-
ALL DISARMED

 -FWD: L=ARMED; R=DISA. (example, the respective location is shown)
 -NO INFORMATION AVAILABLE
 Messages in case of DOORS STATUS:
 -ALL CLOSED
 -FWD: L=OPEN; R=CLOS. (example, the respective location is shown)
 -NO INFORMATION AVAILABLE
 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A61 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 System Status - Failure Examples 1 Figure 044 (SHEET 1)
 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A62 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 System Status - Failure Examples 1 Figure 044 (SHEET 2)
 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A63 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 System Status - Failure Examples 2 Figure 045 (SHEET 1)
 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A64 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 System Status - Failure Examples 2 Figure 045 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A65 1201-299, 1Config-1 Aug 01/05 1 1 1CES 1

 SLIDES STATUS indication - Example
 Figure 046

 1EFF : 211-299, 1 23-73-00Page A66 1 1 Config-1 Aug 01/05R 1 1 1CES 1

 DOORS STATUS indication - Example
 Figure 047

R 1EFF : 211-299, 1 23-73-00Page A67 1 1 Config-1 Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,

 (3) MAINTENANCE MODE (Ref. Fig. 048)
 (a) A MAINTENANCE mode for detailed CIDS failure description is part of the SYSTEM STATUS mode. Failures are written into the directors BITE ground/flight memory and can be read via this mode and via the CFDS in the flight compartment. The last occured failure is the first shown. For failures of continuously monitored systems the BITE ground memory will be updated when the failure has been cancelled.
 No entries into the BITE memory are made in case of emergency conditions (normal power is not available or the CIDS is working with the mandatory layout).
 No subsequent related failures will be entered into the memory after the original failure has been entered:
 Examples:
 -
If one DEU A fails, no further entries into memory are made for the associated components.

 -
If one DEU B fails, no further entries into memory are made for the associated slides bottle pressure, but the system status on the PTP displays SLIDES PRESS LOW.

 (b) The following items from the directors BITE memory are selectable:
 1_ LAST LEG REPORT
 In flight, this report is called CURRENT LEG REPORT.
 It is the only displayed and accessable item within the
 MAINTENANCE mode in flight.
 The LAST/CURRENT LEG REPORT contains class 2 + 1 failures
 (Ref. Para. 8F) of the last/current flight leg.
 The report includes the date, the time and the ATA chapter for
 each failure. There are no entries for flight legs without
 failures but the flight leg counts are incremented.

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A68 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 System Status - Example
 Figure 048

 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page A69 1201-299, 1Config-1 Aug 01/05R 1 1 1CES 1

 2_ PREV LEGS REPORT The PREV LEGS REPORT contains 1 + 2 failures of the last 64 flight legs. The PREV LEGS REPORT has all data, which are stored in the LAST LEG REPORT.
 3_ LRU INDENTIFICATION Messages for LRU IDENTIFICATIONS (examples):
 DIRECTOR 1: Z010H0004114
 DIRECTOR 2: Z010H0004114
 CAM M-COUNT=030 Z050H0000343 (1) (example, the active layout is shown)
 PROG AND TEST PNL Z020H0001112

 NOTE : M-COUNT = modification count, incremented after any programming/saving to Layout M.
 4_ FAULT DATA
 The FAULT DATA mode includes the flight leg, the date, the
 time (UTC), the number of occurences (max 4 counts, for
 intermittent failures) and coded trouble shooting data for
 internal director and DEU failures.
 Present failures on ground are marked with GND (Ref. Para.
 8.B.(3)(b)5 GND SCAN), failures of the last leg with LEG -00,
 (Ref. Para. 8.B.(3)(b)1 LAST LEG REPORT) and failures of the
 previous legs with -01, -02 and up (Ref.Para. 8.B.(3)(b)2 PREV
 LEGS REPORT).

 a CIDS Trouble Shooting Data Table
_ These tables show the meaning of the last 6 digits appearing in the FAULT DATA mode (PTP) and TROUBLE SHOOTING DATA mode (MCDU) for each class 1 and 2 failure.
　
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