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____ as the PRINT message is written by the system and consequently, it cannot be modified by the CFDIU. Therefore, the PRINT column contains a YES and cannot be modified.
 (3) Operational aspects The programming sent by the ACARS (YES or NO messages in the SEND column of the first three functions) and the YES in the PRINT column of the AVIONICS DATA function, are displayed in green (not modifiable by the Captain). The other YES* or NO* messages are displayed in blue. The title, the column names and the name of the different items are displayed in white. Each action on the line keys used for manual programming (4L, 1R, 2R, 3R) switches the YES message to NO and vice versa. If the CFDIU has not received any programming from the ACARS, it displays blanks. All manual programming is memorized by the CFDIU so that at initialization it can present the last configuration in vigor. All manual programming can be modified on the ground and in flight.
 (a) Manual message transmission (Ref. Fig. 053) When the operator requests manual transmission (action on the line key adjacent to SEND* for example), the CFDIU deletes the asterisk. If manual transmission cannot be performed (ACARS BUSY, NOT READY or NOT AVAILABLE) the CFDIU displays the NOT XMITTED TO ACARS message in the scratchpad and displays the asterisk again.
 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.
 When transmission has been performed correctly, the CFDIU displays the XMITTED TO ACARS message in the scratchpad and displays the asterisk again. These two messages are amber. The operator cannot change page as long as the CFDIU has not displayed one of the above messages and displayed the asterisk again. The CFDIU may abandon all its current functions in order to satisfy a manual transmission request.
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 CFDIU - Manual Message Transmission
 Figure 053

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 (b) Automatic message transmission When the CFDIU carries out an automatic transmission, it does not display a message in the scratchpad.

R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 D. Transmission to Ground of CFDIU and System Reports
 (1) Modification of the CFDIU main menu
 (Ref. Fig. 051A)

 (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 REPORTS PROGRAMMING 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 MU or ATSU equipment.
 The programming provided by the ACARS system only concerns the SEND column of the following functions:
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 -POST FLIGHT REPORT
 -
REAL TIME FAILURES

 -
REAL TIME WARNINGS.

 The ACARS MU and ATSU code 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 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
 DC1/NULL.
 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 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 during the flight. The PRINT column allows the operator to program whether the failure message is to be automatically printed when it is transmitted to the ATSU.
　
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