CFDIU - PREVIOUS LEGS REPORT Figure 030
 1EFF : 1 1R 1CES  ALL  1 11 1 31-32-00 Page A46 May 01/05

 (d)
 AVIONICS STATUS (Ref. Fig. 031) The purpose of this item, which is part of the main maintenance menu, is to present, on the ground and in real time, the identity of systems that are affected by an internal or external fault (class 1, 2 or 3). (CLASS 3) is displayed next to the name of a system that is affected by at least one class 3 fault. These messages contain the names of systems affected by a fault when this function is executed, or a NO X DATA message when the system X bus is no longer valid. This information is displayed on the MCDU in clear when this function is activated by the operator.

 (e)
 POST FLIGHT REPORT

 **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 (Ref. Fig. 032)

R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 (Ref. Fig. 032A)
 **ON A/C ALL
 The purpose of this item, which is part of the main maintenance menu, is to present, in a single report after the flight, the ECAM warnings (primary and independent) and the fault messages (class 1 and 2) of the last flight (so as to permit correlation). This item is the "sum" of LAST LEG REPORT and LAST LEG ECAM REPORT items. So these messages are separated into two parts; the first part contains the ECAM warnings associated with the time, the flight phase and the ATA reference, the second contains the failed LRUs associated with the time, the ATA reference and the identifiers. Aircraft identification, the date, the flight time, the flight number (airline) and the departure and arrival airports are included in the header. This information is printed out directly by the printer in clear (not displayed on the MCDUs), when this function is activated by the operator or automatically at the second engine A/C shut down.
 1EFF : ALL 1 31-32-00Page A47 1 1 Aug 01/05 1 1 1CES 1

 CFDIU - AVIONICS STATUS Figure 031 
R 1EFF : 1 1 1CES  ALL  1 111 31-32-00 Page A48 May 01/05

 CFDIU - POST FLIGHT REPORT
 Figure 032

R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 31-32-00Page A49 1201-207, 1May 01/05 1 1 1CES 1

 CFDIU - POST FLIGHT REPORT
 Figure 032A

R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page A50 1401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,

 (f) CURRENT FLIGHT REPORT
 (Ref. Fig. 033)
 The purpose of this item is to enable manual printing or transmission through ACARS MU or ATSU of all current faults and warnings which occured since the beginning of the flight and up to printing and/or transmission request.
 **ON A/C ALL
 (g)
 GMT/DATE INIT (Ref. Fig. 034) In the event of clock fault, a flag comes into view on the main clock. The CFDIU displays the time on the ECAM display unit. If, in addition, there is a long power cutoff (> 200 ms), the CFDS adds the GMT/DATE INIT item in its menu, enabling the crew to reinitialize the time and date on the MCDU. When the main clock is failed, and there is a long power interrupt (> 200ms), the CFDIU sends as GMT 79:99 (displayed on the ECAM display unit, and recorded by each system).

 (h)
 PFR/FILTER PROGRAM

 **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 (Ref. Fig. 035)
R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 (Ref. Fig. 035A)
 **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 (Ref. Fig. 036)
 1EFF : ALL 1 31-32-00Page A51 1 1 Aug 01/05 1 1 1CES 1

 CFDIU - Current Flight Report
 Figure 033

R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page A52 1401-499, 1Aug 01/05 1 1 1CES 1

 CFDIU - GMT/DATE INITIALIZATION Figure 034 
R 1EFF : 1 1 1CES  ALL  1 111 31-32-00 Page A53 May 01/05

 PFR/FILTER PROGRAM - Sheet 1/4
 Figure 035

R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 31-32-00Page A54 1201-207, 1May 01/05 1 1 1CES 1

 PFR/FILTER PROGRAM - Sheet 1/4
 Figure 035A

R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page A55 1401-499, 1Aug 01/05 1 1 1CES 1

 CFDIU - POST FLIGHT REPORT (Not Filtered) - Sheet 2/4
 Figure 036

R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 31-32-00Page A56 1201-207, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,

 (Ref. Fig. 036A)
 **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 (Ref. Fig. 037)
　
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