1_ ENGINE area (upper one)
 The ENGINE area is divided in three parts:
 - ENGINE parameters area which gives the engine primary
 indications such as EPR, EGT, Fuel Flow,...
 - SLATS/FLAPS area which gives the actual SLATS/FLAPS position
 and the crew member selection
 - FUEL ON BOARD area which gives the value of the total fuel
 weight on board the aircraft.
 2_ WARNING area (lower one)
 This area is used to display, in real time, the
 WARNING/CAUTION messages.
 In normal aircraft operation (no aircraft or system failure),
 MEMO information is displayed.
 As soon as a failure is detected, the MEMO messages are
 replaced by warning/caution messages.
 In the left part are displayed the primary failures,
 procedures.
 In the right part are displayed the name of the aircraft
 systems affected by the secondary failures resulting from the
 primary one. 

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 (b) System Display (SD) (Ref. Fig. 022) (For further details, Ref. to 31-67-00). The SD symbology is a set of various specific pages. To each main aircraft system corresponds an SD page. Each page is an operational synoptic diagram of the related system, in order to provide the crew with the main system parameters. Each page is displayed either automatically or manually using the related key located on the ECAM control panel. The list of the available A/C system pages are:
 -
Air bleed . . . . . . . . . . . . . . BLEED

 -
Air conditioning. . . . . . . . . . . COND

 -Cabin pressurization. . . . . . . . . CAB PRESS
 -Electrical power supply (AC/DC) . . . ELEC
 -Flight controls . . . . . . . . . . . F/CTL
 -Fuel. . . . . . . . . . . . . . . . . FUEL
 -Hydraulic power . . . . . . . . . . . HYD
 -APU . . . . . . . . . . . . . . . . . APU
 -Engine secondary parameters . . . . . ENGINE
 -Doors and oxygen. . . . . . . . . . . DOOR/OXY
 -Landing gear, wheels, brakes. . . . . WHEEL
 Each page is related to a particular system of the aircraft needing to be monitored like the ENGINE page. (Ref. Fig. 023) A few parameters are monitored on this page as follows: Item (1) Nacelle temperature: the left sketch is related to the left engine. Item (2) Oil temperature Item (3) Oil pressure Item (4) Oil quantity Item (5) Fuel used Item (6) Engine vibration Item (7) Oil clog indication Item (8) Fuel clog indication
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 SD - BLEED Page
 Figure 022 
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 SD - Engine Page
 Figure 023 
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 1
_
 2
_
 3
_
The COND Page: (Ref. Fig. 024) Item (1) Zone controller mode message Item (2) Cabin and cockpit temperatures Item (3) Zone ducts temperatures Item (4) Hot air and valve indication Item (5) Zone trim air valve status Item (6) FAN status indication
 (Ref. Fig. 025) Item (1) Aft cargo compartment temperature Item (2) Aft cargo downstream isolation valve position Item (3) Aft cargo duct temperature Item (4) Upstream isolation valve position Item (5) Hot air regulating valve position Item (6) Trim air valve position
The CAB PRESS Page (Ref. Fig. 026) Item 1: Cabin differential pressure Item 2: Landing field elevation indication Item 3: Landing field elevation mode Item 4: Cabin vertical speed Item 5: Cabin altitude Item 6: Manual selection indication Item 7: Safety valve Item 8: Safety valve status Item 9: Active system indication Item 10: PACK 2 indication Item 11: Outflow valve position Item 12: EXTRACT message Item 13: Overboard outlet valve Item 14: BLOWER/VENT messages Item 15: Overboard inlet valve Item 16: PACK 1 indication Item 17: INLET message
 Item 18: GND COOL Indication
The ELEC Page (Ref. Fig. 027) Item 1: BAT busbar status Item 2: BAT charge indication Item 3: BAT status voltage/current Item 4: DC ESS busbar status Item 5: DC2 busbar status Item 6: ESS TR contactor indication
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 SD - AIR COND Page
 Figure 024 
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