A320飞机维护手册 AMM 指示/记录系统 4(111)

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 : 001-049, 051-099, 101-149, 151-158, 1 31-37-21Page 11 1201-209, 211-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| |--------------|------------------------------------------------------| | ECYC | Engine Cycle | | 99999 | (00000 to 99999) | | | DMU Engine 1 | | | Engine 2 | | | | | | Each time when flight phase 5 (climb) is reached, | | | the counter is incremented by one. The ECYC is set | | | to zero if a new ESN is recognized by the DMU. It | | | is possible to set the ECYC via the MCDU, if the | | | DMU is changed on the A/C. | |--------------|------------------------------------------------------| | AP | Auto Pilot Status | | 99 | (00 to G8) | | | FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 | |--------------|------------------------------------------------------| | Y1 | Y1 Second Pre event intervals | | 99 | (0 to 99) | |--------------|------------------------------------------------------| | NL | Number of data lines without lines EC and EE | | 999 | (12 to 120) | | | DMU internal parameter | |--------------|------------------------------------------------------| | REASON | Reason for Report Trigger | | XXXXXXXXXX | Up to 30 characters | | XXXXXXXXXX | DUCT OVHT F/D CODE: 4110 | | XXXXXXXXXX | DUCT OVHT FWD CODE: 4120 | | | DUCT OVHT AFT CODE: 4130 | | | 4 TIMES DUCT OVHT F/D CODE: 4140 | | | 4 TIMES DUCT OVHT FWD CODE: 4150 | | | 4 TIMES DUCT OVHT AFT CODE: 4160 | | | 4 TIMES COMPR OUTLET OVHT LH CODE: 4210 | | | 4 TIMES COMPR OUTLET OVHT RH CODE: 4220 | | | PACK OUTLET OVHT LH CODE: 4230 | | | PACK OUTLET OVHT RH CODE: 4240 | | | EXCESSIVE CABIN ALTITUDE CODE: 4310 | | | CABIN ALTITUDE CODE: 5100 | | | CABIN DIFFERENT PRESSURE CODE: 5200 | |--------------|------------------------------------------------------| | N1 | Selected N1 Actual | | 9999 | (0 to 120.0 %rpm) | | | Remark: Leading Parameter | |--------------|------------------------------------------------------| | N2 | Selected N2 Actual |

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-21Page 12 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | 9999 | (0 to 120.0 %rpm) | | | Eng 1 param. 7C.1.344.01 | | | Eng 2 param. 7C.2.344.10 | |--------------|------------------------------------------------------| | PF | Pack Flow | | 999 | (0 to 1.00 kg/sec) | | | param. EEC 8E.1.126.11 LH | | | param. 8E.2.126.00 RH | | | Remark: Leading Parameter | |--------------|------------------------------------------------------| | COT | Pack Compressor Outlet Temperature | | X99 | (-50 to 300 Degrees C) | | | param. PC 8E.1.123.11 LH | | | param. 8E.2.123.00 RH | |--------------|------------------------------------------------------| | RI | Pack Ram Air Inlet Position | | 999 | (0 to 100 %) | | | param. PC 8E.1.130.11 LH | | | param. 8E.2.130.00 RH | |--------------|------------------------------------------------------| | RO | Ram Air Outlet Door Position | | 999 | (0 to 100 %) | | | param. 8E.1.124.11 LH | | | param. 8E.2.124.00 RH | |--------------|------------------------------------------------------| | PBV | Pack Bypass Valve Position | | 999 | (0 to 100 %) | | | param. PC 8E.1.112.11 LH | | | param. 8E.2.112.00 RH | | | Remark: Leading Parameter | |--------------|------------------------------------------------------| | FCV | Flow Control Valve Status | | 1 | 1 = closed | | | 0 = not closed | | | PC 8E.1.062.11.11 LH | | | 8E.2.062.00.11 RH | |--------------|------------------------------------------------------| | P3 | Selected PS3 (Burner Pressure) | | 9999 | (0.0 to 550.0 psia) | | | Eng.1 param. 7C.1.264.01 | | | Eng.2 param. 7C.2.264.10 | |--------------|------------------------------------------------------| | T3 | Selected T3 | | X999 | Format: Nagative values are indicated by 'N' in the|

R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-37-21Page 13 1 1 Aug 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | first position. Otherwise the first position is | | | used for the value. | |--------------|------------------------------------------------------| | TW | Pack Water Extr. Temperature | | X99 | (-10 to 100 Degrees C) | | | param. PC 8E.1.111.11 LH | | | param. 8E.2.111.00 RH | |--------------|------------------------------------------------------| | TP | Pack Outlet Temperature | | X99 | (-60 to 100 Degrees C) | | | param. PC 8E.1.121.11 LH | | | param. 8E.2.121.00 RH | |--------------|------------------------------------------------------| | TPO | Precooler Engine Outlet Temperature | | X99 | (-60 to 400 Degrees C) | | | PC 8E.1.141.11 LH | | | 8E.2.141.00 RH | |--------------|------------------------------------------------------| | PD | Precooler Engine Outlet Pressure | | 99 | (0 to 50 psi) | | | Eng.1 BMC 6F.1.143.01 | | | 6F.2.143.10 | | | Eng.2 6F.1.142.01 | | | 6F.2.142.10 | |--------------|------------------------------------------------------| | ALT | Altitude (Standard Altitude 1013 mbar) | | X9999 | (-1000 to 50000) | | | Format: Negative values are indicated with 'N' in | | | the first position. Otherwise the first position is| | | used for the value. | | | -2000 to 50000ft | | | param. ADIRU 06.1.203.01 | | | param. 06.2.203.10 | |--------------|------------------------------------------------------| | PS | Primary or Secondary System Fault | | 1 | 1 = Inoperational | | | 2 = Operational | | | Main zone control inop. | | | param. ZC. 5D.2.060.10.21 | | | This Bit status is printed in report lines with | | | line identifier 'S#'. | | | Zone secondary control inop. | | | param. 5D.2.060.10.22 | |--------------|------------------------------------------------------|
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 指示/记录系统 4(111)