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RAT OUT Ram air turbine is not in stowed position
PARK BRK Parking brake applied
APU AVAIL APU is running and available
APU BLEED APU bleed is selected ON
RAM AIR ON RAM AIR button is selected ON
MAN LDG ELEV Landing elevation selector is not in AUTO position
ENG A.ICE Engine anti-icing is activated
WING A.ICE Wing anti-icing is activated
LDG LT Landing lights are on
GPWS FLAP 3 LDG FLAP 3 is selected on GPWS panel
GPWS FLAP OFF GPWS Flaps alerts are inhibited
T.O INHIBIT Some messages are automatically inhibited during takeoff
LDG INHIBIT Some messages are automatically inhibited during landing
A319/320/321
Systems Manual
Phoenix Simulation Software P 27
REV 01 SEQ 001 ENGINE / WARNING DISPLAY
Takeoff Memo
A takeoff memo is automatically displayed on the left side of message
area 2 minutes after second engine start. Pressing T.O CONFIG button on
ECAM control panel also displays the takeoff memo.
Takeoff Memo contains a checklist of items required prior to takeoff.
Uncompleted items are shown in Blue color. Completed items are displayed
in Green color.
Last item, “T.O CONFIG...TEST” requires a push of T.O CONFIG button on
ECAM control panel. This push simulates application of takeoff power and
will generate appropriate warnings if something is not properly congured.
Takeoff memo disappears at application of takeoff power. During takeoff, a
magenta “T.O INHIBIT” memo is displayed.
Landing Memo
Landing memo is automatically displayed prior to landing, below 1500 feet
when gear down, or below 800 feet with gear up. Landing memo disappears
at touchdown.
The FLAPS...FULL or FLAPS...CONF 3 item depends on selection of
GPWS LDG FLAP 3 button and requires corresponding ap selection.
During landing, a manenta “LDG INHIBIT” message is displayed.
A319/320/321
Systems Manual
Phoenix Simulation Software P 28
REV 01 SEQ 001 SYSTEM DISPLAY
General
System display (SD), the lower of ECAM displays, has multiple pages dedicated to different aircraft systems. The pages include:
• BLEED (air bleed system)
• PRESS (pressurization)
• ELEC (electrical)
• HYD (hydraulic)
• ENGINE
• FUEL
• APU (auxiliary power unit)
• COND (air conditioning)
• DOOR/OXY (doors / oxygen)
• WHEEL (landing gear)
• F/CTL (ight controls)
• CRUISE (common reference data)
Individual pages are described in detail in chapters dedicated to corresponding systems.
SD Page selection
The SD will automatically display a page corresponding to current ight phase or for monitoring of certain systems. Manual selection
can also be performed using ECAM control panel. Manual selection overrides automatic page sequencing.
Phase of Flight
The SD automatically displays specic pages as next phase of ight becomes active:
Power up DOOR/OXY
1st engine start WHEEL
T/O power ENGINE
1500 ft CRUISE
Gear down WHEEL
Engine shutdown DOOR/OXY
System monitoring
The SD automatically displays appropriate page for monitoring of a system status:
• When APU Master button switched ON, SD will display APU page. It is removed 1.5 minutes after APU is running.
• During engine start, ENGINE page is automatically displayed.
• On the ground, before takeoff, if control stick or rudder pedals are moved, F/CTL page will be displayed to allow
checking the operation of control surfaces. Page is removed 20 seconds after controls are returned to neutral.
• During landing gear retraction or extension, WHEEL page is displayed.
Manual page selection
Any page except CRUISE can be manually displayed by pushing corresponding button on ECAM control panel. Selected button
is lighted, and selection overrides automatic page switching. To return to automatic operation, deselect the page by pushing
lighted button again.
ECAM control panel,
BLEED page selected
SD BLEED page
A319/320/321
Systems Manual
Phoenix Simulation Software P 29
REV 01 SEQ 001 SYSTEM DISPLAY
CRUISE page
The CRUISE page is automatically displayed in ight, above 1500 feet when landing gear is up. The cruise page displays most
important information gathered from different aircraft systems. CRUISE page cannot be manually called via ECAM control panel.
Fuel used per engine
Oil quantity
Cabin differential
pressure
Cabin zone
temperatures
Engine N1 vibration
Engine N2 vibration
Landing elevation
Cabin climb rate
Cabin altitude
Permanent data display
　
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本文鏈接地址：PSS A319/A320/A321 Systems Manual 系統手冊(9)