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时间:2011-03-28 13:22来源:蓝天飞行翻译 作者:航空
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 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-38-00∞∞∞∞∞∞∞∞∞∞Page 282
 May 01/01R
 CES

 TASK 24-38-00-810-846


 Incorrect ARINC Coding of BCL 1
 1. Possible Causes
_______________
 - BCL-1 (1PB1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-38-00-710-001 Operational Test of the Battery Charge Limiter (BCL), (with the CFDS) AMM 24-38-34-000-001 Removal of the Battery Charge Limiter (BCL) (1PB1, 1PB2) AMM 24-38-34-400-001 Installation of the Battery Charge Limiter (BCL) (1PB1, 1PB2)
 3. Fault Confirmation
__________________
 A. Test Do the operational test of the BCL 1 (Ref. AMM TASK 24-38-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives a message, you can find the related trouble shooting procedure in the applicable Page Block 101. If there is no message, replace the BCL-1 (1PB1) (Ref. AMM TASK 24-38-34-000-001) and (Ref. AMM TASK 24-38-34-400-001).
R B. Do the test given in para. 3.

 TASK 24-38-00-810-847


 Incorrect ARINC Coding of BCL 2
 1. Possible Causes
_______________
 - BCL-2 (1PB2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-38-00-710-001 Operational Test of the Battery Charge Limiter (BCL), (with the CFDS) AMM 24-38-34-000-001 Removal of the Battery Charge Limiter (BCL) (1PB1, 1PB2) AMM 24-38-34-400-001 Installation of the Battery Charge Limiter (BCL) (1PB1, 1PB2)
 3. Fault Confirmation
__________________
 A. Test Do the operational test of the BCL 2 (Ref. AMM TASK 24-38-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives a message, you can find the related trouble shooting procedure in the applicable Page Block 101. If there is no message, replace the BCL-2 (1PB2) (Ref. AMM TASK 24-38-34-000-001) and (Ref. AMM TASK 24-38-34-400-001).
R B. Do the test given in para. 3.

 TASK 24-38-00-810-848


 Loss of the BAT1 and BAT2 because of Undervoltage
 1. Possible Causes
_______________
R
 - P/BSW-APU/MASTER SW (14KD)

 - RELAY-BUS 1XP CTL (15XC)


 - RELAY-BUS 2XP CTL (16XC) R - ADIRU-1 (1FP1)
 - wiring
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the R External Power R AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied R from the External Power R ASM 24-24/02
 ASM 24-38/01 R ASM 24-38/02 AWM 24-38-01
 3. Fault Confirmation
__________________
R A. Aircraft Maintenance Configuration
R (1) Energize the aircraft electrical circuits R (Ref. AMM TASK 24-41-00-861-002).
R B. Test
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: On the lower ECAM DU:
 - push the ELEC key to get the  - if the voltage indication is shown in
 ELEC page.  amber, do the trouble shooting given in Para. 4.A.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-38-00∞∞∞∞∞∞∞∞∞∞Page 285
 Feb 01/05 CES

 4. Fault Isolation
_______________

R A. Table of the circuit breakers used in this procedure:

R -------------------------------------------------------------------------------R PANEL DESIGNATION IDENT. LOCATION
R -------------------------------------------------------------------------------R 122VU ELEC/BUS/2XP/CTL 17XN2 V27
R 122VU ELEC/AC/BUS1/CTL 17XN1 V25

R B. If the test confirms the fault:
 
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