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R  |  |  | 'X1.1' %rpm. This stable condition is  |  |  | 
R  |  |  | kept for a time period of 'T1.1'  |  |  | 
R  |  |  | seconds. The vibration parameters are  |  |  | 
R  |  |  | an average of the 'T1.1' observing time |  |  | 
R  |  |  | period and stored in the DMU until the  |  |  | 
R  |  |  | next stable descent is detected. In case|  |  | 
R  |  |  | of report generation, the last stored  |  |  | 
R  |  |  | value is printed.  |  |  | 
R  |  |9.1  | 'N1T.1 %rpm stable N1 value for descent.|  |  | 
R  |  |  |  |  |  | 
R  |  |9.2  | 'X1.1' %rpm tolerence band for descent. |  |  | 
R  |  |  |  |  |  | 
R  |  |9.3  | 'T1.1' seconds stable observing time for|  |  | 
R  |  |  | descent (max. 20 sec).  |  |  | 
R  |----|------|-----------------------------------------|------|---------| 
R  |  |10  | The parameters VN, VL, PHA, PHT and N1  |  |  | 
R  |  |  | in report line V5 and V6 are from the  |  |  | 
R  |  |  | last stable takeoff. This means that the|  |  | 
R  |  |  | a.m. parameters are computed during  |  |  | 
R  |  |  | climb (PH 5.1) when N1 is within N1  |  |  | 
R  |  |  | target 'N1T.2'+/- a tolerance band of  |  |  | 
R  |  |  | 'X1.2' %rpm. This stable condition is  |  |  | 
R  |  |  | kept for a time period of 'T1.2'  |  |  | 
R  |  |  | seconds. The vibration parameters are  |  |  | 
R  |  |  | an average of the 'T1.2' observing time |  |  | 
R  |  |  | period and stored in the DMU until the  |  |  | 
R  |  |  | next stable takeoff is detected. In case|  |  | 
R  |  |  | of report generation, the last stored  |  |  | 
R  |  |  | value is printed.  |  |  | 
R  |  |  |  |  |  | 
R  |  |10.1  | 'N1T.2 %rpm stable N1 value for climb.  |  |  | 
R  |  |  |  |  |  | 
R  |  |10.2  | 'X1.1' %rpm tolerence band for climb.  |  |  | 

R 1EFF : 159-199, 210-210, 1 31-37-73Page 48 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 31-37-73Page 49 1 1 May 01/05 1 1 1CES 1

 +----------------------------------------------------------------------+
 |Code|Item | |Progr.|Standard |
 | No.|No. | Description of Item |MCDU |Value or |
 | | | |/GSE |Table TXY|
 |----|------|-----------------------------------------|------|---------| 
R  | | | | | | 
R  | |10.3 | 'T1.2' seconds stable observing time for| | | 
R  | | | climb (max. 20 sec). | | | 
R  |----------------------------------------------------------------------| 
R  | AI = Programmable by Airbus Industrie | 
R  | C = Programmable by Customer | 
R  +----------------------------------------------------------------------+
 **ON A/C ALL
 B. Cruise Performance Report <02>
 (Ref. Fig. 002)
 The cruise performance report is a collection of aircraft and engine
 information averaged over a period of time in which both the engine and
 the aircraft met the appropriate stability criteria. The cruise
 performance report is generated when one of the logic conditions 1000 to
 5000 (for details see cruise performance report logic) is present. 
R  **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
 (1) Cruise Performance Report Data Field Description <02> (Engine Type
 CFMI with Advanced EVMU)
 +---------------------------------------------------------------------+
 | Value | Content Description |
 |--------------|------------------------------------------------------|
 | TAT/ALT/CAS/| In the report line CE is the averange value for |
 | MN/GW/CG | F02 * 20 sec. of System 1 parameters printed. |
　
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