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R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 26 1 1 Aug 01/05 1 1 1CES 1 (2) Engine Cruise Report <01> for (Engine Type CFMI with Advanced EVMU)
+----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of 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 of the | C | 1 | | | | report was triggered by a code number | | | | | | > 1000; 1=yes, 0=no | | | | |G | Average intervals in seconds | C | 20 | | |H | Overall Average of 'F01' averages | C | 5 | | |I.1 | OIQ 'Y01.5' seconds before flight phase | A | 5 | | | | change from 2 to 3 | | | | |I.2 | OIQ 'Y01.4' seconds after beginning of | A | 10 | | | | flight phase 9. | | | |----|------|-----------------------------------------|------|---------| |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 | | | | | | assign. | |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | | | | | | progr. | |----|------|-----------------------------------------|------|---------| |4000| | The DMU shall generate the Engine | | | | | | Cruise Report based on 'Flight Hours' | | | | | | or 'Flight Legs' programmable via GSE | | | | | | | | | | | | Logic based on Flight Hours: | | | | | | | | | | | | After starting each new time period of | | | | | | 'Y01.1' flight hours and during the | | | | | | first entry into flight phase 6 after | | | | | | 'Y01.2' minutes the stable frame | | | | | | criteria are not met then an Engine | | | | | | Cruise Report is generated and stored | | | | | | in the report buffer. The report has the| | |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 27 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Item |MCDU |Value or | | | | |/GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | subsequent message in the last line: | | | | | | NO STABLE FRAME CONDITION | | | | | | | | | | | | Logic based on Flight Legs: | | | | | | | | | | | | Every 'Y01.3' flight legs and if 'Y01.2'| | | | | | minutes after entry in cruise phase the | | | | | | stable frame criteria is not met, an | | | | | | Engine Cruise Report is be generated and| | | | | | stored in the report buffer. The report | | | | | | has the subsequent message in the last | | | | | | line: | | | | | | NO STABLE FRAME CONDITION | | | | | | | | | | | | In this case the average interval is | | | | | | fixed at 20 seconds. | | | | | | | | | | |4 | The default programming is 'Flight Legs'| C | Legs | |----|------|-----------------------------------------|------|---------| | |4.1 | 'Y01.1' flight hours | C | T22/T23/| | | | | | T23A | | |4.2 | 'Y01.2' minutes after cruise | C | T22/T23/| | | | | | T23A | | |4.3 | 'Y01.3' flight legs | C | T22/T23/| | | | | | T23A | |----|------|-----------------------------------------|------|---------| |5000| | The DMU generates the Cruise Performance| | | | | | Report based on 'Flight Hours' or | | | | | | 'Flight Legs' programmable via GSE. | | | | | | | | | | | | Logic based on Flight Hours: | | | | | | | | | | | | During a time frame of 'Y01.1' flight | | | | | | hours the DMU searches in flight phase | | | | | | 6 for report generation with stable | | | | | | frame criteria where the best aircraft | | | | | | quality number QE is calculated. The | | | | | | report with the best quality number QE | | | | | | is stored in the report buffer and the | | | | | | report stored according to logic 4000 is| | | | | | then deleted. | | | | | | | | |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 28
1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Item |MCDU |Value or | | | | |/GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | Logic based on Flight Legs: | | | | | | | | | | | | Every 'Y01.3' flight legs the DMU | | | | | | searches in flight phase 6 for report | | | | | | generation with stable frame criteria | | | | | | where the best aircraft quality number | | | | | | QE is calculated. The report with the | | | | | | best quality number QE is stored in the | | | | | | report buffer and the report which is | | | | | | stored according to logic 4000 is then | | | | | | deleted. | | | | | | | | | | |5 | The default programming shall be | C | Legs | | | | 'Flight Legs' | | | |----|------|-----------------------------------------|------|---------| 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 指示/记录系统 4(167)
