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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It is the entry point to the technical documentation.

A brief description of the structure of Task numbers follows, for further information please refer to the AMM introduction. CFDS fault messages are not normally reported by the flight crew and are used by maintenance crews. The CFDS also takes into account a major objective of the line maintenance which is to avoid unjustified removals of equipment. Test names are related to the tested parts.

To achieve its purpose, the CFDS has several major functions which supply: The breakdown of each procedure is as follows: Additional information is associated with each message. The advantage of this is that it is not restrictive as far as actions are concerned. TO Power up to 80 kts The wording of the cautions is in fact simply a reminder of the consequences on the aircraft following test activation.

Trouble Shooting Tips Tips for using the various TSM page blocks and useful additional information are given in the following paragraphs: Case related to Type 3 systems: This is the reason why the aircraft systems have 2 types of memorization: All faults can be divided into three groups: For the TSM this is always BlockRef.


airbus a320 TSM

This does not necessarily mean that an effective failure is present. Block page number, confirm the task number at the top left and do the fault isolation procedure. They can be displayed alone without an associated warning or malfunction, in which case they may be the entry point for maintenance related trouble shooting.

Please help us x320 share our service with your friends. Nonetheless, type 2 systems having no specific function during these phases, the probability of occurrence of these cases is very low.

However, only the temporary revisions deleted by the highlights of a normal revision must be removed. Block contain the information required to isolate and correct each fault symptom Ref. In fact, certain faults prevent to run the test more extensively. The flight condition is located between first engine start up plus three minutes or eighty knots plus thirty seconds if tm plan is not available in the FMS and eighty knots plus thirty seconds after touch down.

In some cases it is possible for the trouble shooting to be covered in a chapter different to that of the ATA reference given by the warning, malfunction or CFDS fault message. Faults not monitored by the are also covered. Depending on the fault and its effect, it will be the one generated either by a computer which detects itself faulty self monitoring z320 by the computer in charge of the BITE of the system.


This action may include dynamic phases for example: This is to avoid unjustified LRU removals. The list of faults in the Fault Symptoms P. From these pages the troubleshooter is directed to the procedure in P.

Maintenance message classification 1 General Maintenance message classification is based on fault consequence. Only maintenance messages indicate possible failures.

There is no ground report function for Type 3 systems.

x320 The messages in this section concern faults detected during flight and on ground, the wording GND preceding the list of messages related to the faults detected on the ground in accordance with the same ground report logic as for type 1 systems. This report is the main source of information used to initiate trouble shooting and to decide on the required maintenance actions.

They are always GO without any restriction. These messages are recorded in each system BITE class 3 report.

Airbus A TSM( Trouble shooting manual )

Test re-running after repair of the fault is therefore always necessary to check whether there is another fault or not. In each ATA chapter page blockthe table lists: Block to isolate the fault. It is divided stm the following four sections: This correlation has to be performed by the line mechanic.