A320飞机维护手册 AMM 指示/记录系统 5(101)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page B76 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | SPARE | Unit | |Item | |56-5-A1|56-5-A3|56-5-B4| | | | | |-------|-------|-------|-------|------| |------|-------------------------------|-------|-------|-------|-------|------| | 5.7 | N2 stable frame variation | 0.9 | 0.9 | 0.9 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7.1| Weighting Factor Wa of N2 | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.8 | EGT stable frame variation | 18.0 | 18.0 | 18.0 | | deg C| |------|-------------------------------|-------|-------|-------|-------|------| | 5.8.1| Weighting Factor Wa of EGT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.9 | VACC stable frame variation | 0.10 | 0.10 | 0.10 | | g | |------|-------------------------------|-------|-------|-------|-------|------| | 5.9.1| Weighting Factor Wa of VACC | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.10 | MN stable frame variation | 0.01 | 0.01 | 0.01 | | Mach | |------|-------------------------------|-------|-------|-------|-------|------| |5.10.1| Weighting Factor Wa of MN | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.11 | N1 stable frame variation | 1.6 | 1.6 | 1.6 | | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.11.1| Weighting Factor Wa of N1 | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.12 | PT2 stable frame variation | 0.10 | 0.10 | 0.10 | | psia | |------|-------------------------------|-------|-------|-------|-------|------| |5.12.1| Weighting Factor Wa of PT2 | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.13 | FF stable frame variation | 100 | 100 | 100 | | kg/h | |------|-------------------------------|-------|-------|-------|-------|------| |5.13.1| Weighting Factor Wa of FF | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.14 | HPT stable frame variation | 10.0 | 10.0 | 10.0 | | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.14.1| Weighting Factor Wa of HPT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.15 | LPT stable frame variation | 10.0 | 10.0 | 10.0 | | % | |------|-------------------------------|-------|-------|-------|-------|------| |5.15.1| Weighting Factor Wa of LPT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 6.2 | Number 'X01' for consecutive | 5 | 5 | 5 | | | | | reports | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 9.1 | 'NIT.1' stable N1 value for | 62 | 62 | 62 | | %rpm | | * | descent | | | | | | |------|-------------------------------|-------|-------|-------|-------|------|

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-73Page B77 1 1 Aug 01/05 1 1 1CES 1 +-----------------------------------------------------------------------------+ |Report| Description of Report Item | CFM | CFM | CFM | SPARE | Unit | |Item | |56-5-A1|56-5-A3|56-5-B4| | | | | |-------|-------|-------|-------|------| | 9.2 | 'X1.1' tolerance band for |+/-1.5 |+/-1.5 |+/-1.5 | | % | | * | descent | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 9.3 | 'T1.1' stable observing time | 20 | 20 | 20 | |second| | * | for descent (max. 20 seconds) | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| |10.1 | 'N1T.1' stable N1 value for | 93 | 93 | 93 | | %rpm | | * | take off | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| |10.2 | 'X1.2' tolerance band for |+/-1.5 |+/-1.5 |+/-1.5 | | % | | * | take off | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| |10.3 | '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 B78 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| | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.1 |'Y01.1' flight hours | 0 | 0 | 0 | | hours| |------|-------------------------------|-------|-------|-------|-------|------| | 4.2 |'Y01.2' minutes after cruise | 10 | 10 | 10 | | min | | | entry | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 4.3 |'Y01.3' flight legs | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.1 |'P01' stable periods | 5 | 5 | 5 | | | | | (1 period = 20 seconds) | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.2.1| HPTL1 valve position lower | 70 | 70 | 70 | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.2.2| HPTL2 valve position upper | 105 | 105 | 105 | | % | | | limit | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3 | IALT stable frame variation | 150 | 150 | 150 | | ft | |------|-------------------------------|-------|-------|-------|-------|------| | 5.3.1| Weighting Factor Wa of IALT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4 | GS stable frame variation | 6 | 6 | 6 | | kts | |------|-------------------------------|-------|-------|-------|-------|------| | 5.4.1| Weighting Factor Wa of GS | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5 | ROLL ANGLE stabel frame | 4.0 | 4.0 | 4.0 | | deg | | | variation | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.5.1| Weighting Factor Wa of ROLL | 1 | 1 | 1 | | | | | ANGLE | | | | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.6 | TAT stable frame variation | 2.0 | 2.0 | 2.0 | | deg C| |------|-------------------------------|-------|-------|-------|-------|------| | 5.6.1| Weighting Factor Wa of TAT | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7 | N2 stable frame variation | 0.9 | 0.9 | 0.9 | | % | |------|-------------------------------|-------|-------|-------|-------|------| | 5.7.1| Weighting Factor Wa of N2 | 1 | 1 | 1 | | | |------|-------------------------------|-------|-------|-------|-------|------|
　
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