The purpose, function, layout and locations of an ECAM Cockpit. Say no to plagiarism. Get a tailor-made essay on "Why Violent Video Games Shouldn't Be Banned"? Get an Original Essay The pilot's job on all aircraft includes continuous monitoring of flight instruments. It also includes checking the aircraft for damage and hazards for proper operation of the engine and airframe systems. For commercial aircraft, this can mean monitoring numerous indicators such as temperature and pressure in addition to maneuvering the aircraft. The electronic centralized aircraft monitoring system (ECAM) is designed to assist the pilot in this task. The basic concept behind ECAM is to automatically perform monitoring tasks for the pilot. When a problem is detected or an error occurs. The main display unit, together with an audible and visual display, alerts the pilot. You are then shown the corrective actions needed to take to correct the error. By automatically monitoring the system, the pilot is free to fly the aircraft until a problem occurs and is detected by the ECAM unit. ECAM Unit Arrangement Initial ECAM systems monitored airframe systems only, and engine parameters were displayed on traditional full-time cockpit gauges. Newer models of ECAM systems incorporate displays of engine parameters and airframe systems. An ECAM system has two monitors. These can be LCD or CRT. The left or upper monitor, depending on the aircraft panel layout, displays system status information and any alerts associated with corrective actions in a checklist format. The right or bottom monitor displays system information in pictorial form, as a diagram of the system referenced on the primary monitor. ECAM monitors are typically powered by separate signal generators where the aircraft's data inputs are fed into two flight warning computers. The analog inputs are first sent through an analog system data converter and then into the alarm computers. Alarm computers process the information and forward it to signal generators to illuminate the monitors. There are four basic modes of an ECAM system: flight mode, warning mode, fault mode and manual mode. For a normal flight the flight phase is used. The flight phases of a normal airplane are: pre-flight, takeoff, climb, cruise, descent, approach and post-landing. Warning and fault information will be displayed automatically depending on the situation. When warning information is displayed on the primary monitor, the secondary monitor will automatically display the system diagram with numerical values. The same applies to the fault-related mode, which takes control over all other modes regardless of which mode is selected at the time of the fault. Color coding used on the display unit to draw attention to topics in order of importance. The display modes are selected by startup. Signal generators are also tested. A maintenance panel allows you to test ads and further tests on demand. BITE stands for integrated test equipment. It is standard for monitoring systems to monitor themselves and the aircraft's systems. All system inputs to the flight warning computers can also be tested for continuity from this panel, as can the system data analog converter inputs and outputs. Any individual system faults will be listed normally on the display.