R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A56 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 Mechanical Advisory Report Logic <07> (Engine Type CFMI with 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 | 'Y07.1' Pre-event intervals in | C | 4 | | | | seconds. | | | | |H | 'Y07.2' Post-event intervals in | C | 5 | | | | seconds. | | | | |I | Max. No. of reports per trigger engine | C | 10 | | | | and flight leg. | | | | |J | Max. No. of reports per engine and | C | 50 | | | | flight 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. | |----|------|-----------------------------------------|------|---------| |4110|4 | OIT > OITL1 in all flight phases | | | |4120| | OIT > OITL2 in all flight phases | | | |4130| | OIT > OITL3 for 'Y07.3' min. in all | | | | | | flight phases | | | |4210| | OIP < OIPL1.1 at N2L2.1 in flight phases| | | | | | 2, 3 and 9 | | | |4220| | OIP < OIPL1.2 at N2L2.2 in flight phases| | |
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A57 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| |----|------|-----------------------------------------|------|---------|
| | | 4 thru 8 | | |
|4230| | OIP > OIPL2 in all flight phases | | |
|4310| | VB1 is above Advisory Level in all | | |
| | | flight phases | | |
| | | EVMU 3D.1.035.01.11 Engine 1 | | |
| | | 3D.1.035.10.11 Engine 2 | | |
|4320| | VB2 is above Advisory Level in all | | |
| | | flight phases | | |
| | | EVMU 3D.1.035.01.12 Engine 1 | | |
| | | 3D.1.035.10.12 Engine 2 | | |
| | | | | |
| |4.1.1 | OITL1 limit in C (yellow limit) | C | T22/T23/|
| | | | | T23A |
| |4.1.2 | OITL2 limit in C (red limit) | C | T22/T23/|
| | | | | T23A |
| |4.1.3 | OITL3 limit in C | C | T22/T23/|
| | | | | T23A |
| |4.1.4 | 'Y07.3' time limit in minutes | C | T22/T23/|
| | | | | T23A |
| |4.2.1 | OIPL1.1 limit defined in the following | A | T22/T23/|
| | | table: | | T23A |
| | | (linear interpolation and linear | | |
| | | extrapolation below 50% and above 100%)| | |
| | | OIPL1.1 (psia) | N2L2.1 (%rpm) | | |
| | | ________________|_______________ | | |
| | | 0 | 0 | | |
| | | 0 | 54 | | |
| | | 13 | 55 | | |
| | | 13 | 65 | | |
| | | 38 | 105 | | |
| | | | | |
| |4.2.2 | OIPL1.2 defined in the following table: | A | T22/T23/|
| | | (linear interpolation and linear | | T23A |
| | | extrapolation below 50% and above 100%)| | |
| | | OIPL1.2 (psia) | N2L2.2 (%rpm) | | |
| | | ________________|_______________ | | |
| | | 0 | 0 | | |
| | | 0 | 54 | | |
| | | 13 | 55 | | |
| | | 13 | 65 | | |
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 5(50)
