R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page B3 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 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 | | | |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 | '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 | A | 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 | | | | | | progr. | |----|------|-----------------------------------------|------|---------|
| |4 | Aborted engine 1 or 2 start detected | | |
| | | by FADEC: | | |
| | | Start Abort Active | | |
| | | Engine 1 7C.1.270.01.26 = 1 | | |
| | | Engine 2 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 | | |
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page B4 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| |----|------|-----------------------------------------|------|---------| | | | Disagree | | | | | | Engine 1 7C.1.270.01.15 = 1 | | | | | | Engine 2 7C.2.270.10.15 = 1 | | | |4420|4.1.2 | Start Abort = HPSOV Demand/Position | | | | | | Disagree | | | | | | Engine 1 7C.1.270.01.16 = 1 | | | | | | Engine 2 7C.2.270.10.16 = 1 | | | |4430|4.1.3 | Start Abort = EGT Overtemperature | | | | | | Deteceted | | | | | | Engine 1 7C.1.270.01.17 = 1 | | | | | | Engine 2 7C.2.270.10.17 = 1 | | | |4440|4.1.4 | Start Abort = Stall Deteceted | | | | | | Engine 1 7C.1.270.01.18 = 1 | | | | | | Engine 2 7C.2.270.10.18 = 1 | | | |4450|4.1.5 | Start Abort = No Engine Lightoff | | | | | | Deteceted | | | | | | Engine 1 7C.1.270.01.20 = 1 | | | | | | Engine 2 7C.2.270.10.20 = 1 | | | |4460|4.1.6 | Hung Start | | | | | | Engine 1 7C.1.270.01.21 = 1 | | | | | | Engine 2 7C.2.270.10.21 = 1 | | | | | | or | | | | | | Engine 1 7C.1.270.01.15 = 1 | | | | | | Engine 2 7C.2.270.10.15 = 1 | | | |4470|4.1.7 | Start Abort = Illegal Start Sequence | | | | | | Engine 1 7C.1.270.01.24 = 1 | | | | | | Engine 2 7C.2.270.10.24 = 1 | | | |4480|4.1.8 | Slow Start Deteceted | | | | | | Engine 1 7C.1.270.01.25 = 1 | | | | | | Engine 2 7C.2.270.10.25 = 1 | | | | | | | | | | |4.2 | It is possible to suppress each logic | | | | | | item individually via the MCDU. | | | |----|------|-----------------------------------------|------|---------| |5000|5 | In case of exceedance of EGTL during | | | | | | appropriate engine start. | | | | |5.1 | EGTL limit in C | C | T22/T23/| | | | | | T23A | |----|------|-----------------------------------------|------|---------| |6000|6 | Every 'F10.1'th cycle at the moment when| | | | | | N2 is equal or greater than N2trigger | | | | | | during engine start. | | |
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page B5 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| |----|------|-----------------------------------------|------|---------| | | | N2 Engine 1 7C.1.344.01 | | | | | | Engine 2 7C.2.344.10 | | | | |6.1 | 'F10.1' cycle | C | T22/T23/| | | | | | T23A | | |6.2 | N2 trigger value in %rpm | C | T22/T23/| | | | | | T23A | | |6.3 | In this case 7 post-event data sets are | | | | | | printed out. | | | |----|------|-----------------------------------------|------|---------| |7001|7 | A programmable number 'X10' of | | | |. | | consecutive legs. | | | |7002| | | | | |7003| | This means: During the next 'X10' legs | | | |7004| | the engine start report is automatically| | | |7005| | generated when N2 >= N2trigger during | | | |. | | appropriate engine start. | | | |. | | | | | |700X|7.1 | Number 'X10' for consecutive legs | C | T22/T23/| | | | programmable up to 9. | | T23A | |----|------|-----------------------------------------|------|---------| |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 <01> is generated at the next| | | | | | start of engine 1 and 2 (2 reports) when| | | | | | N2 = N2trigger after entering flight | | | | | | phase 1.1 (based on code 6000). | | | |----------------------------------------------------------------------| | A = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 指示/記錄系統 5(69)
