R 1EFF : 159-199, 210-210, 1 31-37-73Page 85 1 1 May 01/05 1 1 1CES 1
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|Code|Item | |Progr.|Standard |
| No.|No. | Description of Function Item |MCDU |Value or |
| | | |GSE |Table TXY|
|----|------|-----------------------------------------|------|---------|
R | | | the 'T1.1' observing time period and | | |
R | | | stored in the DMU until the next stable | | |
R | | | descent is detected. In case of report | | |
R | | | generation the last stored value is | | |
R | | | printed. | | |
R | |6.1 | 'N1T.1' %rpm stable N1 value for descent| C | T22/T23/|
R | | | | | T23A |
R | |6.2 | 'X1.1' %rpm tolerance band for descent | C | T22/T23/|
R | | | | | T23A |
R | |6.3 | 'T1.1' seconds stable observing time | C | T22/T23/|
R | | | for descent (max. 20 sec). | | T23A |
R |----|------|-----------------------------------------|------|---------|
R | |7 | The parameters VN, VL, PHA, PHT and N1 | | |
R | | | report line V5 and V6 are from the last | | |
R | | | stable take off. This means the a.m. | | |
R | | | parameters are computed during climb | | |
R | | | (PH 5.1) when N1 is within N1target | | |
R | | | 'N1T.2' +/- a tolerance band of 'X1.2' | | |
R | | | %rpm. This stable condition is kept | | |
R | | | for a time period of 'T1.2' seconds. The| | |
R | | | vibration parameters are averaged for | | |
R | | | the 'T1.2' observing time period and | | |
R | | | stored in the DMU until the next stable | | |
R | | | take off is detected. In case of report | | |
R | | | generation the last stored value is | | |
R | | | printed. | | |
R | | | | | |
R | |7.1 | 'N1T.2' %rpm stable N1 value for climb | C | T22/T23/|
R | | | | | T23A |
R | |7.2 | 'X1.2' %rpm tolerance band for climb | C | T22/T23/|
R | | | | | T23A |
R | |7.3 | 'T1.2' seconds stable observing time for| C | T22/T23/|
R | | | climb (max. 20 sec) | | T23A |
R |----|------|-----------------------------------------|------|---------|
R |8100|8.1 | ACARS MU uplink request with IMI 'REQ02'| | |
R | | | The report <02> is immediately generated| | |
R | | | and transmitted to the ACARS MU. | | |
R |----|------|-----------------------------------------|------|---------|
R |8200|8.2 | ACARS MU uplink request with INI 'G02' | | |
R | | | The report <02> is generated as soon as | | |
R | | | stable frame criteria are met, i.e. the | | |
R | | | DMU is immediately starts searching for | | |
R 1EFF : 159-199, 210-210, 1 31-37-73Page 86 1 1 May 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | stable frame criteria independant of | | | | | | any other logic. | | | |----------------------------------------------------------------------| | AI = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+ 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(25)