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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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 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-38-00-710-001  Operational Test of the Battery Charge Limiter (BCL), (with the CFDS)
 AMM 24-38-00-710-001  Operational Test of the Battery Charge Limiter (BCL), (without 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 Battery charge Limiter (BCL) (with the CFDS) (Ref. AMM TASK 24-38-00-710-001).
 4. Fault Isolation_______________
 A. If the test of the BCL is correct and if the battery voltage on the
 applicable voltmeter has the specified value (28VDC):

 - replace the BCL-1 (1PB1), (Ref. AMM TASK 24-38-34-000-001) and (Ref. AMM TASK 24-38-34-400-001).
 B. Do the operational test of the Battery Charge Limiter (BCL) (without the CFDS) to make sure that the system operates correctly (Ref. AMM TASK 24-38-00-710-001).
 「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 272
 May 01/01R
 CES

 TASK 24-38-00-810-842


 No Electrical Parameters of the BAT2 are shown on the ELEC Page
 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 24-38-00-710-001  Operational Test of the Battery Charge Limiter (BCL), (without 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 Battery Charge Limiter (BCL) (with the CFDS) (Ref. AMM TASK 24-38-00-710-001).
 4. Fault Isolation_______________
 A. If the test of the BCL is correct and if the battery voltage on the
 applicable voltmeter has the specified value (28VDC):

 - replace the BCL-2 (1PB2), (Ref. AMM TASK 24-38-34-000-001) and (Ref. AMM TASK 24-38-34-400-001).
 B. Do the operational test of the Battery Charge Limiter (BCL) (without the CFDS) to make sure that the system operates correctly (Ref. AMM TASK 24-38-00-710-001).
 「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 273
 May 01/01R
 CES  TASK 24-38-00-810-843


 Incorrect Discharge of the Battery 1
 1. Possible Causes
_______________
R - SEC-1 (1CE1) R - SEC-2 (1CE2) R - SEC-3 (1CE3)
 - PRESS SW-B HYD, FLT CTL (10CE1)

 - PRESS SW-G HYD, FLT CTL (10CE2)

 - PRESS SW-Y HYD, FLT CTL (10CE3)

 - ELAC-1 (2CE1)

 - BCL-1 (1PB1)

 - BAT-1 (2PB1)

 - PRESS SW-FLT CTL, G (1151GN)

 - PRESS SW-FLT CTL, B (2151GN)

 - PRESS SW-FLT CTL, Y (3151GN)


 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific ammeter
 No specific warning notice(s)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
IPC 27920803 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) AMM 24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2) AMM 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power AMM 27-92-17-000-001 Removal of the Flight Control Pressure Switch (10CE2) AMM 27-92-17-000-002 Removal of the Flight Control Pressure Switch (10CE3) AMM 27-92-17-000-003 Removal of the Flight Control Pressure Switch (10CE1) AMM 27-92-17-400-001 Installation of the Flight Control Pressure Switch
 
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