R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A40 1201-209, 1May 01/05 1 1 1CES 1

R **ON A/C 106-149, 159-199, 210-299, 301-399, 401-499,

 (2) Engine Gas Path Advisory Report Logic <06> (Engine Type CFMI with Advanced EVMU)
 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |A | Report Format | | | | |B | Parameter Table | | | | |C | First three lines of Report | C | Blank | | |D | Print Out Rules | C | | | |E | Transfer to ACARS MU | C | Yes | | |F | Increment of the report counter if the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | | |G | 'Y06.1' Pre-event print intervals in | C | 6 | | | | seconds. | | | | |H | 'Y06.2' Post-event print intervals in | C | 5 | | | | seconds. | | | | |I | 'M06.1' Number of Post-event data set | C | 5 | | | | up to 20. | | | | |J | Max. No. of reports per trigger, engine | C | 10 | | | | and flight leg. | | | | |K | Max. No of reports per engine and flight| C | 50 | | | | leg. | | | |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Remote Print Button assignment. | C | not | | | | | | assigned| |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | | | | | | progr. | |----|------|-----------------------------------------|------|---------| |4000|4 | Report generation, if Stall bit is set | | | | | | to '1'. | | | | | | Eng.1 param. 7C.1.270.01.18 = 1 | | | | | | Eng.2 param. 7C.2.270.10.18 = 1 | | | |----|------|-----------------------------------------|------|---------|
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A41 1401-499, 1Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| |5100|5 | EGT > EGTL1 in Flight Phases 3, 4, 5 | | | | | | or | | | |5200| | EGT > EGTL2 in all PH except | | | | | | PH 1.1, 3, 4, 5 | | | | | | or | | | |5300| | EGT > EGTL3 in all PH | | | | | | or | | | |5400| | N1 > N1L1.1 in all PH | | | | | | or | | | |5500| | N1 > N1L1.2 in all PH | | | | | | or | | | |5600| | N2 > N2L1.1 in all PH | | | | | | or | | | |5700| | N2 > N2L1.2 in all PH | | | | | | | | | | |5.1 | EGTL1 limit in C | C | T22/T23/| | | | | | T23A | | |5.2 | EGTL2 limit in C (yellow limit) | C | T22/T23/| | | | | | T23A | | |5.3 | EGTL3 limit in C (red limit) | C | T22/T23/| | | | | | T23A | | |5.4 | N1L1.1 limit in %rpm (yellow limit) | C | T22/T23/| | | | | | T23A | | |5.5 | N1L1.2 limit in %rpm (red limit) | C | T22/T23/| | | | | | T23A | | |5.6 | N2L1.1 limit in %rpm (yellow limit) | C | T22/T23/| | | | | | T23A | | |5.7 | N2L1.2 limit in %rpm (red limit) | C | T22/T23/| | | | | | T23A | |----|------|-----------------------------------------|------|---------| |6000|6 | If in PH 5, 5.1, 6, 7, 7.1 the fuel | | | | | | shut off valve is closed. | | | | | | 7C.1.270.01.14 = 1 or | | | | | | 7C.2.270.10.14 = 1 | | | | | | The report generation is only performed | | | | | | in the case that the status of the 'fuel| | | | | | shut off valve' = 1 is stable for at | | | | | | least 4 seconds. | | | |----|------|-----------------------------------------|------|---------| | |7 | Report Generation stops when exceedance | | | | | | parameter is again within its limits or | | | | | | 'M06.1' is reached. | | |

R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A42 1401-499, 1Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ06'| | | | | | The report <06> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| |  A  =  Programmable by Airbus Industrie | |  C  =  Programmable by Customer | +----------------------------------------------------------------------+

 **ON A/C ALL
 F. Engine Mechanical Advisory Report <07>
 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
 (Ref. Fig. 007)