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R  |  |  | HPT and LPT variation are programmable  |  |  | 
R  |  |  | in the range from 0.0 to 99.9 %.  |  |  | 
R  |----|------|-----------------------------------------|------|---------| 
R  |  |6  | The parameters VN, VL, PHA and N1 in  |  |  | 
R  |  |  | report line V3 and V4 are from the last |  |  | 
R  |  |  | stable descent. This means that the a.m.|  |  | 
R  |  |  | parameters are computed during descent  |  |  | 
R  |  |  | (PH 7.1) when N1 is within N1 target  |  |  | 
R  |  |  | 'N1T.1' +/- a tolerence band of 'X1.1'% |  |  | 
R  |  |  | rpm. This stable condition is kept for a|  |  | 
R  |  |  | time period of 'T1.1' seconds. The  |  |  | 
R  |  |  | vibration parameters are averaged about |  |  | 

R 1EFF : 159-199, 210-210, 1 31-37-73Page 85 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|
 |----|------|-----------------------------------------|------|---------| 
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 | +----------------------------------------------------------------------+
　
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