• The pilot can use the pushbutton on the ECAM control panel to call up any system page, except
the CRUISE page, for display at any time.
• The corresponding pushbutton on the ECAM control panel lights up.
• A failure-related display automatically replaces a page the pilot has manually called up.
‐ Automatic, related to a failure :
• The relevant system page automatically appears, as soon as any fault or malfunction triggers a
caution or warning message.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON SD
A330/A340 FLEET DSC-31-20 P 2/10
FCOM 19 AUG 10
‐ Automatic, advisory :
• The relevant system page automatically appears, when a parameter drifts out of its normal
range.
• The value (shown in green) pulses, as long as it is outside its limits.
• The advisory mode is inhibited in some flight phases.
Note: If an advisory is triggered when the ECAM is in the single-display configuration, an
advisory message appears on the upper part of the E/WD, and the associated key on
ECAM control panel flashes to identify the appropriate system page.
‐ Automatic, flight phase mode
• If no other mode is engaged, the SD displays the system page related to the present flight
phase, as shown in the following diagram.
• Phase 2 : The F/CTL page replaces the WHEEL page for 20 s, when either pilot moves his
sidestick (more than 3 ° in pitch or roll), or when the rudder pedal deflection is more than 22 °.
• The APU page appears, when the APU MASTER switch is ON. It disappears when APU RPM
has been above 95 % for 10 s, or when the APU MASTER switch is switched OFF.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON SD
A330/A340 FLEET DSC-31-20 P 3/10
FCOM 19 AUG 10
• The ENGINE page appears at the beginning of the start sequence, or when a pilot selects
“CRANK”. It disappears at the end of the start sequence.
For a description of the ENGINE and AIR indications that appear, when the SD is displaying the
CRUISE page, see the relevant FCOM chapter.
SYSTEM PAGES
Applicable to: ,
The lower ECAM DU can display 14 system pages (For description see relevant FCOM chapter) :
ENGINE ‐ (Secondary engine parameters)
‐ BLEED (Air bleed)
‐ CAB PRESS (Cabin pressurization)
‐ ELEC AC (AC Electrical power)
‐ ELEC DC (DC Electrical power)
‐ HYD (Hydraulic)
‐ C/B (Circuit Breakers)
‐ APU (Auxiliary Power Unit)
‐ COND (Air conditioning)
‐ DOOR/OXY (Doors/oxygen)
‐ WHEEL (Landing Gear, Braking, ground spoilers, ...)
‐ F/CTL (Flight Controls)
‐ FUEL (Fuel)
‐ CRUISE (Cruise)
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON SD
A330/A340 FLEET DSC-31-20 P 4/10
FCOM 19 AUG 10
The pilot may manually call up a system page for display on the lower ECAM DU, or the system may
automatically display a page.
‐ Manual :
• The pilot can use the pushbutton on the ECAM control panel to call up any system page, except
the CRUISE page, for display at any time.
• The corresponding pushbutton on the ECAM control panel lights up.
• A failure-related display automatically replaces a page the pilot has manually called up.
‐ Automatic, related to a failure :
• The relevant system page automatically appears, as soon as any fault or malfunction triggers a
caution or warning message.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
INDICATIONS ON SD
A330/A340 FLEET DSC-31-20 P 5/10
FCOM 19 AUG 10
‐ Automatic, advisory :
• The relevant system page automatically appears, when a parameter drifts out of its normal
range.
• The value (shown in green) pulses, as long as it is outside its limits.
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 3(59)
