(15)
FQI The FQI issues four buses, FQI-1A, 1B, 2A, 2B. DMC 1 acquires 1A and 2A. DMC 3 acquires 1A and 2B. DMC 2 acquires 1B and 2B. Each DMC preferably uses the FQI-1 (A or B) bus parameters. If the FQI CHANNEL SUPERIORITY signal (bit 13 of word 276) requests the switching to the FQI-2 bus, the DMCs switch to this FQI-2 bus. However the DMC keeps using a given FQI-X bus only if this bus is valid. If the two FQI-1 and 2 buses are invalid, the DMC permanently switches from one to the other until finding a valid one. Meanwhile, the fuel quantity parameters are flagged (XX) on the ECAM E/W image. TCAS (Ref. Fig. 014) Each DMC receives and processes TCAS data. The NDs indicate the position of intruders in the airspace in ROSE or ARC mode. The PFDs provide the crew with vertical speed indications to avoid these intruders.
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-68-00Page 46 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1
ECU - CFM Engines
Figure 013
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-68-00Page 47 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1
TCAS Buses
Figure 014
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The Flight Warning Computers ( FWC ) ensure the monitoring and the validity of these data. If one part of the TCAS is faulty, a message is displayed on the engine page of the upper ECAM display unit.
B. FWC Message Bus (RS 422) Inside each DMC, the principle of selection of the FWC 1 or FWC 2 message bus obeys the same rules as for the ARINC 429 bus. Each DMC preferably works with the FWC 1 RS-422 bus. In case of detected failure, it automatically switches to the FWC 2 RS-422 bus. A given FWC RS-422 bus is considered as valid if : - each block is complete : detection of the start of block (Soh code for E/W blocks, Stx for S blocks) and of the end of block (Etb code for E/W blocks, Eot for S blocks) - the number of characters which are received by the DMC matches the number of characters which are transmitted. This number is given in the 3-digit number which follows the end of block code (the 3 characters of the 3-digit number are included in the total number of characters which are transmitted) - each character is valid : for the characters, a parity check is made. If a character is not valid, the block is considered as invalid if the failure is confirmed during 3 successive transmissions - the time between two successive blocks of the same nature does not exceed 1.5 s.
C. Weather Radar Buses (ARINC 453)
R **ON A/C 001-049, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 015)
R **ON A/C 051-099,
R (Ref. Fig. 015A)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
A Weather Radar equipment complying with ARINC 708-4 is installed.
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-68-00Page 49 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1
R **ON A/C 001-049, 101-105, 151-199, 201-299, 301-302,
Each DMC receives from the W/R transceiver unit his two data buses, D1
and D2.
The DMC processes information from the W/R transceiver provided that W/R
operation is enabled by the W/R request control signal).
Provided that the W/R operation is requested on the W/R control unit, the
ND presents a W/R image in all the ND modes except the PLAN mode. If both
pilots select the PLAN mode, the DMCs send the W/R REQUEST discrete
signal in the open state, which disables the W/R XCVR, thus avoiding
useless operating hours.
Data bus selection :
The DMCs which operate on side 1 normally work with the DATA 1 buses
(XCVR 1-1), which correspond to the CAPT range selection. However, the
DMCs which operate on side 1 may operate with a DATA 2 bus, i.e.
using the data corresponding to the range selected by the F/O, in case of
an FMGC 1 failure which leads to an automatic changeover to the FMGC 2
data in the DMC 1.
R **ON A/C 051-099,
R Each DMC receives from the W/R transceivers units their two data buses,
R D1 and D2.
R The DMC processes information from the operating W/R transceiver (only
R one at a time according to the position of the 1-2 selection switch on
R the W/R control unit and provided that W/R operation is enabled by the
R W/R request control signal).
R Provided that the W/R operation is requested on the W/R control unit, the
R ND presents a W/R image in all the ND modes except the PLAN mode. If both
R pilots select the PLAN mode, the DMCs send the W/R REQUEST discrete
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