R 1EFF : 159-199, 210-210, 1 31-37-73Page B0 1 1 May 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(2) Engine Start Report Logic <10> (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 | 2 | | |E | Transfer to ACARS MU | C | No | | |F | Increment of the report counter if the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | | |G | 'Y10.1' Pre-event print interval in sec.| C | 5 | | |H | 'Y10.2'Post-event print interval in sec.| C | 2 | | |I | 'Y10.3' time in seconds when Fuel Flow | AI | 20 | | | | is measured after SAV = open | | | |----|------|-----------------------------------------|------|---------| |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 | 1.1 | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | |----|------|-----------------------------------------|------|---------| | |4 | Aborted engine 1 or 2 start detecetd | | | | | | by FADEC: | | | | | | Start Abort Active | | | | | | Eng.1 param. 7C.1.270.01.26 = 1 | | | | | | Eng.2 param. 7C.2.270.10.26 = 1 | | | | | | | | | | |4.1 | Logic algorithm | | | | | | The report is generated if the a.m. | | | | | | Start Abort Active bit and one of the | | | | | | following bits (item 4.1.1 to 4.1.8) of | | | | | | the same engine are set to '1'. | | | | | | | | | |4410|4.1.1 | Start Abort = SAV Demand/Position | | | | | | Disagree | | |
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page B1 1201-209, 1May 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | Eng.1 param. 7C.1.270.01.15 = 1 | | | | | | Eng.2 param. 7C.2.270.10.15 = 1 | | | |4420|4.1.2 | Start Abort = HPSOV Demand/Position | | | | | | Disagree | | | | | | Eng.1 param. 7C.1.270.01.16 = 1 | | | | | | Eng.2 param. 7C.2.270.10.16 = 1 | | | |4430|4.1.3 | Start Abort = EGT Overtemperature | | | | | | Deteceted | | | | | | Eng.1 param. 7C.1.270.01.17 = 1 | | | | | | Eng.2 param. 7C.2.270.10.17 = 1 | | | |4440|4.1.4 | Start Abort = Stall Deteceted | | | | | | Eng.1 param. 7C.1.270.01.18 = 1 | | | | | | Eng.2 param. 7C.2.270.10.18 = 1 | | | |4450|4.1.5 | Start Abort = No Engine Lightoff | | | | | | Deteceted | | | | | | Eng.1 param. 7C.1.270.01.20 = 1 | | | | | | Eng.2 param. 7C.2.270.10.20 = 1 | | | |4460|4.1.6 | Hung Start | | | | | | Eng.1 param. 7C.1.270.01.21 = 1 | | | | | | Eng.2 param. 7C.2.270.10.21 = 1 | | | | | | or | | | | | | Eng.1 param. 7C.1.270.01.22 = 1 | | | | | | Eng.2 param. 7C.2.270.10.22 = 1 | | | |4470|4.1.7 | Start Abort = Illegal Start Sequence | | | | | | Eng.1 param. 7C.1.270.01.24 = 1 | | | | | | Eng.2 param. 7C.2.270.10.24 = 1 | | | |4480|4.1.8 | Slow Start Deteceted | | | | | | Eng.1 param. 7C.1.270.01.25 = 1 | | | | | | Eng.2 param. 7C.2.270.10.25 = 1 | | | | | | | | | | |4.2 | It is possible to suppress each logic | | | | | | item individually via MCDU. | | | |----|------|-----------------------------------------|------|---------| |5000|5 | In case of exceedance of EGTL during | | | | | | appropriate engine start. | | | | |5.1 | EGTL limit in C | C | T22/T23 | |----|------|-----------------------------------------|------|---------| |6000|6 | Every 'F10.1'th cycle at the moment when| | | | | | N2 =/> N2 trigger during engine start. | | | | | | Eng.1 param. 7C.1.344.01 | | | | | | Eng.2 param. 7C.2.344.10 | | | | |6.1 | 'F10.1' cycle | C | T22/T23 |
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page B2 1201-209, 1May 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |6.2 | N2 trigger value in %rpm | C | T22/T23 | | |6.3 | In case 7 post-event data sets is | C | T22/T23 | | | | printed out. | | | |----|------|-----------------------------------------|------|---------| |7001|7 | A programmable number 'X10' of consecu- | | | |7002| | tive legs. | | | |7003| | This means: During the next 'X10' legs | | | |7004| | the engine start report is automatically| | | |7005| | be generated when N2 = N2trigger during | | | | . | | appropriate engine start. | | | | . | | | | | |700X|7.1 | Number 'X10' for consecutive legs | C | T22/T23 | | | | programmable up to 9. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ10'| | | | | | The report <10> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----|------|-----------------------------------------|------|---------| |8200|8.2 | ACARS MU uplink request IMI 'G10': | | | | | | The report <10> is generated at the next| | | | | | start of engine 1 and 2 when N2 = N2 | | | | | | trigger after entering PH1.1. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
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