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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