The purpose, function, layout and locations of an ECAM cockpit.Say no to plagiarism. Get a tailor-made essay on “Why Violent Video Games Should Not Be Banned”? Get an Original Essay The pilot's job on all aircraft includes continuous monitoring of flight instruments. This also includes checking the aircraft for damage and hazards and ensuring the engine and airframe systems are functioning properly. For commercial aircraft, this may involve monitoring numerous indicators such as temperature and pressure, in addition to maneuvering the aircraft. The electronic centralized aircraft monitoring (ECAM) system 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 a failure occurs. The main display unit, accompanied by an audible and visual display, alerts the pilot. The corrective measures to be taken are then displayed to correct the fault. 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 Layout 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 and airframe system parameters. 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 warnings associated with corrective actions in a checklist format. The right or lower monitor displays related system information in image form, such as a diagram of the system being referenced on the main monitor. ECAM monitors are typically powered by separate signal generators where data inputs from the aircraft are placed into two flight warning computers. . The analog inputs are first transmitted through a system data analog converter and then to the warning computers. Warning computers process the information and transmit it to signal generators to illuminate the monitors. There are four basic modes of an ECAM system: flight mode, advisory mode, fault mode, and manual. For normal flight, the flight phase is used. The phases of a normal aircraft in flight phase are pre-flight, takeoff, climb, cruise, descent, approach and after landing. Advice and troubleshooting information will appear automatically depending on the situation. When advisory information is displayed on the primary monitor, the secondary monitor will automatically display the system diagram with numerical values. The same goes for the fault-related mode, which takes control of all other modes, regardless of the mode selected at the time of the fault. Color coding used on the display unit to draw attention to topics in order of importance. Display modes are selected via the ECAM control panel shown in the unit layout. Flight failure notification system. Keep in mind: this is just a sample. Get a personalized document now from our expert writers. Get a Personalized Test Self-Test of ECAM Theft Warning Computers After Getting Started. Signal generators are also tested. A maintenance panel allows for ad testing and other tests on request. BITE stands for equipment of..