• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

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

 |  | | 38 | 105  |  | |
 |  | |  |  | | 


R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 31-37-73Page A58

1401-499, 1Aug 01/05 1 1 1CES 1 +----------------------------------------------------------------------+ |Code|Item | |Progr.|Standard | | No.|No. | Description of Function Item |MCDU |Value or | | | | |GSE |Table TXY| |----|------|-----------------------------------------|------|---------| | |4.2.3 | OIPL2 limit in psi | C | T22/T23/| | | | | | T23A | |----|------|-----------------------------------------|------|---------| | |5 | Generation stops when exceedance param. | | | | | | are again within their limits or 10 sets| | | | | | of post event data are generated. | | | |----|------|-----------------------------------------|------|---------| |8100|8.1 | ACARS MU uplink request with IMI 'REQ07'| | | | | | The report <07> is immediately generated| | | | | | and transmitted to the ACARS MU. | | | |----------------------------------------------------------------------| |  A  =  Programmable by Airbus Industrie | |  C  =  Programmable by Customer | +----------------------------------------------------------------------+


 **ON A/C ALL
 G. Engine Divergence Report <09> (Ref. Fig. 008) The Engine Divergence Report shall be a time series collection of engine related information prior to and after the detection of an engine divergence condition. The engine divergence logic is intended to detect rapid degradation in engine performance over the course of a few hours. The report is generated when one of the logic conditions 1000 to 4180 (for deiails see the Engine Divergence Report logic) is present.
 1EFF : ALL 1 31-37-73Page A59 1 1 May 01/05R 1 1 1CES 1


 Engine Divergence Report <09>
 (Engine Type CFMU with EVMU)
 Figure 008 
R 1EFF :  ALL  1  31-37-73 Page A60 
1  1  May 01/05
 1  1
 1CES  1

 


R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,

 (1) Engine Divergence Report Data Field Description <09>(Engine Type CFMI with Advanced EVMU)
 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | ESN | Engine Serial Number | | 999999 | (000000 to 999999) | | | Eng 1 param. 7C.1.046.01 digit 3, 2, 1 | | | 7C.1.047.01 digit 6, 5, 4 | | | Eng 2 param. 7C.2.046.01 digit 3, 2, 1 | | | 7C.2.047.01 digit 6, 5, 4 | |--------------|------------------------------------------------------| | EHRS | Engine Flight Hours | | 99999 | (00000 to 99999 hours) | | | DMU Engine 1 and Engine 2 | |--------------|------------------------------------------------------| | ERT | Engine Running Time | | 99999 | (00000 to 65536 hours) | | | Eng 1 param. 7C.1.050.01 | | | Eng 2 param. 7C.2.050.10 | |--------------|------------------------------------------------------| | ECYC | Engine Cycle | | 99999 | (00000 to 99999) | |--------------|------------------------------------------------------| | AP | Auto Pilot Status | | 99 | (00 to G8) | | | FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 | | | | | | XX Auto Pilot Modes: | | | || | | | ||__Lateral Modes: 0 = NO MODE | | | | 1 = HEADING | | | | 2 = TRACK | | | | 3 = NAV | | | | 4 = LOC CAPTURE | | | | 5 = LOC TRACK | | | | 6 = LAND TRACK | | | | 7 = RUNWAY | | | | 8 = ROLL GO AROUND | | | | | | | |__Longitudinal Modes: 0 = NO MODE | | | 1 = PITCH G/A | | | 2 = PITCH T/O |
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 31-37-73Page A61 1201-209, 1May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | 3 = G/S TRACK | | | 4 = G/S CAPTURE | | | 5 = V/S | | | 6 = FPA | | | 7 = ALT | | | 8 = ALT ACQ | | | 9 = OPEN CLB | | | A = OPEN DES | | | B = IM CLB | | | C = IM DES | | | D = CLB | | | E = DES | | | F = FINAL DES | | | G = EXPEDITE | | | | | | AP1 | AP2 | | | Report Line EC: | Report Line EE: |Difinition: | | | -------------------|-------------------|------------ | | | / | / |No Mode Act. | | | -------------------|-------------------|------------ | | | 01.1.275.00.11 = 1 | 01.2.275.00.11 = 1|RUNWAY Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.12 = 1 | 01.2.275.00.12 = 1|NAV Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.13 = 1 | 01.2.275.00.13 = 1|LOC CAPTURE | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.14 = 1 | 01.2.275.00.14 = 1|LOC TRACK | | | | |Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.15 = 1 | 01.2.275.00.15 = 1|Roll GO | | | | |AROUND Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.16 = 1 | 01.2.275.00.16 = 1|HEADING Mode | | | -------------------|-------------------|------------ | | | 01.1.275.00.17 = 1 | 01.2.275.00.17 = 1|TRACK Mode | | | -------------------|-------------------|------------ | | | 01.1.274.00.15 = 1 | 01.2.274.00.15 = 1|PITCH TO Mode| | | -------------------|-------------------|------------ | | | 01.1.274.00.16 = 1 | 01.2.274.00.16 = 1|PITCH GA Mode| | | -------------------|-------------------|------------ | | | 01.1.274.00.17 = 1 | 01.2.274.00.17 = 1|V/S Mode | | | -------------------|-------------------|------------ | | | 01.1.274.00.18 = 1 | 01.2.274.00.18 = 1|FPA Mode |
 
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 5(51)