R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 30 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Item |MCDU |Value or | | | | |/GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | HPT and LPT variation are programmable | | | | | | in the range from 0.0 to 99.9%. | | | |----|------|-----------------------------------------|------|---------| |6001|6 | Independent from the other logic a best | | | |6002| | stable frame search logic for an Engine | | | |6003| | Cruise Report <01> is be started as long| | | | | | as 'X01' is not zero (once per leg | | | | | | only). | | | |6004| | | | | |6005| | Each time when an Engine Cruise Report | | | | . | | <01> is generated by this logic, the | | | | . | | number 'X01' is decremented until zero | | | | . | | is reached. | | | | . | | | | | | | | The start value of 'X01' is programmable| | | |600X| | | | | | | | | | | | | | In case of change of engine serial | | | | | | number 'X01' is automatically set to 5 | | | | | | | | | | |6.1 | Number 'X01' for consecutive reports up | C | T22/T23/| | | | to 9 | | T23A | |----|------|-----------------------------------------|------|---------| |7000|7 | In case the ENGINE DIVERGENCE REPORT | | | | | | <09> was generated, the stable frame | | | | | | search logic for the ENGINE CRUISE | | | | | | REPORT <01> is be started immediately | | | | | | independent of the best stable frame | | | | | | logic and the report is generated with | | | | | | code 7000. | | | | | | | | | | | | In case there are further Divergence | | | | | | Reports generated before a Cruise Report| | | | | | has been initiated, there is only one | | | | | | Engine Cruise Report. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ01'| | | | | | The report <01> is immediately | | | | | | generated and transmitted to the ACARS | | | | | | MU. | | | |----|------|-----------------------------------------|------|---------| |8200|8.2 | ACARS MU uplink request with IMI 'G01': | | |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 31 1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Item |MCDU |Value or | | | | |/GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | | | The report <01> is generated as soon as | | | | | | stable frame criteria are met, i.e. the | | | | | | DMU immediately starts searching for | | | | | | stable frame criteria independant of any| | | | | | other logic. | | | |----|------|-----------------------------------------|------|---------| | |9 | The parameters VN, VL, PHA, PHT and N1 | | | | | | in report line V3 and V4 are from the | | | | | | last stable descent. This means that the| | | | | | a.m. parameters are computed during | | | | | | descent (PH 7.1) when N1 is within N1 | | | | | | target 'N1T.1'+/- a tolerance band of | | | | | | 'X1.1' %rpm. This stable condition is | | | | | | kept for a time period of 'T1.1' | | | | | | seconds. The vibration parameters are | | | | | | an average of the 'T1.1' observing time | | | | | | period and stored in the DMU until the | | | | | | next stable descent is detected. In case| | | | | | of report generation, the last stored | | | | | | value is printed. | | | | |9.1 |'N1T.1' %rpm stable N1 value for descent.| C | T22/T23/| | | | | | T23A | | |9.2 | 'X1.1' %rpm tolerance band for descent. | C | T22/T23/| | | | | | T23A | | |9.3 | 'T1.1' seconds stable observing time for| C | T22/T23/| | | | descent (max. 20 sec). | | T23A | |----|------|-----------------------------------------|------|---------| | |10 | The parameters VN, VL, PHA, PHT and N1 | | | | | | in report line V5 and V6 are from the | | | | | | last stable take-off. This means that | | | | | | the a.m. parameters are computed during | | | | | | climb (PH 5.1) when N1 is within N1 | | | | | | target 'N1T.2'+/- a tolerance band of | | | | | | 'X1.2' %rpm. This stable condition is | | | | | | kept for a time period of 'T1.2' | | | | | | seconds. The vibration parameters are | | | | | | an average of the 'T1.2' observing time | | | | | | period and stored in the DMU until the | | | | | | next stable take-off is detected. In | | | | | | case of report generation, the last | | | | | | stored value is printed. | | | | | | | | |
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page 32
1 1 Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Item |MCDU |Value or | | | | |/GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |10.1 | 'N1T.2' %rpm stable N1 value for climb. | C | T22/T23/| | | | | | T23A | | |10.2 | 'X1.2' %rpm tolerence band for climb. | C | T22/T23/| | | | | | T23A | | |10.3 | 'T1.2' seconds stable observing time for| C | T22/T23/| | | | climb (max. 20 sec). | | T23A | |----------------------------------------------------------------------| | A = Programmable by Airbus Industrie | | C = Programmable by Customer | +----------------------------------------------------------------------+ 中國航空網(wǎng) 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(tǒng) 4(169)
