Technical documentation for the aircrafts. Creating and updating the manual, maintenance procedures, troubleshooting (AMM, TSM). Greetings of the day dear friends. I am in search of A(CFMA) AMM in PDF documents are normally available in ADOC. Airbus A Tsm. BOOK ID: byku1lDmnQdq [Pdf] Airbus A Tsm DOWNLOAD Book Free. May 9th, – Podle zÃ¡kona o evidenci.
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Size px x x x x There are two general divisions of monitored and non-monitored faults.
The use of this function stm also be requested by the TSM procedures. Consequently, if a difference is detected by a system it is considered as a fault and therefore generates a maintenance message in the test results. It will be used to confirm the presence of a fault or to eliminate any ambiguity.
Each chapter is sub-divided into sections which are identified by a tsmm digit number made up of three elements: This system organization in three types essentially remains transparent for the operator as the CFDIU manages any differences.
It should only be used if the printed PFR is not available as the information is less complete and the presentation is not so friendly. This type of system enables: Introduction The introduction provides the following information: Block Task Supporting Data are given to show the system layout and interconnections with other systems.
Examples of trouble shooting these faults are given in the following trouble shooting examples. These are managed at chapter level by: The deletion of one configuration does not change the three digit alphanumeric indicator of the remaining task s. For these systems, the flight condition is between takeoff and landing.
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This is achieved with the normal cockpit controls engagement levers, pushbutton switches by selecting the related control off then on or by action on the corresponding txm breaker.
They are always GO without any restriction. The layout is as follows: This does not necessarily mean that an effective failure is present. Nonetheless, their definitions make it possible to understand why certain menus are simplified.
airbus a320 TSM
Furthermore, after aircraft power up, it enables to check that all computers have correctly satisfied the related a3320 up tests. CXN01 corresponds to the first customer version.
These tests txm also be menu-guided tests. In order to be able to launch the proper maintenance actions, all faults: Class 1 maintenance messages are presented in the Post Flight Report at the end of the flight.
For some of these faults the cockpit effect does not automatically appear to the crew when it is activated e. In certain multiple fault cases, the test may only indicate the first fault encountered. The contents of these is as follows: The faults detected during flight and which remain present on ts, are in the PFR and not in the ground report. From these pages the troubleshooter is directed to the procedure in P.
The user who wants to use these messages must do so carefully as the information involved is non-correlated and non-priority information. It is a user-friendly monitoring device providing direct access to system menus which detect a fault for example, flag displayed on the PFD. This architecture provides for a better targeted diagnosis by correlating data between system computers as well as reducing bus links with the CFDIU.
However, only the temporary revisions deleted by the highlights of a normal revision must be txm. It is requested that this form be used for any questions concerning the TSM. This function enables a quick access to the class 3 messages of a given system.
This section may be consulted to check the interrogated computer standard. In general, these data are read in the case of events which do not result from effective part failure, already covered by the replacement of the failed part.
Airbus A TSM( Trouble shooting manual )
ts, To achieve its purpose, the CFDS has several major functions which supply: Trouble Shooting Tips Tips for using the various TSM page blocks and a302 additional information are given in the following paragraphs: TO Power up to 80 kts In most of the cases, computers may be recovered after an abnormal behaviour or a detected fault, w320 by a software reset reset of microprocessor or by interrupting the power supply of its processing parts for a short time.
Please copy and paste this embed script to where you want to embed Embed Script. This means that one fault symptom is effective for at least one aircraft in the fleet.
Case related to Type 2 systems: For the TSM this is always The breakdown of each procedure is as follows: We are a non-profit group that run this website to share documents. Block The primary fault only is given in the TSM to avoid confusion with too many associated faults.
The first four columns contain the fault message, ATA reference, source and class. In the TSM with each maintenance message, the test or the procedure will be indicated making it possible to recheck the component on the ground – To better manage the effect of the test on the system and its ground handling the test function may be divided into two groups: The purpose is to be able to test on the ground, the maximum number of components, i.
When a trouble shooting operation is completely different according to equipment design example: Types of systems Systems have been divided into three categories in order to limit the complexity: