R 1EFF : ALL 1 31-66-00Page 61 1 1 Aug 01/05 1 1 1CES 1
STS , ADV and overflow indication R Figure 031
R 1EFF : 106-149, 303-399, 401-499, 1 31-66-00Page 62 1 1 Aug 01/05 1 1 1CES 1
STS , ADV and overflow indication R Figure 032
1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-66-00Page 63 1201-299, 301-302, 1Aug 01/05 1 1 1CES 1
B. FQI The FQI issues 4 buses, FQI-1A, 1B, 2A, 2B. DMC1 acquires 1A and 2A DMC3 acquires 1A and 2B DMC2 acquires 1B and 2B. Each DMC uses preferably the FQI-1 (A or B) bus parameters. If the FQIS CHANNEL SUPERIORITY signal (label 276 bit 13 of both FQI channels) requests the switching to the FQI-2 bus, the DMCs switches to this FQI-2 bus. However, the DMC keeps using a given FQI-X bus only if this bus is valid. A given FQI-X bus is valid only if all parameters used by the DMC are valid. If the 2 FQI-1 and 2 buses are invalid, the DMC switches permanently from one to the other until finding a valid one. Meanwhile the fuel quantity parameters are flagged (XX) on the ECAM E/W image.
1EFF : ALL 1 31-66-00Page 64 1 1 Aug 01/05 1 1 1CES 1 ECAM SYSTEM/STATUS DISPLAY - DESCRIPTION AND OPERATION
______________________________________________________
1. General
_______
The System Display (SD) is normally presented on the lower ECAM display
unit, on the center instrument panel: the System Display Display Unit (SD
DU).
It provides 11 system pages, a cruise page and a status page.
These pages are displayed one at a time.
They can be called automatically or manually. The SD can be presented on the
upper ECAM display unit (Engine/Warning Display Display Unit - EWD DU) or on
a Navigation Display Display Unit (ND DU) after a DU failure
(Ref. 31-68-00).
2. Component Location
__________________
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 001)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 002)
**ON A/C ALL
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------1WT1 DMC-1 85VU 127 824 31-63-34 1WT2 DMC-2 86VU 128 824 31-63-34 1WT3 DMC-3 85VU 127 824 31-63-34 4WT2 DU-ECAM, LOWER 4VU 210 831 31-63-22 6WT CTL PNL-ECAM 11VU 210 831 31-61-12
1EFF : ALL 1 31-67-00Page 1 1 1 Aug 01/05 1 1 1CES 1
SD - Component Location
Figure 001
R 1EFF : 106-149, 303-399, 401-499, 1 31-67-00Page 2 1 1 Aug 01/05 1 1 1CES 1
SD - Component Location
Figure 002
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-67-00Page 3 1201-299, 301-302, 1May 01/05 1 1 1CES 1
3. System Description
__________________
A. General
(1) Areas on the SD
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 003)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 004)
**ON A/C ALL
The System Display is divided in two areas:
- one large area at the top, to display the system pages
- one small area at the bottom, to display permanent data. The permanent data area is always displayed, whatever the page presented. It consists of:
-total air temperature
-static air temperature
R **ON A/C 106-149, 303-399, 401-499,
-Delta ISA indication
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
-G load if excessive
R **ON A/C 106-149, 303-399, 401-499,
-G load if excessive or a message linked to the DU monitoring process:
-
CHECK CAPT PFD (upper line)
-
CHECK F/O ND (lower line)
-DISPLAY SYSTEM VERSION INCONSISTENCY (needs the 3 available lines)
1EFF : ALL 1 31-67-00Page 4 1 1 Aug 01/05 1 1 1CES 1
SD - Display Areas Figure 003
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-67-00 Page 5 Aug 01/05
SD - Display Areas
Figure 004
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-67-00Page 6 1201-299, 301-302, 1May 01/05 1 1 1CES 1R - DU NOT MONITORED
R **ON A/C ALL
-identification of the active DMC during the switching test
-Universal Coordinated Time
-gross weight
NOTE : (a) The display indications given in this note are for
____ description purpose only and do not represent an operational configuration.
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