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 |  |  |  |  | T23A  |
 |  |4.5  | 'Y04.1' seconds after PH 4 entry  | C  | T22/T23/|
 |  |  |  |  | T23A  |
 |  |4.6  | T/O delta N1 summary limits  |  |  |
 |  |  | delta N1 = N1MX - N1  |  |  |
 |  |  | N1MX = 7C.1.342.01 Eng.1  |  |  |
 |  |  |  7C.2.342.10 Eng.2  |  |  |
 |  |  | N1  = 7C.1.346.01 Eng.1  |  |  |
 |  |  |  7C.2.346.10 Eng.2  |  |  |
 |  |  |  |  |  |
 |  |4.7.1 | delta N1 is more than 10% rpm.  | C  | T11/T23/|
 |  |  |  |  | T23A  |
 |  |4.7.2 | delta N1 is more than 8% rpm and is  | C  | T11/T23/|
 |  |  | equal or less than 10% rpm.  |  | T23A  |
 |  |4.7.3 | delta N1 is more than 6% rpm and is  | C  | T11/T23/|
 |  |  | equal or less than 8% rpm.  |  | T23A  |
 |  |4.7.4 | delta N1 is more than 4% rpm and is  | C  | T11/T23/|
 |  |  | equal or less than 6% rpm.  |  | T23A  |
 |  |4.7.5 | delta N1 is more than 2% rpm and is  | C  | T11/T23/|
 |  |  | equal or less than 4% rpm.  |  | T23A  | 

R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A9

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| |----|------|-----------------------------------------|------|---------| | |4.7.6 | delta N1 is more than 0.2% rpm and is | C | T11/T23/| | | | equal or less than 2% rpm. | | T23A | | |4.7.7 | delta N1 is equal or less than 0.2% rpm.| C | T11/T23/| | | | | | T23A | | |4.8 | The calculation is made 'Y04.3' seconds | | | | | | after entry into flight phase 4. | | | | | | | | | | |4.8.1 | 'Y04.3' seconds after PH 4 entry. | C | T11/T23/| | | | | | T23A | |----|------|-----------------------------------------|------|---------| |5001|5 | Each time when a report is generated by | | | |5002| | this logic the number 'X04' is decreased| | | |5003| | until zero is reached. The conditions | | | |5004| | are described under code No. 4000/4001 | | | |5005| | (without item 4.2). | | | |. | | | | | |. | | The number (X04) is programmable. | | | |. | | | | | |. | | In case of change of the engine serial | | | |. | | number, (X04) are automatically set to | | | |. | | five. | | | |500X| | The code shows in an increasing order, | | | | | | i.e. the first report has the code 5001,| | | | | | the next code is 5002 and so on until | | | | | | 5005 is reached. | | | | | | | | | | |5.1 | Number 'X04' for consecutive legs up to | C | T22/T23/| | | | 9. | | T23A | | |5.2 | Number 'X04' in case of ESN change. | | 5 | | | | | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI | | | | | | 'REQ04': | | | | | | The report <04> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----|------|-----------------------------------------|------|---------| |8200|8.2 | ACARS MU uplink request with IMI 'G04': | | | | | | The report <04> is generated as the next| | | | | | take-off according to code 4000 or 4100 | | | | | | depending on which logic is armed. | | | |----------------------------------------------------------------------| |  A  =  Programmable by Airbus Industrie |

R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A10 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| |----|------|-----------------------------------------|------|---------| |  C  =  Programmable by Customer | +----------------------------------------------------------------------+

 **ON A/C ALL
 D. Engine Report On Request <05> (Ref. Fig. 005) The engine on request report is a time series collection of aircraft and engine parameters as a function of a manually initiated trigger. The report is generated when one of the logic conditions 1000 to 3000 (for details see engine report O/R logic) is present.

R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
 (1) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ESN | Engine Serial Number | | 999999 | (000000 to 999999) | | | Eng 1 param. 7C.1.046.01 digit 3, 2, 1 | | | 7C.1.047.01 digit 6, 5, 4 | | | Eng 2 param. 7C.2.046.01 digit 3, 2, 1 | | | 7C.2.047.01 digit 6, 5, 4 | |--------------|------------------------------------------------------| | EHRS | Engine Flight Hours | | 99999 | (00000 to 99999 hours) | | | DMU Engine 1 and Engine 2 | |--------------|------------------------------------------------------| | ERT | Engine Running Time | | 99999 | (00000 to 65536 hours) | | | Eng 1 param. 7C.1.050.01 | | | Eng 2 param. 7C.2.050.10 | |--------------|------------------------------------------------------| | ECYC | Engine Cycle | | 99999 | (00000 to 99999) | |--------------|------------------------------------------------------| | AP | Auto Pilot Status |
　
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