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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Task idents begin at and raise, in sequence, to maximum within the P. 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.

Only maintenance messages indicate possible failures. CXN02corresponds to first aircraft within the second customer version. The others are GO without conditions. For these systems, the flight condition is between takeoff and landing.

Type 2 systems cannot receive this information no input bus and generate it by default. PFR, test result, trouble shooting data if available.

Block to isolate the fault. This is essentially achieved by analysis of all cockpit events which are triggered by the monitoring of the aircraft systems. The contents of these is as follows: This type of system enables: The list does not give details of wiring to be checked. All faults present on ground and actually detected by the system will be analyzed and reported by this test. The following data are recorded in the PFR: The wording of the cautions is in fact simply a reminder of the consequences on the aircraft following test activation.


Effectivity Statements 1 Page effectivity block The statement of effectivity in the effectivity block at the bottom left of each page corresponds to the sum of the effectivities included on the page. Faults detected during flight will generate maintenance messages in the PFR associated with this flight if class 1 or 2 as defined in Para 4.

Record of Temporary Revisions. We need your help to maintenance this website.

Case related to Type 2 systems: Trouble Shooting Summary Ref. Test re-running after repair of the fault is therefore always necessary to check whether there is another fault or not. There is no ground report function for Type 3 systems. The test function shall be used in this case. In order to a32 at the first opportunity the proper maintenance action it is necessary to provide the information to the maintenance teams.

We need your help! The test has detected at least one fault. Report “airbus a TSM”.

airbus a320 TSM

The advantage of this is that it is not restrictive as far as actions are concerned. Nonetheless, their definitions make it possible to understand why certain menus are simplified. As a general rule, the test of the system including the LRU incriminated by the maintenance message message ATA will be activated. In fact, certain faults prevent to run the test more extensively.

• View topic – A AMM and TSM IN PDF FORMAT

Under these conditions this message is qualified by the unit generating it as having priority over all messages transmitted by the other systems for the same fault.


CFDS fault messages are not normally reported by the flight crew and are used by maintenance crews. Confirmation tests of spurious warnings will also be covered, if applicable. To limit BITE complexity all these conditions are assumed to be correctly applied by the operator.

In order to be able to launch the proper maintenance actions, all faults: The faults detected during flight and which remain present on ground are in the PFR and not in the ground report. Before you get access for a wiring check, make sure that you obey the applicable warning s: The first column contains warnings and malfunctions.

The Fault Symptom pages in each section are divided into the following three main columns: Block is customized by airline. This is detailed in the procedure and only mentioned in the list eg: This form of trouble shooting is not recommended.

Thank you for interesting in our services. Blockand – the titles of the tasks of P. They must be incorporated as stated on the TR transmittal sheet.