A320飞机维护手册 AMM NAVIGATION 导航3(3)

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 -LRU IDENTIFICATION (Ref. Fig. 017A) Allows to display the P/N and the software numbers of the equipment.
 -GND SCANNING (Ref. Fig. 020) Based on the monitoring and fault analysis during flight, provides information of the failures detected while using this function.
 -TROUBLE SHOOTING DATA (Ref. Fig. 021) Provides correlation parameters and snapshot data concerning the failure displayed in the LAST LEG REPORT and PREVIOUS LEGS REPORT.
 -CLASS 3 FAULTS (Ref. Fig. 022) Allows to display the class 3 faults recorded during the last flight leg.
 -GROUND REPORT (Ref. Fig. 022) Allows to present the class 1 or 3 internal failures detected on ground.
 -SYSTEM TEST (Ref. Fig. 024A, 025A) Allows a check of the correct operation of the MMR.
 (2) List of components All the components are listed in Para. 2. Component Location.
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 MMR - System Test
 Figure 025A

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 34-36-00Page 60 1301-399, 401-499, 1Config-2 Aug 01/05 1 1 1CES 1R **ON A/C ALL

 

 (3) Reporting function The tables below give the list of internal/external failures.
 (a) Internal failure:
 -----------------------------------------------------------------------------I ATA I CLASS I MESSAGE I I I (A/C) I I I----------------------------------------------------------------------------I 34-36-31 I 1 I MMRi (40RTi) I I 34-36-11 I 1 I LOCALIZER ANTENNA (3RT)/COAX CABLE/MMRi(40RTi) I I 34-36-18 I 1 I GLIDE ANTENNA (4RT)/COAX CABLE/MMRi (40RTi) I I 34-36-16 I 1 I GPS ANTENNAi (43RTi)/COAX CABLE/MMRi(40RTi) I I I I i = (1,2) I -----------------------------------------------------------------------------
(b) External failure:
 -----------------------------------------------------------------------------I ATA I CLASS I MESSAGE I I I (A/C) I I -----------------------------------------------------------------------------I 31-32-34 I 3 I CFDIU (1TW)/MMRi (40RTi) I I 22-83-34 I 3 I FMGCi (1CAi)/RMPi (1RGi)/MMRi (40RTi) I I 22-83-34 I 3 I FMGCj (1CAj) BUS ILS/MMRi (40RTi) I I 22-83-34 I 3 I FMGC1 (1CA1) BUS GPS/MMRi (40RTi) I I 22-83-34 I 3 I FMGC2 (1CA2) BUS GPS/MMRi (40RTi) I I 34-12-34 I 3 I ADIRUk (1FPk)/MMRi (40RTi) I I 32-31-71 I 3 I LGCIUi (5GAi)/FMGCi (1CAi)/MMRi (40RTi) I I 31-62-34 I 1 I DMCi (1WTi)/MMRi (40RTi) I I I I j,i = (1,2) or (2,1) I I I I k = 1, 2 or 3 I -----------------------------------------------------------------------------
1EFF : ALL 1 34-36-00Page 61

1 1 Config-2 May 01/05 1 1 1CES 1 **ON A/C 051-099,

 (4) Interactive function To gain access to the BITE, it is necessary to use one MCDU (Ref. 22-82-00). (Ref. Fig. 017, 018, 019, 020, 021, 022, 023, 024, 025) All the information displayed on the MCDU during the BITE TEST configuration can be printed by the printer (Ref. 31-35-00).

R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 (4) Interactive function To gain access to the BITE, it is necessary to use one MCDU (Ref. 22-82-00). (Ref. Fig. 017A, 018A, 020, 021, 022, 023, 024A, 025A) All the information displayed on the MCDU during the BITE TEST configuration can be printed by the printer (Ref. 31-35-00).
 **ON A/C 051-099,
 B. BITE Implementation
 (1) Activation of the receiver face test The receiver face test can be activated by pushing the TEST pushbutton switch on the receiver face, if the test inhibit discrete is not active. The sequence below is then generated on the receiver face. Depending on the outcome of the receiver face test, one of the following results is displayed:
 -----------------------------------------------------------------------------I SEQUENCE I LRU STATUS I CONTROL I ANT FAIL I I TIME I I NO. I LED (DS1) I FAIL LED I LED I DEFINITION I DEFINITION I I I I (DS2) I (DS3) I I I I---------------------------------------------------------------------------I I 1 I Red I Red I Red I LED self- I 2 seconds I I I I I I test I I I---------------------------------------------------------------------------I I 2 I Green I Red I Red I LED self- I 2 seconds I I I I I I test I I I---------------------------------------------------------------------------I I 3 I Off I Off I Off I Unit self- I 2 seconds I I I I I I test I minimum I I---------------------------------------------------------------------------I
 1EFF : ALL 1 34-36-00Page 62 1 1 Config-2 Aug 01/05 1 1 1CES 1

 -----------------------------------------------------------------------------
I SEQUENCE I LRU STATUS I CONTROL I ANT FAIL I I TIME I
 I NO. I LED (DS1) I FAIL LED I LED I DEFINITION I DEFINITION I
 I I I (DS2) I (DS3) I I I
 I---------------------------------------------------------------------------I 
R  I 4 I Green I Off I Off I Unit passedI 30 seconds I 
　
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