The functions entering into this category are:
 -
LAST LEG REPORT

 -
LAST LEG ECAM REPORT

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 -AVIONICS STATUS.
 The remaining functions:

 -PREVIOUS LEGS REPORT
 -SYSTEM REPORT/TEST can only be printed page by page (see example). If the operator controls printing of several pages while remaining in the same function, the CFDIU only sends the header at the first print request.

R **ON A/C 001-049, 051-099, 101-105,
 D. Transmission to Ground of CFDIU and System Reports
 (1) Modification of the CFDIU main menu
 (Ref. Fig. 051)

 (a) The POST FLIGHT REP PRINT item is replaced by: POST
 * SEND FLT REP PRINT * This function is available when the ACARS option is installed on the aircraft; it cannot be reprogrammed. It enables:
 -printing of the POST FLIGHT REPORT, filtered or not filtered, if the line key adjacent to PRINT* is activated
 - or, sending of the POST FLIGHT REPORT, filtered or not filtered, to the ACARS if the line key adjacent to *SEND is activated.
 Colors:
 The *SEND and PRINT* controls are blue.
 POST FLIGHT REPORT printing corresponds to the basic definition
 of the CFDIU.

 (b) Addition of the ACARS/PRINT PROGRAM item in the CFDIU main menu This function gives access to the reprogramming page.
 (2) Programming principle Programming of the various functions is carried out manually or is delivered by the ACARS. The programming provided by the ACARS only concerns the SEND column of the following functions:
 -POST FLIGHT REPORT
 -
REAL TIME FAILURES

 -
REAL TIME WARNINGS.

R 1EFF : ALL 1 31-32-00Page B0 1 1 May 01/05 1 1 1CES 1

 CFDIU - Modification of Main Menu for Transmission to the Ground
 Figure 051

R 1EFF : 001-049, 051-099, 101-105, 1 31-32-00Page B1 1 1 May 01/05 1 1 1CES 1

 The ACARS codes this programming on label 270 bit 29 (POST FLIGHT
 REPORT), bit 28 (REAL TIME FAILURES) and bit 27 (REAL TIME WARNING)
 at a rate of 1 second.
 These bits are set to 1 when the function is active.
 The remaining functions are only manually programmable.

 -POST FLIGHT REPORT The SEND column enables display of the programming received from the ACARS. 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 ACARS.
 -
REAL TIME FAILURE messages The SEND column enables display of the programming received from the ACARS. 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 ACARS.

 -
REAL TIME WARNING messages The SEND column enables display of the programming received from the ACARS. YES indicates that the CFDIU must automatically transmit, in real time, all the warning messages provided by the FWC. The PRINT column allows the operator to program whether the warning message is to be automatically printed when it is transmitted to the ACARS.

 -AVIONICS DATA This function enables transmission to the ground of system pages displayed on the MCDU to be programmed (only when requested manually), to which access has been gained by the SYSTEM REPORT/TEST item. Principle: The 6R line key allocated to PRINT by the system, controls printing of the page and its transmission to the ACARS. The SEND column enables the operator to program this transmission and indicates to the CFDIU that it must add the PRINT ALSO SEND message (amber) in the scratchpad line of all the system pages. (Ref. Fig. 052)
R 1EFF : 001-049, 051-099, 101-105, 1 31-32-00Page B2 1 1 May 01/05 1 1 1CES 1

 CFDIU - Modification of Main Menu for Transmission to the Ground

 Figure 051A 
R 1EFF : 106-149, 155-199, 208-299, 301-399, 1401-499, 1 1CES  1 111 31-32-00 Page B3 Aug 01/05

 CFDIU - Modification of Main Menu for Transmission to the Ground R Figure 051B
R 1EFF : 151-154, 201-207, 1 31-32-00Page B4 1 1 May 01/05 1 1 1CES 1

 CFDIU - AVIONICS DATA
 Figure 052

R 1EFF : 001-049, 051-099, 101-105, 1 31-32-00Page B5 1 1 May 01/05 1 1 1CES 1

 NOTE : In this specific case, the print control cannot be programmed
　
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