A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 On one MCDU, get the SYSTEM REPORT/TEST INST menu page (Ref. TASK 31-32-00-860-008).

 1EFF : 106-149, 229-299, 303-399, 401-499, 1 31-50-00Page 537 1 1 Aug 01/05 1 1 1CES 1 Subtask 31-50-00-865-072

 B. Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION -------------------------------------------- IDENT. LOCATION-----------------------------
49VU SDAC/1/SPLY  3WV  F04
 49VU SDAC/2/26VAC SYNC/AC ESS BUS  6WV  F03
 49VU SDAC/1/26VAC SYNC/AC ESS BUS  5WV  F02
 49VU FWS/FWC1/SPLY  3WW  F01
 121VU EIS/FWC2/SPLY  2WW  Q07
 121VU EIS/SDAC/2/SPLY  2WV  Q06
 121VU EIS/SDAC/1/BUS2/26VAC SYNC AC  7WV  Q03
 121VU EIS/SDAC/2/BUS2/26VAC SYNC AC  8WV  Q02
 4. Procedure_________
 Subtask 31-50-00-740-052
 A. Test

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the MCDU, push the line key adjacent to the ECAM 1 indication.

2.
 Push the next page key.

3.
 Push the line key adjacent to the SYSTEM CONFIGURATION indication.

4.
 Push the line key adjacent to the ECAM PIN PROGRAM SOFT indication.

On the MCDU, theECAM-1/FWC1/2-SDAC1/2-ECP page comesinto view.
The ECAM-1/FWC1/2-SDAC1/2-ECP next page comes into view.
The ECAM-1/SYSTEM CONFIGURATION pagecomes into view.
The ECAM-1/ECAM PIN PROGRAM SOFT pagecomes into view.
 1EFF : 106-149, 229-299, 303-399, 401-499, 1 31-50-00Page 538 1 1 Aug 01/05 1 1 1CES 1

 5. Close-up
________ Subtask 31-50-00-860-090
 A. Put the aircraft back to its initial configuration.
 (1)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view.

 (2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002)

 (3)
 Put the system back to the serviceable condition.

 (4)
 Put the aircraft back to the serviceable condition.

 1EFF : 106-149, 229-299, 303-399, 401-499, 1 31-50-00Page 539 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL

R TASK 31-50-00-710-011 R Operational Test of the MASTER CAUT and MASTER WARN lights R 1. Reason for the Job
__________________ R To make sure that the MAST WARN and MAST CAUT lights operate correctly. R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-41-00-861-002 R R 24-41-00-862-002 R R 31-60-00-860-001 R 31-60-00-860-002
R 3. Job Set-up
__________
R Subtask 31-50-00-860-093 Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power EIS Start Procedure EIS Stop Procedure
R A. Aircraft Maintenance Configuration
R Energize the aircraft electrical circuits
R (Ref. TASK 24-41-00-861-002)
R Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
R (Ref. TASK 31-60-00-860-001)

 1EFF : ALL 1 31-50-00Page 540 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 31-50-00Page 541 1 1 Aug 01/05 1 1 1CES 1

R  Subtask 31-50-00-865-077 
R  B. Make sure that this(these) circuit breaker(s) is(are) closed: 
R  -------------------------------------------------------------------------------
R  PANEL  DESIGNATION  IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  49VU ENGINE/2/FIRE DET/LOOP B  8WD2  A07 
R  49VU ENGINE/1/FIRE DET/LOOP A  7WD1  A06 
R  49VU SDAC/1/SPLY  3WV  F04 
R  49VU SDAC/2/26VAC SYNC/AC ESS BUS  6WV  F03 
R  49VU SDAC/1/26VAC SYNC/AC ESS BUS  5WV  F02 
R  121VU EIS/SDAC1 AND 2/BUS2/28VDC  44WV  P03 
R  121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/B  2WE1  Q44 
R  121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A  1WE1  Q43 
　
中國航空網 m.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 5(165)