R 1EFF : 159-199, 210-210, 1 31-37-73Page 43 1 1 May 01/05 1 1 1CES 1

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 |Code|Item | |Progr.|Standard |
 | No.|No. | Description of Item |MCDU |Value or |
 | | | |/GSE |Table TXY|
 |----|------|-----------------------------------------|------|---------| 
R  | | | sunsequent message in the last line: | | | 
R  | | | NO STABLE FRAME CONDITION | | | 
R  | | | | | | 
R  | | | Logic based on Flight Legs: | | | 
R  | | | | | | 
R  | | | Every 'Y01.3' flight legs and if 'Y01.2'| | | 
R  | | | minutes after entry in cruise phase the | | | 
R  | | | stable frame criteria is not met, an | | | 
R  | | | Engine Cruise Report is be generated and| | | 
R  | | | stored in the report buffer. The report | | | 
R  | | | has the subsequent message in the last | | | 
R  | | | line: | | | 
R  | | | NO STABLE FRAME CONDITION | | | 
R  | | | | | | 
R  | | | In this case the average interval is | | | 
R  | | | fixed at 20 seconds. | | | 
R  | | | | | | 
R  | |4 | The default programming is 'Flight Legs'| C | Legs | 
R  |----|------|-----------------------------------------|------|---------| 
R  | |4.1 | 'Y01.1' flight hours | C | T22/T23/| 
R  | | | | | T23A | 
R  | |4.2 | 'Y01.2' minutes after cruise | C | T22/T23/| 
R  | | | | | T23A | 
R  | |4.3 | 'Y01.3' flight legs | C | T22/T23/| 
R  | | | | | T23A | 
R  |----|------|-----------------------------------------|------|---------| 
R  |5000| | The DMU generates the Cruise Performance| | | 
R  | | | Report based on 'Flight Hours' or | | | 
R  | | | 'Flight Legs' programmable via GSE. | | | 
R  | | | | | | 
R  | | | Logic based on Flight Hours: | | | 
R  | | | | | | 
R  | | | During a time frame of 'Y01.1' flight | | | 
R  | | | hours the DMU searches in flight phase | | | 
R  | | | 6 for report generation with stable | | | 
R  | | | frame criteria where the best aircraft | | | 
R  | | | quality number QE is calculated. The | | | 
R  | | | report with the best quality number QE | | | 
R  | | | is stored in the report buffer and the | | | 
R  | | | report stored according to logic 4000 is| | | 
R  | | | then deleted. | | | 
R  | | | | | | 

R 1EFF : 159-199, 210-210, 1 31-37-73Page 44

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 | | | Logic based on Flight Legs: | | | R | | | | | | R | | | Every 'Y01.3' flight legs the DMU | | | R | | | searches in flight phase 6 for report | | | R | | | generation with stable frame criteria | | | R | | | where the best aircraft quality number | | | R | | | QE is calculated. The report with the | | | R | | | best quality number QE is stored in the | | | R | | | report buffer and the report which is | | | R | | | stored according to logic 4000 is then | | | R | | | deleted. | | | R | | | | | | R | |5 | The default programming shall be | C | Legs | R | | | 'Flight Legs' | | | R |----|------|-----------------------------------------|------|---------|
R  |  |  | Parameter for stable frame criteria  |  |  | 
R  |  |5.1  | 'P01' stable period  | C  | T22/T23/| 
R  |  |  | (5 subperiods = 100 sec)  |  | T23A  | 
R  |  |  | Stable frame basic condition in order  |  |  | 
R  |  |  | to avoid report triggering in flight  |  |  | 
R  |  |  | phases where parameters are of no use.  |  |  | 
R  |  |5.2  | HPTL1 < HPT < HPTL2  |  |  | 
R  |  |  | HPT = 7C.1.306.01 Engine 1  |  |  | 
　
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