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R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A7 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| |----|------|-----------------------------------------|------|---------| |----|------|-----------------------------------------|------|---------| |1000|1 | Manual selection via MCDU | | | |----|------|-----------------------------------------|------|---------| |2000|2 | Flight phase dependent manual | | | | | | selection via remote print button | | | | | | if programmed. | | | | |2.1 | Remote Print Button assignment. | C | not | | | | | | assigned| |----|------|-----------------------------------------|------|---------| |3000|3 | Programmable Start Logic | | | | |3.1 | Trigger condition | C | not | | | | | | progr. | |----|------|-----------------------------------------|------|---------|

 |4000|4  | The report is generated and stored every|  |  |
 |  |  | 'F04'th Take-Off and is triggered when, |  |  |
 |  |  | during a searching time period of 20 |  |  |
 |  |  | seconds, the sum of the EGT of both |  |  |
 |  |  | engines is maximal. The searching time |  |  |
 |  |  | period is started 'Y04.1' seconds after |  |  |
 |  |  | entering flight phase 4. |  |  |
 |  |  | The trigger stays armed during flight |  |  |
 |  |  | phase 5. |  |  |
 |  |  | |  |  |
 |  |4.1  | The report is postponed to the next |  |  |
 |  |  | flight leg if at least one of the EGT |  |  |
 |  |  | values on Eng.1 or Eng.2 is below EGTL |  |  |
 |  |  | at the moment when the starter air valve|  |  |
 |  |  | switches from the closed position to the|  |  |
 |  |  | open position at engine start. |  |  |
 |  |  | Starter Air Valve open: |  |  |
 |  |  | Eng.1 param. 7C.1.270.01.13 = 1 |  |  |
 |  |  | Eng.2 param. 7C.2.270.10.13 = 1 |  |  |
 |  |  | |  |  |
 |  |  | or |  |  |
 |  |  | |  |  |
 |  |  | if the Wing Anti-Ice Status or the Na-|  |  |
 |  |  | celle Anti-Ice Status is switched during|  |  |
 |  |  | the search time period. |  |  |
 |  |  | |  |  |
 |  |  | Wing Anti-Ice Valve closed: |  |  |
 |  |  | param. 29.1.001.00.18 = 0 right hand |  |  |
 |  |  | 29.2.001.00.18 = 0 |  |  | 

R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A8 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| |----|------|-----------------------------------------|------|---------| | | | param. 29.1.001.11.18 = 0 left hand | | | | | | 29.2.001.11.18 = 0 | | | | | | Nacelle Anti-Ice Valve closed: | | | | | | Eng.1 param. 5D.2.061.10.28 = 0 | | | | | | Eng.2 param. 5D.2.061.10.27 = 0 | | | |----|------|-----------------------------------------|------|---------| |4100|4.1.1 | The same rules as described for Log. No.| C | disarmed|

 |  |  | 4000 is valid and in addition the report|  |  |
 |  |  | is postponed when the Wing Anti-Ice  |  |  |
 |  |  | Status or the Nacelle Anti-Ice Status is|  |  |
 |  |  | open during the search time period. This|  |  |
 |  |  | trigger condition is basically disarmend|  |  |
 |  |  | and can be armed via a GSE programmable.|  |  |
 |  |  |  |  |  |
 |  |4.2  | The report trigger logic is restarted in|  |  |
 |  |  | flight leg 'F04+n' (n=1, 2, ..F04) after|  |  |
 |  |  | no report generation in the previous leg|  |  |
 |  |  | 'F04+ (n-1)'.  |  |  |
 |  |  |  |  |  |
 |  |4.3  | EGTL  | C  | T22/T23/|
 |  |  |  |  | T23A  |
 |  |4.4  | 'F04'th Take Off  | C  | T22/T23/|
　
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