
ECAM F/CTL page - FlyByWire Simulations
The blue and green hydraulic servo jack is unavailable. The green and blue hydraulic pressure is within normal operating range. The associated computer or actuator is failed. The corresponding systems are available. The pitch trim is in normal operations. The yellow and yellow hydraulic pressure is decreasing.
A32NX: F/CTL ALTN LAW (PROT LOST) : r/MicrosoftFlightSim - Reddit
2023年2月27日 · Alternate Law (no protection) will happen if any of the flight computers encounters an error or is shut down. You might be disabling/enabling something you shouldn't. The first thing that comes to mind is disabling the ADIRS. Alternate law is no big deal, you should never be flying in a way that activates the protections anyway.
On the A320 family program, TR reference 105-1 was issued in June 2007 (fig. 3). A similar TR reference 568-1 was issued for the QRH 2.38. These TR have been incorporated in the June 2008 revisions (REV 42) of the A320 family FCOM and QRH. On the A310/A300-600 and A330/340 programs the note had already been incorporated in their respective FCOM ...
F/CTL L/R Sidestick Fault - Fenix Sim
You receive this error and flight controls may be unresponsive. To resolve this fault, open the MCDU Menu and go to the Config menu. Select Controls Config and change to page #2. From there move your sidestick among all of the axis' until it is properly responding. You can adjust your nullzones settings until the side stick responds correctly.
A320系列 飞控常见排故经验总结A320系列机务在线 - 认真、负责 …
2015年8月30日 · 某a320飞机航前apu起动好后ecam出现警告信息:f/ctl flap sys 1 fault。 伴随故障信息:SFCC 1 21CV。 本机对调SFCC1和SFCC2后故障转移,复位SFCC2更换SFCC1 ,故障依旧。
F/CTL PITCH TRIM/MCDU/CG DISAGREE警告信息的说明
2024年5月16日 · 2019年8月29日A320飞机航前出港进入跑道后机组反馈按压起飞构型测试不通过,ECAM有信息F/CTL PITCH TRIM/MCDU/CG DISAGREE。 协调机组重新输入无燃油重量和无燃油重心,复位FAC电门后起飞构型测试正常,飞机正常出港。 F/CTL PITCH TRIM / MCDU / CG DISAGREE是一个构型警告信息,触发阶段02/03。 适用于单通道飞机并FWC安装版本在 H2-F6A 及以上。 根据空客的介绍,该信息大多数情况是操作人员输入数据错误导致的警告。 A.在02 …
A320系列 飞控常见排故经验总结 - 机务在线 - Powered by Discuz!
2017年2月9日 · 某A320飞机航前APU起动好后ECAM出现警告信息:F/CTL FLAP SYS 1 FAULT。 伴随故障信息:SFCC 1 21CV。 本机对调SFCC1和SFCC2后故障转移,复位SFCC2更换SFCC1 ,故障依旧。 暂时拔掉SFCC2控制跳开关7CV和8CV,自检测试正常,警告信息消失。 更换SFCC2 22CV后故障排除。 1、增升系统包括在每个机翼上的两个后缘襟翼和五个前缘缝翼(舵面的数字从翼根向翼尖编号)。 舵面的位置从控制手柄选择,手柄将指令信号通过指令 …
A320 ECAM FLT CTL PAGE - AviationHunt
The A320 ECAM F/CTL page with its parameters is described in the image above as follows: 1: Spoilers status (left) 2: Hydraulic system pressure indication; 3: Spoilers status (right) 4: FCDC Message; 5: Aileron position; 6: Servo control hydraulic pressure; 7: Servo control electrical status; 8: Aileron scale; 9: SEC computer operation
Version 1.1 Caution: "F/CTL slats fault" during startup engine …
2024年11月18日 · In verion 1.1 during startup engine number 2, on ECAM appears caution: "F/CTL slats fault" and then immediately disappears. Look at the photo at attachment. This thing happens every time after update to version 1.1. During startup engine number 1 there are no cautions. Is it bug? Or am I doing something wrong? Martin S.
空客F/CTL FLAP SYS FAULT排故隔离汇总A320系列机务在线 - 认真 …
2017年7月29日 · 机务在线a320系列热门机型维修经验讨论区空客f/ctl flap sys fault排故隔离汇总 设为首页 收藏本站 微信登录 帐号登录 立即注册