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A320飞机维护手册 AMM 指示/记录系统 5(110)

时间:2011-03-25 12:19来源:蓝天飞行翻译 作者:admin 点击:
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R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page C3 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | SPARE | SPARE | Unit | |Item | |56-5-B8|56-5-B9| | | | | | |-------|-------|-------|-------|------| |------|-------------------------------|-------|-------|-------|-------|------| | 5.11 | VACC stable frame variation | 0.03 | 0.03 | | | g | |------|-------------------------------|-------|-------|-------|-------|------| |5.11.1| Weighting Factor Wa of VACC | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.12 | MN stable frame variation | 0.008 | 0.008 | | |Mach | |------|-------------------------------|-------|-------|-------|-------|------| |5.12.1| Weighting Factor Wa of MN | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.13 | N1 stable frame variation | 1.6 | 1.6 | | | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.13.1| Weighting Factor Wa of N1 | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.14 | PT2 stable frame variation | 0.05 | 0.05 | | | psia | |------|-------------------------------|-------|-------|-------|-------|------| |5.14.1| Weighting Factor Wa of PT2 | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.15 | FF stable frame variation | 100 100 | | | kg/h | |------|-------------------------------|-------|-------|-------|-------|------| |5.15.1| Weighting Factor Wa of FF | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.16 | HPT stable frame variation | 10.0 | 10.0 | | | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.16.1| Weighting Factor Wa of HPT | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.17 | LPT stable frame variation | 10.0 | 10.0 | | | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.17.1| Weighting Factor Wa of LPT | 100 | 100 | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 6.1 | 'N1T.1' stable N1 value for | 62 | 62 | | | % | | * | descent | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 6.2 | 'X1.1' tolerance band for |+/-1.5 |+/-1.5 | | | % | | * | descent | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 6.3 | 'T1.1' stable observing time | 20 | 20 | | |second| | * | for descent (max. 20 seconds) | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 7.1 | 'N1T.2' stable N1 value for | 93 | 93 | | | %rpm | | * | take off | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 7.2 | 'X1.2' rpm tolerance band for |+/-1.5 |+/-1.5 | | | % | | * | take off | | | | | |


R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page C4 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | SPARE | SPARE | Unit | |Item | |56-5-B8|56-5-B9| | | | | | |-------|-------|-------|-------|------| |------|-------------------------------|-------|-------|-------|-------|------| | 7.3 | 'T1.2' stable observing time | 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 C5 1 1 Aug 01/05 1 1 1CES 1


 M. Report Limits for Engine T/O Report <04>
 (1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | SPARE | Unit | |Item | |56-5-A1|56-5-A3|56-5-B4| | | | | |-------|-------|-------|-------|------| | | |DMU/ID |DMU/ID |DMU/ID | | | | | | CFM #1| CFM #2| CFM #3| | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.3 | EGTL temperature limit cold | 100 | 100 | 100 | | deg C| | | engine start detection | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.4 | F04th Take OFF | 5 | 5 | 5 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.5 | Y04.1 seconds after PH 4 entry| 40 | 40 | 40 | | sec | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.1| Delta N1 | >10 | >10 | >10 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.2| Delta N1 | 8..10 | 8..10 | 8..10 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.3| Delta N1 | 6..8 | 6..8 | 6..8 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.4| Delta N1 | 4..6 | 4..6 | 4..6 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.5| Delta N1 | 2..4 | 2..4 | 2..4 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.6| Delta N1 | 0.2..2| 0.2..2| 0.2..2| | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.7.7| Delta N1 | <= 0.2| <= 0.2| <= 0.2| | % | |------|-------------------------------|-------|-------|-------|-------|------| | 4.8.1|Y04.3 seconds after PH 4 entry | 5 | 5 | 5 | | sec | | |calculation of N1 Summary Limit| | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.1 | Number 'X04' consecutive legs | 5 | 5 | 5 | | | +-----------------------------------------------------------------------------+
 
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