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 zákona o evidenci.

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This architecture provides for a better targeted diagnosis by correlating data between system computers as well as reducing bus links with the CFDIU. It then realises the BITE function and therefore reports on behalf of all system computers.

This means that one fault symptom is effective for at least one aircraft in the fleet. The warnings and malfunctions are sorted rsm to facilitate location in each of the sections and sub-divisions. Consequently, normally these tests are not performed during a short stopover. However, only the temporary revisions deleted by the highlights of a normal revision must be removed.

The contents of these is as follows: Trouble Shooting Tips Tips for using the various TSM page blocks and useful additional information are given tsk the following paragraphs: CXN01 corresponds to the first customer version. To achieve its purpose, the CFDS has several major functions which supply: This report s320 the main source of information used to initiate trouble shooting and to decide on the required maintenance actions.

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This is a32 an aid in trouble shooting faults difficult to resolve. Each page of the index is divided into five columns. The faults detected during flight and which remain present on ground are in the PFR and not in the ground report.

Examples of trouble shooting these faults are given in the following trouble shooting examples.

Record tzm Temporary Revisions. Before you get access for a wiring check, make sure that you obey the applicable warning s: Introduction The introduction provides the following information: Block a Possible Causes This lists all the suspect items in the fault isolation procedure to allow assembly of all items required to fix the fault. The advantage of this is that it is not restrictive as far as actions are concerned.

This function enables a quick access to the class 3 messages of a given system. Touch down up to 80 kts Front Matter The front matter contains information on the revision status, management of pages and updating records for the TSM.

airbus a320 TSM

Test re-running after repair of the fault is therefore always necessary to check whether there is another fault or not. CXN02corresponds to first aircraft w320 the second customer version.

This is achieved with the normal cockpit controls engagement levers, a30 switches by selecting the related control off then on or by action on the corresponding circuit breaker. This type of system enables: Nonetheless, type 2 systems having no specific ts during these phases, the probability of occurrence of these cases is very low.

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All faults can be divided into three groups: The purpose is to supply additional information on conditions prevailing when the maintenance message was generated. Faults not monitored by the are also covered.

Intech | AMM / TSM

This is detailed in the procedure and only mentioned in the list eg: Alternatively, if the user knows which system has generated the fault this step can be skipped and z320 trouble shooting started at the next text. In order to limit the number of cockpit a230 displayed to the pilots after a single fault, some systems do not generate a cockpit event while they send a class 1 or class 2 fault message because it is already done by another system.

The microfilm cassettes are filmed with the appropriate pages for the revision inserted. Therefore, each system has in memory an information linked to fsm message transmitted to the CFDIU which defines its internal or external attribute so that the CFDIU can give priority to the most accurate one.