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.
R 1EFF : 001-049, 062-099, 101-149, 151-156, 1 31-51-00Page 7 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL

 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.

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-51-00Page 301 1 1 Aug 01/05 1 1 1CES 1 Subtask 31-51-00-865-050

 C. Make sure that this(these) circuit breaker(s) is(are) closed:
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 指示/記錄系統 6(3)