返回首页
当前位置: 主页 > 航空资料 > 机务资料 >

A320飞机维护手册 AMM 指示/记录系统 5(103)

时间:2011-03-25 12:19来源:蓝天飞行翻译 作者:admin 点击:
  


R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page B82 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | CFM | Unit | |Item | |56-5-A5|56-5-B6|56-5-B5|56-5-A4| | | | |-------|-------|-------|-------|------| | 5.8 | EGT stable frame variation | 18.0 | 18.0 | 18.0 | 18.0 | deg C| |------|-------------------------------|-------|-------|-------|-------|------| | 5.8.1| Weighting Factor Wa of EGT | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.9 | VACC stable frame variation | 0.10 | 0.10 | 0.10 | 0.10 | g | |------|-------------------------------|-------|-------|-------|-------|------| | 5.9.1| Weighting Factor Wa of VACC | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.10 | MN stable frame variation | 0.010 | 0.010 | 0.010 | 0.010 |Mach | |------|-------------------------------|-------|-------|-------|-------|------| |5.10.1| Weighting Factor Wa of MN | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.11 | N1 stable frame variation | 1.6 | 1.6 | 1.6 | 1.6 | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.11.1| Weighting Factor Wa of N1 | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.12 | PT2 stable frame variation | 0.10 | 0.10 | 0.10 | 0.10 | psia | |------|-------------------------------|-------|-------|-------|-------|------| |5.12.1| Weighting Factor Wa of PT2 | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.13 | FF stable frame variation | 100 | 100 | 100 | 100 | kg/h | |------|-------------------------------|-------|-------|-------|-------|------| |5.13.1| Weighting Factor Wa of FF | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.14 | HPT stable frame variation | 10 | 10 | 10 | 10 | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.14.1| Weighting Factor Wa of HPT | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.15 | LPT stable frame variation | 10.0 | 10.0 | 10.0 | 10.0 | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.15.1| Weighting Factor Wa of LPT | 1 | 1 | 1 | 1 | | |------|-------------------------------|-------|-------|-------|-------|------| | 6.2 | Number 'X01' for consecutive | 5 | 5 | 5 | 5 | | | | reports | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 9.1 | 'N1T.1' stable N1 value for | 62 | 62 | 62 | 62 | %rpm | | * | descent | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 9.2 | 'X1.1' tolerance band for |+/-1.5 |+/-1.5 |+/-1.5 |+/-1.5 | % | | * | descent | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 9.3 | 'T1.1' stable observing time | 20 | 20 | 20 | 20 |second| | * | for descent (max. 20 seconds) | | | | | |


R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page B83 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | CFM | Unit | |Item | |56-5-A5|56-5-B6|56-5-B5|56-5-A4| | | | |-------|-------|-------|-------|------| |------|-------------------------------|-------|-------|-------|-------|------| | 10.1 | 'N1T.1' stable N1 value for | 93 | 93 | 93 | 93 | %rpm | | * | take off | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 10.2 | 'X1.2' tolerance band for |+/-1.5 |+/-1.5 |+/-1.5 |+/-1.5 | % | | * | take off | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 10.3 | 'T1.2' stable observing time | 20 | 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 B84 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | SPARE | SPARE | SPARE | Unit | |Item | |56-5-B7| | | | | | | |-------|-------|-------|-------|------| | | |DMU/ID | | | | | | | | C5xxxx| | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.1 |'Y01.1' flight hours | 0 | | | | hour | |------|-------------------------------|-------|-------|-------|-------|------| | 4.2 |'Y01.2' minutes after cruise | 10 | | | | min | | | entry | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.3 |'Y01.1' flight legs | 1 | | | | hour | |------|-------------------------------|-------|-------|-------|-------|------| | 5.1 |'P01': stable periods | 5 | | | | | | | (1 period = 20 seconds) | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.2.1| HPTL1 valve position lower | 70 | | | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.2.2| HPTL2 valve position upper | 105 | | | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3 | IALT stable frame variation | 150 | | | | ft | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3.1| Weighting Factor Wa of IALT | 1 | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4 | GS stable frame variation | 6 | | | | kts | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4.1| Weighting Factor Wa of GS | 1 | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5 | ROLL ANGLE stabel frame | 4.0 | | | | deg | | | variation | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5.1| Weighting Factor Wa of ROLL | 1 | | | | | | | ANGLE | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.6 | TAT stable frame variation | 2.0 | | | | deg C| |------|-------------------------------|-------|-------|-------|-------|------| | 5.6.1| Weighting Factor Wa of TAT | 1 | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7 | N2 stable frame variation | 0.9 | | | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7.1| Weighting Factor Wa of N2 | 1 | | | | | |------|-------------------------------|-------|-------|-------|-------|------|
 
中国航空网 www.aero.cn
民航翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 指示/记录系统 5(103)
 

------分隔线----------------------------