are listed below:
ATA 21 PACK 1 From pack controller 7HH
AFT CRG HEAT (option)
PACK 2 From pack controller 27HH
ZONE CONT From ECS zone controller 8HK
ATA 22 nil
ATA 23 CIDS1 From CIDS1 director 101RH
CIDS2 From CIDS2 director 102RH
ATA 24 DC BUS TIE From DC ESS bus sply 4PC & DC norm bus 1 1PC1
AC GEN From GPCU 1XG or GAPCU (24XG)
ATA 26 SDCU From smoke detector 10WQ
ATA 27 F/CTL From FCDC1 or 2 3CE1 (or 2)
SFCS From SFCC1 (21CV) or SFCC2 (22CV)
ATA 28 FUEL From FQI 3QT
ATA 30 ICE DETECT From WHC1 (2DG1) or WHC2 (2DG2)
ATA 31 CFDIU From CFDIU 1TW
DAR (option) From CFDIU 1TW
QAR (option) From CFDIU 1TW
DMU (option) From CFDIU 1TW
ATA 32 BRAKES From BSCU channel 1 or 2 10GG
ATA 34 ADR From ADIRU2 (1FP2) or ADIRU3 (1FP3)
IR From ADIRU1 (1FP1) or ADIRU3 (1FP3)
ATA 36 AIR BLEED From BMC1 (1HA1) or BMC2 (1HA2)
ATA 49 APU From ECB 59KD
ATA 77 ENG1 FADEC From ECU1 4000KS (for CFM motor)
ENG2 FADEC From ECU2 4000KS
ENG1 FADEC From EEC1 4000KS (for IAE motor)
ENG2 FADEC From EEC2 4000KS
ENG1 EIU From EIU1 1KS1
ENG2 EIU From EIU2 1KS1
ENG EVMU From EVMU 2EV
NOTE : The MAINTENANCE part of the STATUS page is only available on ground
____ when both engines are stopped.
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4. Symbology Used in the Operational Presentation
______________________________________________
--------------------ELEC | AC ESS BUS FAULT | ------------------------
An underlined title plus a framed wording indicates a primary failure.
NAV ADR 1 FAULT
---
An underlined title plus a plain wording indicates an independent fault.
*FUEL
An asterisk plus a title (plain) indicates a secondary fault.
Each page related to a fault analysis mentions:
-
the fault name,
-
the SYSTEM page called by the fault,
-
the detector (item of equipment providing the fault to the warning
system),
-
the MASTER light activated by the fault,
-
the aural warning triggered by the fault,
-
the ATA chapter number to file the fault,
-
the flight phases which inhibit the fault,
-
the operational sequence of crew action with associated warning titles and ECAM messages as seen by the crew during the flight.
1EFF : ALL 1 31-51-00Page 8 1 1 May 01/05R 1 1 1CES 1
OPERATIONAL PRESENTATION - SERVICING
____________________________________
TASK 31-51-00-610-001
Load OEB REMINDER information into FWCs using MCDUs.
1. Reason for the Job__________________
Load OEB REMINDER information into the FWC data base in one operation or
element by element.
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
31-51-00-610-002 Delete OEB REMINDER information from FWCs using MCDUs.
31-51-00-610-003 Crossload OEB REMINDER information into FWCs using
MCDUs. 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________ Subtask 31-51-00-860-050
A. Aircraft Maintenance Configuration
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002)
Subtask 31-51-00-010-050
B. Get access to the Avionics Compartment
(1)
Put the access platform in position below the access door 824.
(2)
Open the access door 824.
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C. Make sure that this(these) circuit breaker(s) is(are) closed:
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