(7)
Not Applicable
(8)
Not Applicable
R **ON A/C 051-099, 106-149, 201-209, 211-299, 301-399, 401-499,
(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. 036A)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 34-43-00Page A41 1201-209, 211-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
TCAS - PREVIOUS LEGS REPORT
Figure 036
R 1EFF : 001-049, 101-105, 151-199, 1 34-43-00Page A42 1 1 May 01/05 1 1 1CES 1
TCAS - PREVIOUS LEGS REPORT
Figure 036A
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A43 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
TCAS - PREVIOUS LEGS REPORT
Figure 036B
R 1EFF : 201-207, 210-210, 1 34-43-00Page A44 1 1 May 01/05 1 1 1CES 1
TCAS - LRU IDENTIFICATION
Figure 037
R 1EFF : 001-049, 101-105, 151-199, 1 34-43-00Page A45 1 1 May 01/05 1 1 1CES 1
R TCAS - LRU IDENTIFICATION
R Figure 037A
R 1EFF : 051-099, 1 34-43-00 Page A46
1 1 May 01/05
1 1
1CES 1
TCAS - LRU IDENTIFICATION
Figure 037B
R 1EFF : 106-149, 201-207, 210-299, 301-399, 1 34-43-00Page A47 1401-499, 1Aug 01/05 1 1 1CES 1
TCAS - LRU IDENTIFICATION
R Figure 037C
1EFF : 208-209, 1 34-43-00 Page A48
1 1 May 01/05
1 1
1CES 1
TCAS - GROUND SCANNING
Figure 038
1EFF : 001-049, 101-105, 151-199, 1 34-43-00Page A49 1 1 May 01/05 1 1 1CES 1
TCAS - GROUND SCANNING
Figure 038A
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A50 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
TCAS - GROUND SCANNING Figure 038B
1EFF : 1 1 1CES 201-207, 210-210, 1 111 34-43-00 Page A51 May 01/05
TCAS - GROUND REPORT Figure 039
1EFF : 1 1 1CES 001-049, 101-105, 151-199, 1 111 34-43-00 Page A52 May 01/05
(4) LRU IDENTIFICATION
**ON A/C 051-099,
(Ref. Fig. 037A)
R **ON A/C 106-149, 201-207, 211-299, 301-399, 401-499,
(Ref. Fig. 037B)
**ON A/C 208-209,
(Ref. Fig. 037C)
R **ON A/C 051-099, 106-149, 201-209, 211-299, 301-399, 401-499,
(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. 038A)
(6)
TROUBLE SHOOTING DATA This function allows to analyze the snapshot of the recorded fault to detect any software bug. Two types of data are displayed:
-
some correlation parameters which are the date and the UTC hour displayed in clear english,
-
some snapshot data delivered in hexadecimal code or in clear
message.
(Ref. Fig. 040)
(7) 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. 039A)
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A53 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
TCAS - GROUND REPORT
Figure 039A
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A54 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
TCAS - GROUND REPORT Figure 039B
1EFF : 1 1 1CES 201-207, 210-210, 1 111 34-43-00 Page A55 May 01/05
TCAS - TROUBLE SHOOTING DATA
Figure 040
R 1EFF : 051-099, 106-149, 201-209, 211-299, 1 34-43-00Page A56 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(8) Not Applicable
**ON A/C 201-207, 210-210,
Post SB 34-1238 For A/C 201-207,
(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. 036B)
(4)
LRU IDENTIFICATION
(Ref. Fig. 037B)
(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. 038B)
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