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时间:2011-03-26 00:16来源:蓝天飞行翻译 作者:admin
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R  flight leg. 
R  - GROUND REPORT 
R  (Ref. Fig. 023) 
R  Allows to present the class 1 or 3 internal failures detected 
R  on ground. 
R  - SYSTEM TEST 
R  (Ref. Fig. 024, 025) 
R  Allows a check of the correct operation of the MMR. 
R  (2) List of components 
R  All the components are listed in Para. 2. Component Location. 

R 1EFF : 051-099, 1 34-36-00Page 45 1 1 Config-2 May 01/05 1 1 1CES 1R MMR - Last Leg Report R Figure 017


R 1EFF : 051-099, 1 34-36-00Page 46 1 1 Config-2 May 01/05 1 1 1CES 1


 MMR - Last Leg Report and LRU Identification
 Figure 017A

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-36-00Page 47 1301-399, 401-499, 1Config-2 Aug 01/05 1 1 1CES 1R MMR - Previous Legs Report R Figure 018


R 1EFF : 051-099, 1 34-36-00Page 48 1 1 Config-2 May 01/05 1 1 1CES 1


 MMR - Previous Legs Report
 Figure 018A

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-36-00Page 49 1301-399, 401-499, 1Config-2 Aug 01/05 1 1 1CES 1R MMR - LRU Identification R Figure 019


R 1EFF : 051-099, 1 34-36-00Page 50 1 1 Config-2 May 01/05 1 1 1CES 1


 MMR - Ground Scanning R Figure 020
 1EFF : ALL 1 34-36-00Page 51 1 1 Config-2 May 01/05 1 1 1CES 1


 MMR - Trouble Shooting Data R Figure 021
 1EFF : ALL 1 34-36-00Page 52 1 1 Config-2 May 01/05 1 1 1CES 1


 MMR - Last Leg Class 3 Faults R Figure 022
 1EFF : ALL 1 34-36-00Page 53 1 1 Config-2 May 01/05 1 1 1CES 1


R  MMR - Ground Report Figure 023
 1EFF : 1 1 1CES  ALL  1 111 Page 5434-36-00 Config-2 May 01/05

 

R  MMR - System Test 
R  Figure 024
 1EFF :  051-099,  1  34-36-00 Page 55 
1  1  Config-2 May 01/05
 1  1
 1CES  1

 

 MMR - System Test
 Figure 024A

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-36-00Page 56 1301-399, 401-499, 1Config-2 Aug 01/05 1 1 1CES 1


R  MMR - System Test 
R  Figure 025
 1EFF :  051-099,  1  34-36-00 Page 57 
1  1  Config-2 May 01/05
 1  1
 1CES  1

 


R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 A. CFDIU Interface
 (1) BITE description The BITE facilitates maintenance on in-service aircraft. It detects and identifies a failure related to the MMR. The BITE of the MMR is connected to the CFDIU. The BITE:
 -transmits permanently MMR status and its identification message to the CFDIU
 -memorizes the failures which occurred during the last 63 flight legs
 -monitors data inputs from the various peripherals
 -transmits to the CFDIU the result of the tests performed and self-tests
 -can communicate with the CFDIU through the menus. The BITE can operate in two modes:
 -
the normal mode

 -
the menu mode.


 (a)
 Normal mode During the normal mode, the BITE cyclically monitors the status of the MMR. It transmits its information to the CFDIU during the concerned flight. In case of fault detection, the BITE stores the information in the fault memories. These items of information are transmitted to the CFDIU by an ARINC 429 message with label 356.

 (b)
 Menu mode The menu mode can only be activated on ground. This mode enables communication between the CFDIU and the MMR BITE by means of the MCDU. (Ref. Fig. 016) When you get access to the SYSTEM REPORT/TEST/NAV page, the ILS1 and ILS2 indications can be shown instead of the MMR1 and MMR2 indications. In this case, you must do the following steps:

 -
make sure that the the engines are shut down - open CFDIU SUPPLY circuit breaker 2TW - open CFDIU BACK UP circuit breaker 8TW

 -
make sure that MMR1 and MMR2 circuit breakers, 42RT1 and 42RT2, are closed

 


 -wait for 30 seconds then close the CFDIU circuit breakers 2TW and 8TW
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-36-00Page 58 1301-399, 401-499, 1Config-2 Aug 01/05 1 1 1CES 1 -wait for 180 seconds then get access to the SYSTEM


 REPORT/TEST/NAV page. All the information displayed on the MCDU during the BITE Test configuration can be printed by the printer (Ref. 31-35-00). The MMR menu mode is composed of:
 -LAST LEG REPORT (Ref. Fig. 017A) This menu contains the fault messages (class 1 internal and external) detected during the last flight.
 -PREVIOUS LEGS REPORT (Ref. Fig. 018A) This report contains the fault messages related to the external or internal failures (class 1) recorded during the previous 63 flight legs.
 
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