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 - or warning/caution messages, giving the title of the failure and the corresponding procedures/actions to be performed.
 (b) Lower display unit
R  (Ref. Fig. 008) In normal operation, the display unit will present :
 1 either an A/C system synoptic diagram, corresponding to the
_ current phase of flight or to the crew manual selection, or to the caution/ warning that is being shown to the crew eventually ;
 2 or status messages, i.e. :
_
 -
an operational summary of the aircraft condition,

 -
an explanation of possible autoland capability downgrading,

 -indications of the aircraft status following all failures except those that do not affect the flight,
 -general contents, limitations (speed, altitude), peculiar or
 emergency postponable procedures, information, etc. These STATUS messages will appear once the crew has cleared all the pages correponding to the current warning/caution, or upon manual call. At last, the two bottom lines are reserved for the display of A/C parameters such as TAT, SAT, A/C Gross weight.
R (3) EIS reconfigurations
R  (Ref. Fig. 009) The selected architecture offers a large versatility thanks to several redundancies :
 -DMC 3 can replace DMC 1 or DMC 2,
 -transfers between PFD and ND images are available,
 -upper ECAM DU image (Engines and Memo/Warning) can be transferred on lower ECAM DU which is normally dedicated to systems/status display,
 -Upper or lower ECAM DU image can be transferred on CAPT or F/O ND,
 -the two FWCs and the two SDACs are identical and are configured in such a way that all the master warnings and cautions are still operative in case of one FWC and/or SDAC failure.
 1EFF : ALL 1 31-00-00Page 17 1 1 Aug 01/05 1 1 1CES 1

 Indicating/Recording System-EIS - DUs Reconfiguration R Figure 009
R 1EFF : ALL 1 31-00-00Page 18 1 1 Aug 01/05 1 1 1CES 1

 INSTRUMENTS AND CONTROL PANELS - MAINTENANCE PRACTICES
______________________________________________________
 TASK 31-10-00-700-001
 Test Program after Removal/Installation of a VU panel
 1. Reason for the Job
__________________
 Do the tests necessary to make sure that all the primary functions are
 operational after removal/installation of VU panel.
 It is possible that your version of the panel does not have all of these functions. Do only the tests that are applicable to your version of the panel.
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
21-21-00-710-001 Operational Test of the Cabin Recirculation Fans 14HG and 15HG. 21-26-00-710-002 Operational Check of Override Function (BLOWER and EXTRACT)
 21-27-00-710-001 Operational Check of Fault Warning
R  21-31-00-710-003 Operational Test of Manual Mode Selection and Manual
R  Mode Pressure Control and Functional Test of Manual
R Mode Cabin Altitude/Outflow Valve Position Indication 21-31-00-710-004 Operational Test of the Outflow Valve Closing in Ditching Configuration 21-43-00-710-002 Operational Test of the FWD Cargo Compartment Heating System 21-51-00-710-002 Operational Test of the Flow Control and Indicating System 21-51-00-710-003 Operational Test of the Flow Control Valves Closing 21-55-00-710-001 Operational Test of the Emergency Ram-Air Inlet 21-63-00-720-001 Functional Test of the Cockpit and Cabin Temperature Control without CFDS/MCDU. 22-60-00-710-002 Operational Test of the Automatic Change-Over Function
R  22-70-00-610-008 Upload the FM Data 22-96-00-710-001 Operational Test of the AFS 22-97-00-710-001 Operational Test of the LAND CAT III Capability
 1EFF : ALL 1 31-10-00Page 201 1 1 Nov 01/04 1 1 1CES 1

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-33-00-710-002

23-36-00-710-001 23-36-00-710-002 23-42-00-710-001 23-44-00-700-001
23-51-00-710-001 23-71-00-710-001 23-71-00-720-002 23-73-00-710-003 23-73-00-710-004
R  23-73-00-710-006 23-73-00-710-017 23-73-00-710-021 23-73-00-710-026 24-21-00-710-040 24-21-00-710-042 24-22-00-710-001 24-22-00-710-002
24-24-00-710-001 24-25-00-710-001 24-26-00-710-001 24-28-00-710-001

R  24-41-00-740-002
R  24-41-00-740-002 24-41-00-861-002 24-56-00-710-001
Operational Test of the Passenger Entertainment System (Music)Operational Test of the Passenger Entertainment (Video)Operational Test of the Landscape CameraOperational Test of the Mechanic CallOperational Test of the Service InterphoneOperational Test of the Audio ManagementOperational Test of the CVR and the CVR Channel RecordingFunctional Test of the bulk-erase function and bulk-erase inhibition-logic of the CVROperational Test of the Cabin and Flight Crew Interphone-SystemOperational Test of the Emergency Evacuation (EVAC) Signalling System Operational Check of Battery-Bus powered P AOperational Test of the Cabin SignsOperational Test of the Cabin and Flight Crew Interphone-SystemOperational Test of the Emergency Evacuation (EVAC) Signalling SystemOperational Test of the IDG Disconnect and Reconnect (Reset) Function - Engine StaticOperational Test of the IDG Disconnect and Reconnect (Reset) Function - Engine StaticOperational Test of the Generator Line Contactor (GLC-1) Opening in the Smoke ProcedureOperational Test of the Transfer InhibitionOperational Test of the Emergency Generation SystemOperational Test of the AC Essential Generation SwitchingOperational Test of the Manual and Automatic Shedding of the GalleysOperational Test of the Static Inverter (3XB) when the Aircraft Electrical Circuits are Energized from the External Power Operational Test of the Ground power Control Unit (GPCU) Operational Check of GAPCU via CFDSEnergize the Aircraft Electrical Circuits from the External PowerOperational Test of the Galley Supply
　
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