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A320 training manual download. A320 ATA 32 L3 TECHNICAL TRAINING MANUAL
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It will not be updated. All rights reserved. The inputs received by the FWC are used to elaborate red warnings. Various items of information for systems like engines, fuel, navigation and which do not agree with a warning, are directly sent to the DMCs. They send a320 training manual download to the Display Units DUs. Dkwnload DUs compute and display the images on each unit.
DMC 3 can drive a320 training manual download of the six DUs. Each FWC generates all warning and trainig messages, supplies the attention getters, computes the flight phase and provides aural warnings.
The EWD is dedicated to the presentation of information. On the lower area are displayed: 4 Memos, failure messages and actions to be performed. During TakeOff TO and landing, most a320 training manual download the warnings are inhibited.
Immediate crew awareness is required, but not immediate corrective action. The crew must decide when to take the corrective action. These warnings are associated with: The alerts are classified in three levels. They depend on the importance and urgency of the corrective actions required. The level 2 system failure has no direct consequence on flight safety. Corrective or palliative action must be taken by the crew immediately.
The attention getters lights and sounds are not activated by a level 1 alert. STATUS Some defects which do not trigger warnings or cautions, but which require further maintenance actions, will be indicated to the crew by means of a status indication, pulsing after engine shutdown.
It is necessary to call the status page manually to see the title of the affected system. There are 3 separate types of warnings or cautions: A secondary failure is a loss of an item of equipment or system resulting from a primary failure. Example: Loss of a pair of spoilers after a hydraulic system failure. Example: Green hydraulic system failure may lead to the loss of a pair of spoilers.
In A320 training manual download Centralized Aircraft Monitoring ECAM normal display, when a value mabual from its normal range, the corresponding system page is displayed automatically in order to attract crew attention well before reaching the warning or caution level.
The affected parameter and the system page title pulse. In this case the crew may revert to manual pressure control and prevent warning activation. As the corresponding system page cannot be displayed automatically on the System Display SDthe pilot has to fetch the information on the ECP: the associated key light flashes to indicate which system is concerned.
On the status and System Display SDthe hydraulic page is called automatically. This may be different to your aircraft configuration.
Then, actions indicated on the EWD have to be done. On the EWD, the messages associated to the corrective action have disappeared. On the left hand side of the EWD, the result смотрите подробнее the нажмите для продолжения appears indicating that it is a primary failure. On the right hand side, the secondary failures are displayed.
The system page trainihg to the first secondary failure is displayed. When you press CLR again, the title of the first secondary failure disappears. The system page associated with the next secondary a3320 is displayed. When you kanual CLR a third time, the title of the secondary failure disappears. On the status page, the cruise page related to the present flight phase comes back.
The warning has been cleared. Data warning computation and memo are achieved by the FWCs, warning announcements and data display are made through loudspeakers and Display Units DUs. The aural warnings and synthetic sownload are delivered by the FWCs to the узнать больше здесь loudspeakers.
The FWCs compute all warnings and cautions. The FWCs perform three main functions: 4 Data acquisition, 4 Flight phase computation, 4 Data warning computation corresponding to warning situations. The FWCs provide aural and visual information in order to: 4 Show, in real time, all the system failures and dangerous configurations with their level of seriousness, 4 Identify the systems or circuits affected by a failure, 4 Provide the appropriate corrective action.
The ECP is a control and display unit. It is possible to read this information manuaal the MCDU. They are Liquid Crystal Displays. In case both SDACs fail the amber cautions and most of the system displays are lost. All attention getters and loudspeakers remain operative. All other EWD messages, aural warnings and a320 training manual download getters are lost.
This enables manual source reconfiguration for attitude and heading data. On the EWD, the failed component is also displayed.
The switching is automatic. The crew has to carefully monitor the aircraft systems through the overhead panel or ECAM system pages. Most of the amber a320 training manual download are lost. The crew has to a320 training manual download monitor the overhead panel. The DMCs process the data and generate the images to be displayed.
The FWCs then supply: 4 the DMCs for the display of alert messages, 4 the attention getters, 4 the loudspeakers with aural alerts and synthetic voice messages. As a further means of getting the attention, there is a loudspeaker on each side of the cockpit for aural alerts and synthetic voice messages. Various items of information for systems like engines, fuel, navigation and which are not related to warning, are directly sent to the DMCs.
The inputs received by the SDACs are used to elaborate amber warnings. These signals will then be sent to the FWC to generate warnings. These computers are a320 training manual download heart of the ECAM system.
Each FWC generates all warning messages to display and supplies the attention getters. It also computes the flight phases and supplies aural warnings. It is divided into two areas: the upper area and the lower area. The lower area is used for: 4 warning and caution messages, 4 memo messages. ICE appears on the right a20 area. During TO and landing, most of the warnings are inhibited to avoid distraction of the crew.
For example, at TO, when the second engine is set to TO power and until the aircraft has reached 1. It flashes on the lower memo area to signal to the pilot that a parameter drifts from its normal value. Overflow arrow: only concerns the warning messages and indicates that the messages exceed the capacity of the display on the left memo area.
In this case, the heading titles of the a320 training manual download messages are displayed on the dwonload memo area. Data warning computation and memo information are achieved by the FWCs. Warning announcement and data display is made through loudspeakers and Display Units DUs. The FWCs give aural and visual information in order to: 4 know, in real time, all the system failures and dangerous configurations with their level of seriousness, 4 identify the systems or circuits affected by a failure, 4 take the appropriate corrective action.
They fulfil three main functions: 4 data acquisition, 4 data concentration, 4 data digitalization. A320 training manual download SDACs acquire, from the aircraft systems, the malfunction and failure data corresponding to caution situations and send ni reaktor 6 free download to the FWCs for generation of the corresponding alert and procedure messages.
They are also used as data concentrators a320 training manual download other systems example: Flight Data Interface Unit. All recorder for windows 10 free signals discrete, analogue, digital entering into the A320 training manual download majual concentrated and converted into a320 training manual download format.
They fulfil three main functions: 4 a320 training manual download acquisition, 4 data warning computation corresponding to warning situations, 4 flight phase computation. The A320 training manual download also manuxl aural alerts as well as synthetic voices for radio height, automatic call out and other announcements.
These are: 4 system and warning titles, 4 procedures associated with the warnings, 4 status and a3200. They also have BITE for maintenance operation. It receives the DMC data in order to bring its keys lights out. It is also linked to the DUs for the brightness control. They receive data from the aircraft systems, decode and process it so that it can be displayed on the EFIS displays.
The feedback information is: 4 data acquisition, 4 acknowledgment signals, 4 PFD processing channel, 4 DU a320 training manual download information, 4 ND processing channel, 4 critical parameter feedback signals pitch and roll angles, altitude, heading, aircraft position.
They also acquire some discretes for example: reconfiguration of the DUs. This configuration is called "ECAM mono display". All the ECAM images are lost momentarily. ECAM in mono display. Loss of text messages on EWD display.
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