-POST FLIGHT REPORT The SEND column enables display of the programming received from the ATSU. YES indicates that this report will be transmitted automatically at the end of the flight. The end of flight condition is determined by the transition to flight phase 10. The PRINT column allows the operator to program whether this report is to be automatically printed when it is transmitted to the ATSU.
-
REAL TIME FAILURE messages The SEND column enables display of the programming received from the ATSU. YES indicates that the CFDIU must automatically transmit, in real time, all the internal failure messages provided by the systems or created by the CFDIU. The PRINT column allows the operator to program whether the failure message is to be automatically printed when it is transmitted to the ATSU.
-
REAL TIME WARNING messages
1EFF : 151-154, 201-207, 1 31-32-00Page B12 1 1 Aug 01/05R 1 1 1CES 1
CFDIU - ATSU/PRINT Program
Figure 054
R 1EFF : 151-154, 201-207, 1 31-32-00Page B13 1 1 May 01/05 1 1 1CES 1
R The SEND column enables display of the programming received from
R the ATSU.
R YES indicates that the CFDIU must automatically transmit, in real
R time, all the warning messages provided by the FWC.
R The PRINT column allows the operator to program whether the warning
R message is to be automatically printed when it is transmitted to
R the ATSU.
R - AVIONICS DATA
R This function enables transmission to the ground of system pages
R displayed on the MCDU to be programmed (only when requested
R manually), to which access has been gained by the SYSTEM
R REPORT/TEST item.
R Principle:
R The 6R line key allocated to PRINT by the system, controls printing
R of the page and its transmission to the ATSU.
R The SEND column enables the operator to program this transmission
R and indicates to the CFDIU that it must add the PRINT ALSO SEND
R message (amber) in the scratchpad line of all the system pages.
R NOTE : In this specific case, the print control cannot be programmed____
R as the PRINT message is written by the system and
R consequently, it cannot be modified by the CFDIU. Therefore,
R the PRINT column contains a YES and cannot be modified.
R (3) Operational aspects
R The programming sent by the ATSU (YES or NO messages in the SEND
R column of the first three functions) and the YES in the PRINT column
R of the AVIONICS DATA function, are displayed in green (not modifiable
R by the Captain).
R The other YES* or NO* messages are displayed in blue.
R The title, the column names and the name of the different items are
R displayed in white.
R Each action on the line keys used for manual programming (4L, 1R, 2R,
R 3R) switches the YES message to NO and vice versa.
R If the CFDIU has not received any programming from the ATSU, it
R displays blanks.
R All manual programming is memorized by the CFDIU so that at
R initialization it can present the last configuration in vigor.
R All manual programming can be modified on the ground and in flight.
R (a) Manual message transmission
R When the operator requests manual transmission (action on the
R line key adjacent to SEND* for example), the CFDIU deletes the
R asterisk.
R If manual transmission cannot be performed (ATSU BUSY, NOT READY
R or NOT AVAILABLE) the CFDIU displays the NOT XMITTED TO ATSU
R message in the scratchpad and displays the asterisk again.
R 1EFF : 151-154, 201-207, 1 31-32-00Page B14 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 31-32-00Page B15 1 1 May 01/05 1 1 1CES 1 correlation between the fault messages and the ECAM warnings is carried out by means of GMT).
R R R NOTE : In both cases, transmission is not attempted again, except____ if the operator presses the line key again after the CFDIU has displayed the asterisk again.
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