A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER 6(6)

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 | | (8043KM) / SCV (8058KM) | ----+----------------------------------------+-------------------------+-------217 | No LRU Fault detected | --| 1 ----+----------------------------------------+-------------------------+-------218 | Power supply interrupt | POWER SUPPLY INTERRUPT | 1 ----+----------------------------------------+-------------------------+-------219 | | |
 to | N O T U S E D | | 229 | | | ----+----------------------------------------+-------------------------+-------230 | ECB internal Failure | ECB (59KD) | 1 ----+----------------------------------------+-------------------------+-------231 | ECB internal Failure | ECB (59KD) | 3 ----+----------------------------------------+-------------------------+-------232 | ECB internal Failure | ECB (59KD) | 3 ----+----------------------------------------+-------------------------+-------233 | ECB internal Failure | ECB (59KD) | 2 ----+----------------------------------------+-------------------------+-------234 | ECB internal Failure | ECB (59KD) | 3 ----+----------------------------------------+-------------------------+-------235 | ECB internal Failure | ECB (59KD) | 3 ----+----------------------------------------+-------------------------+-------236 | ECB internal Failure | ECB (59KD) | 2 ----+----------------------------------------+-------------------------+-------237 | ECB internal Failure | ECB (59KD) | 3 ----+----------------------------------------+-------------------------+------- -------------------------------------------------------------------------------FCN | Fault Description | CFDS Message | Class ----+----------------------------------------+-------------------------+-------238 | ECB internal Failure | ECB (59KD) | 3 ----+----------------------------------------+-------------------------+-------239 | N O T U S E D | --| -----+----------------------------------------+-------------------------+-------240 | Data Memory Module shows | DATA MEMORY MODULE | 3

 | wrap test failure | (8062KM) | ----+----------------------------------------+-------------------------+-------241 | Data Memory Module shows read failure | DATA MEMORY MODULE | 3
 | | (8062KM) | ----+----------------------------------------+-------------------------+-------242 | Data Memory Module shows checkword | DATA MEMORY MODULE | 3
 | failure | (8062KM) | ----+----------------------------------------+-------------------------+-------243 | Data Memory Module shows APU | DATA MEMORY MODULE | 3
 | S/N failure | (8062KM) | ----+----------------------------------------+-------------------------+-------244 | Data Memory Module shows write failure | DATA MEMORY MODULE || 3
 | | (8062KM) | ----+----------------------------------------+-------------------------+-------245 | Oil Level Shows Low | LOW OIL LEVEL | 2 ----+----------------------------------------+-------------------------+-------246 | | |
 to | N O T U S E D | | 299 | | | ----+----------------------------------------+-------------------------+-------300 | ECB internal Failure | --| 1 ----+----------------------------------------+-------------------------+-------301 | ECB internal Failure | --| 1 ----+----------------------------------------+-------------------------+-------302 | | --| 1 ----+----------------------------------------+-------------------------+-------303 | ECB internal Failure | --| 1 ----+----------------------------------------+-------------------------+-------

 

R  **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
 E. AIDS The Aircraft Integrated Data System (AIDS) contains two programmed reports linked to the APU. The two programmed reports are:
 -Main Engine Start (MES) IDLE,
 -SHUTDOWN.
 (1)
 MES/IDLE Report The Main Engine Start (MES)/IDLE report is supplied after every fiftieth MES and it is used to monitor APU performance. The report includes:

 -
the data from both Main Engine Starts (MES),

 -
the idle mode that follows (until the APU is shutdown),

 -
the data from the last APU start, which includes the APU operation hours and the start cycles.

 

 (2)
 SHUT DOWN Report The SHUT DOWN report is supplied after every APU shutdown occurs and is used for trouble shooting. The printer 4TW of the MCDUs prints out both the reports and ground software analyzes the reports. This information includes the APU operation hours and the start cycles.

 

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-73-00Page 85 201-210, Config-2 Aug 01/05
 CES  ANALYZERS - DESCRIPTION AND OPERATION

_____________________________________
 1.
 General

_______ The Built-In Test Equipment (BITE) of the Electronic Control Box (ECB) 59KD makes an analysis of the performance of the Auxiliary Power Unit (APU). The readout of this analysis is shown on the Multifunction Control and Display Units (MCDUs) 3CA1 (3CA2), through the function of the Centralized Fault Display System (CFDS) (Ref. 31-32-00).
　
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