R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page B92 1 1 Aug 01/05 1 1 1CES 1
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|Report| Description of Report Item | CFM | CFM | CFM | SPARE | Unit |
|Item | |56-5-A1|56-5-A3|56-5-B4| | |
| | |-------|-------|-------|-------|------|
| 7.2 | 'X1.2' rpm tolerance band for |+/-1.5 |+/-1.5 |+/-1.5 | | % | | * | take off | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 7.3 | 'T1.2' stable observing time | 20 | 20 | 20 | |second| | * | for take off (max. 20 seconds)| | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | * Remark: Only for Advanced EVMU available | +-----------------------------------------------------------------------------+
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page B93 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | SPARE | Unit | |Item | |56-5-B1|56-5-B2|56-5-B3| | | | | |-------|-------|-------|-------|------| | | |DMU/ID |DMU/ID |DMU/ID | | | | | | CFM #5| CFM #6| CFM #7| | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.1 |'Y02.1' flight hours | 1 | 1 | 1 | | hours| |------|-------------------------------|-------|-------|-------|-------|------| | 5.2 |'Y02.2' flight legs | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3 | 'P02' stable periods | 5 | 5 | 5 | | | | | ( 1 period = 20 seconds) | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4.1| HPTL1 valve position lower | 70 | 70 | 70 | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4.2| HPTL2 valve position upper | 105 | 105 | 105 | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5 | IALT stable frame variation | 150 | 150 | 150 | | ft | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5.1| Weighting Factor Wa of IALT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.6 | GS stable frame variation | 6 | 6 | 6 | | kts | |------|-------------------------------|-------|-------|-------|-------|------| | 5.6.1| Weighting Factor Wa of GS | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7 | ROLL ANGLE stable frame | 0.8 | 0.8 | 0.8 | | deg | | | variation | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7.1| Weighting Factor Wa of ROLL | 1 | 1 | 1 | | | | | ANGLE | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.8 | TAT stable frame variation | 1.1 | 1.1 | 1.1 | | deg C| |------|-------------------------------|-------|-------|-------|-------|------| | 5.8.1| Weighting Factor Wa of TAT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.9 | N2 stable frame variation | 0.9 | 0.9 | 0.9 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 5.9.1| Weighting Factor Wa of N2 | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.10 | EGT stable frame variation | 18.0 | 18.0 | 18.0 | | deg C| |------|-------------------------------|-------|-------|-------|-------|------| |5.10.1| Weighting Factor Wa of EGT | 1 | 1 | 1 | | |
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