ATR42-600的驾驶舱是ATR系列的玻璃驾驶舱。 The Cockpit of the ATR42-600 is the Glass Cockpit evolution of the ATR family.
新的航空电子设备大大减少了飞行员的工作量，增强了态势感知和安全性。 The new avionics greatly reduce Pilots workload and enhance situational awareness and safety.
5个显示单元（DU）将有关飞机和系统状态的信息分类如下： 5 Display Units (DU) cluster the information about aircraft and systems status as follow ：
·两个主飞行显示器（PFD）将与飞行有关的数据分组，如姿态、速度、速度趋势、高度和自动飞行控制模式。 ·Two Primary Flight Displays (PFD) which group data related to the flight such as attitude, speed, speed trend, altitude and auto flight control modes.
两个多功能显示器（MFD）将与导航相关的数据与显示器（ND）进行分组，显示器定位A/C位置和飞行管理系统（FMS）中输入的飞行计划的进程。 Two Multi Function Displays (MFD) which group data related to Navigation with Display (ND) which locates the A/C position and progress along the flight plan entered in the Flight Management ·System (FMS).
MFD还可以承载显示系统状态的系统显示器（SD） The MFD can host also the System Display (SD) which displays Systems Status.
中央发动机和警告显示器（EWD）提供信息和警报信息： A central Engine and Warning Display (EWD) gives information and alerting messages:
·永久数据窗口重新组合有关发动机状态、燃油和控制表面（饰件和襟翼设置）的基本信息， ·The permanent data window regroups essential information on Engines status, fuel and control surfaces (Trims and Flap settings),
·小心和警告窗口显示故障标题， ·The Caution and Warning window displays malfunction titles,
·EWD程序窗口根据飞行阶段显示适当的程序，或在可能发生故障后显示以下故障程序。 ·The EWD procedure Window, displays the appropriate procedure according to the flight phase or the following failure procedure to follow after a possible malfunction.
·集成电子备用仪表（IESI）可作为显示器故障时的备用参考。 ·An Integrated Electronic Stand-by Instrument (IESI) serves as a backup reference in case of Displays failure.
驾驶ATR42-600的最低机组人员由两名飞行员组成。为了便于飞行员安装，这两个座位是收起他们横向滑动对飞行甲板侧壁。 The minimum crew to fly an ATR42-600 is composed of two pilots. To facilitate the pilots installation, the two seats are stowed away by sliding them laterally against the Flight Deck sidewalls.
当飞行员倾斜座椅就位时，可以水平和垂直调节。 When in position the Pilots reclining seats can be adjusted horizontally and vertically.
可视座椅位置计可用于座椅调节。飞行员将彩球对准以确保正确的坐姿。 A visual seat position gage can be used for Seat adjustment. The Pilot aligns the colored balls to ensure proper sitting position.
方向舵踏板可以前后调节，以获得最佳的舒适性。 The Rudder Pedals can be adjusted forward and backward for best comfort.
位于驾驶舱门前面板上的第三个可折叠座椅用作观察者座椅。 A third foldable seat located on the front panel of the Cockpit Door is used as an observer seat.
对于系统状态监控，ATR采用“黑暗驾驶舱原理”，即在系统正常运行时熄灭所有面板灯。 For system status monitoring, ATR uses the "dark cockpit philosophy" which consist on extinguishing all panel lights when systems are operating normally.
银色边框轮廓区分按钮（P/B）开关。 A silver border outline differentiates the pushbutton (P/B) switches.
一些按钮有一个额外的荧光琥珀色轮廓，以便在能见度低的情况下（例如驾驶舱内有烟雾）进行定位。 Some pushbuttons have an additional fluorescent amber outline to facilitate their localization in case of low visibility (smoke in the Cockpit for example).
按钮颜色编码为： The pushbutton color coding is:
在正常工作条件下黑暗或不发光。指示正常工作状态的灯的使用限制在最低限度， Dark or not illuminated in normal operating conditions. The use of lights to indicate a normal operating status is limited to a minimum,
蓝色表示手动和临时系统选择。例如：“ON”与外部电源或除冰系统相关，“IGN”与手动点火相关，“HIGH”与气流客舱通风选择相关，“MAN”与客舱温度选择相关， Blue for manual and temporary system selection. For example: "ON" associated with External Power or De-Icing Systems, "IGN" with manual ignition and "HIGH" in air flow cabin ventilation selection and "MAN" with cabin temperature selection,
系统自动启动时为绿色。例如：“运行”与燃油泵或“可用”与外部电源可用性。 Green when a system starts automatically. For example: "RUN" with fuel pumps or "AVAIL" with External Power availability.
系统设置为关闭时为白色。 White when a system is set to Off.
琥珀色表示系统故障指示或按钮与系统状态不匹配。 Amber for system malfunction indication or pushbutton mismatch with system status.
它通常与主警告和单个蜂鸣音有关。例如：“FAULT”与DC GEN1相关，“OVHT”与座舱温度选择相关，或“LEAK”与发动机引气相关。 It is generally associated with the Master Caution and single chime. For example : "FAULT" associated with the DC GEN1, "OVHT" with cabin temperature selection or "LEAK" with engine bleed.
信号灯没有银色衬里，其颜色代表系统状态： The annunciator lights have no silver lining and their color is representative of systems status:
·正常工作条件下不亮， ·not illuminated for normal operating condition,
·蓝色表示手动和临时系统选择， ·blue for manual and temporary system selection,
·系统自动启动时为绿色， ·green when the system is automatically activated,
·系统设置为关闭时为白色。 ·white when the system is set to OFF.
·琥珀色警告，故障不需要机组立即采取行动， ·amber for Caution, the malfunction does not require an immediate crew action,
·红色表示警告，这里的情况需要船员立即采取行动。 ·red for warning, here the situation requires an immediate crew action.
在显示单元上，系统状态也使用相同的颜色编码显示： On display units, systems status are also shown using the same color coding:
·绿色表示正常运行， ·Green for normal operation,
·蓝色表示手动和临时系统选择，白色表示“关闭”系统设置。 ·Blue for manual and temporary system selection, white for "OFF" system setting.
·琥珀色表示警告， ·amber for Caution,
·红色表示警告。 ·and red for warning.