R 1EFF : 001-049, 101-105, 151-199, 1 34-43-00Page A33 1 1 May 01/05 1 1 1CES 1
TCAS - Internal Fault Messages
Figure 034A
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A34 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
TCAS - Internal Fault Messages
Figure 034B
R 1EFF : 201-207, 210-210, 1 34-43-00Page A35 1 1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------| LIST OF EXTERNAL FAULT MESSAGES | |-----------------------------------------------------------------------------| | ATA | CLASS | MESSAGE | |-----------------------------------------------------------------------------| | 341234 | 1 | ADIRU1 (1FP1)/TCAS (1SG) | | 240000 | 1 | POWER SUPPLY INTERRUPT | | 355212 | 1 | ATC - TCAS CTL PNL (3SH)/TCAS (1SG) | | 313234 | 3 | CFDIU (1TW)/TCAS (1SG) | -------------------------------------------------------------------------------
NOTE : Fault of the selected ATC is a class 1 failure.____ Fault of the ATC in standby is a class 3 failure.
NOTE : Fault of one radio altimeter is a class 3 fault whereas____ it becomes a class 1 fault when two radio altimeters are faulty.
The class 3 recorded external faults are displayed through the menu sequence as shown in the following figure.
R **ON A/C 001-049, 101-105, 151-199,
(Ref. Fig. 035)
R **ON A/C 051-099,
R (Ref. Fig. 035A)
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-43-00Page A36 1 1 May 01/05 1 1 1CES 1
TCAS - External Fault Messages
Figure 035
R 1EFF : 001-049, 101-105, 151-199, 1 34-43-00Page A37 1 1 May 01/05 1 1 1CES 1
TCAS - External Fault Messages
Figure 035A
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A38 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 201-299, 301-399, 401-499,
2 External faults
_ External faults and associated messages are listed in the table below:
-------------------------------------------------------------------------------
| LIST OF EXTERNAL FAULT MESSAGES |
|-----------------------------------------------------------------------------|
| ATA | CLASS | MESSAGE |
|-----------------------------------------------------------------------------|
| 344233 | 3 | RA1 (2SA1)/TCAS (1SG) |
| 344233 | 3 | RA2 (2SA2)/TCAS (1SG) |
| 344233 | 1 | RA1 (2SA1)+RA2 (2SA2)/TCAS (1SG) |
| 345233 | 3 | ATC 1(1SH1)/TCAS (1SG) |
| 345233 | 3 | ATC 2(1SH2)/TCAS (1SG) |
| 345233 | 1 | ATC1 (1SH1)+ATC2 (1SH2)/TCAS (1SG) |
| 341234 | 3 | ADIRU1 (1FP1)/TCAS (1SG) |
| 240000 | 1 | POWER SUPPLY INTERRUPT |
| 355212 | 1 | ATC - TCAS CTL PNL (3SH)/TCAS (1SG) |
| 313234 | 3 | CFDIU (1TW)/TCAS (1SG) |
-------------------------------------------------------------------------------
NOTE : Fault of one ATC is a class 3 fault.
____ Fault of both ATCs is a class 1 fault.
NOTE : Fault of one radio altimeter is a class 3 fault whereas
____ it becomes a class 1 fault when two radio altimeters are faulty.
The class 3 recorded external faults are displayed through the CLASS 3 FAULTS menu sequence as shown in the following figure.
R **ON A/C 106-149, 201-209, 211-299, 301-399, 401-499,
(Ref. Fig. 035A)
**ON A/C 201-207, 210-210,
Post SB 34-1238 For A/C 201-207,
(Ref. Fig. 035B)
R 1EFF : 106-149, 201-299, 301-399, 401-499, 1 34-43-00Page A39 1 1 Aug 01/05 1 1 1CES 1
TCAS - External Fault Messages
Figure 035B
R 1EFF : 201-207, 210-210, 1 34-43-00Page A40 1 1 May 01/05 1 1 1CES 1 **ON A/C 001-049, 101-105, 151-199,
(3)
PREVIOUS LEGS REPORT The messages are identical to those shown in the Para. above but concern the last 63 flights if faults have occurred during these flights. (Ref. Fig. 036)
(4)
LRU IDENTIFICATION
(Ref. Fig. 037)
(5)
GROUND SCANNING This function enables consultation of the TCAS computer fault recordings as defined by the Component Manufacturer. The TCAS peripheral monitoring and internal cyclic tests are used in order to detect transient faults. (Ref. Fig. 038)
(6)
GROUND REPORT This function is used to present class 1, 2 or 3 internal faults when they are detected on ground. These faults differ from those displayed on the LAST LEG REPORT page. The following figure shows examples of internal faults recorded on ground by the TCAS system. The relevant trouble shooting data are displayed by pressing the line key adjacent to the fault indication. (Ref. Fig. 039)
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