Subtask 49-61-34-010-058
 C. Get Access
 (1)
 Open the AFT cargo-compartment door 826 (Ref. TASK 52-30-00-860-001).

 (2)
 Put the access platform below the AFT cargo-compartment door 826.

 (3) Remove the access panel 152HW (Ref. TASK 25-55-11-000-003). R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
 4. Procedure
_________ R **ON A/C 001-049, 101-105, 107-107,
 (Ref. Fig. 401/TASK 49-61-34-991-003-A)
 **ON A/C 151-199,

 (Ref. Fig. 401A/TASK 49-61-34-991-003-B)
 **ON A/C 201-210,

 (Ref. Fig. 401B/TASK 49-61-34-991-003)

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-61-34Page 403 201-210, Config-2 Aug 01/05
 CES

 ECB - Removal/Installation Figure 401/TASK 49-61-34-991-003-A

R EFF : 001-049, 101-105, 107-107, 49-61-34Page 404 Config-2 Aug 01/05
 CES

 ECB - Removal/Installation Figure 401A/TASK 49-61-34-991-003-B 
R  EFF :  151-199,  Page 40549-61-34 Config-2 May 01/05
 CES 

 ECB - Removal/Installation Figure 401B/TASK 49-61-34-991-003 
R  EFF :  201-210,  Page 40649-61-34 Config-2 May 01/05
 CES 

R  **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
 Subtask 49-61-34-020-052
 A. Removal of the ECB CAUTION : DO NOT REPLACE THE ECB AND THE DATA MEMORY MODULE AT THE SAME
_______
 TIME.

 WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME DAMAGED OR
_______ INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
 (1) At the ECB tray (1) turn the fluted knobs (2) counterclockwise to release the electronic control box (3).
 NOTE : The ECB installation points forward in those aircraft, that do
____ not have the optional bulk cargo door. Aircraft with the optional bulk cargo door, have the ECB installation pointed rearwards.
 (2)
 Carefully pull the ECB (3) out from the tray (1) to disconnect the electrical connection (4).

 (3)
 Remove the ECB (3) from the tray (1).

 (4)
 Put blanking caps on the disconnected electrical connectors.

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-61-34Page 407 201-210, Config-2 Aug 01/05
 CES  TASK 49-61-34-400-003

 Installation of the Electronic Control Box (ECB) (131-9(A))
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  access platform 2.0 m (6 ft. 7 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 25-55-11-000-003 Removal of the Sidewall Panels in the AFT Cargo Compartment - FR47/FR59 25-55-11-400-003 Installation of the Sidewall Panels in the AFT Cargo Compartment - FR47/FR59 25-55-12-000-003 Removal of the Sidewall Panels in the AFT Cargo Compartment - FR59/FR65 25-55-12-400-003 Installation of the Sidewall Panels in the AFT Cargo Compartment - FR59/FR65 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST Menu Page 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-008 Close the Bulk Cargo-Compartment Door
R  **ON A/C 001-049, 101-105, 107-107,
 49-61-34-991-003-A Fig. 401

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-61-34Page 408 201-210, Config-2 Aug 01/05
 CES  -------------------------------------------------------------------------------

REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
**ON A/C 151-199,
 49-61-34-991-003-B Fig. 401A
 **ON A/C 201-210,
 49-61-34-991-003 Fig. 401B R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
 3. Job Set-up
__________
 Subtask 49-61-34-860-064

 A. Aircraft Maintenance Configuration.
 (1)
 Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 (2)
　
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 機載輔助動力 AIRBORNE AUXILIARY POWER5(111)