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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These messages are recorded in each system BITE class 3 report. The CFDS also takes into account a major objective of the line maintenance which is to avoid unjustified tsj of equipment. Confirmation tests of spurious warnings will also be covered, if applicable.
All faults present on ground and actually detected by the system will be analyzed and reported by this test. In such a case the indexes are useful to direct the trouble shooter to the correct chapter.
This is to avoid unjustified LRU removals. The advantage of this is that it is not restrictive as far as actions are concerned.
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. This type hsm system enables: The number of identifiers is limited to 6. The index pages are divided into three columns. Additional information is associated with each message. In fact, the safety procedures associated with these tests are in the AMM.
All faults detected by the systems without cockpit event are covered by a CLASS 3 fault maintenance message.
airbus a TSM – Free Download PDF
Consequently, this test may be initiated x320 the cockpit by a single operator whenever required during stopovers. Type 2 systems cannot receive this information no input bus and generate it by default. It may also be an aid in relation to the corresponding warning message and with the GMT.
If the operator wants to repeat the test he is not obliged to apply these instructions on configuration resetting. This means that in most of the cases, the fault message is associated with a cockpit event ECAM warning, local warning, flag, maintenance status The general rule is that an even suffix identifies a component on the right hand side and an odd suffix identifies a fsm on the left hand side.
Block Task Supporting Data are given to show the system layout and interconnections twm other systems. This function enables a quick access to the class 3 messages of a given system.
In order to limit the number of cockpit events 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.
Please fill this form, we will try to respond as soon as possible. Thank you for interesting in our services. The use of this function may also be requested by the TSM procedures. In order to launch at the first opportunity the proper maintenance action it is necessary to provide the information to the maintenance teams. Test re-running after repair of the fault is tsmm always necessary to check whether there is another fault or not.
Tzm layout is as follows: There are two general divisions of monitored and non-monitored faults. In order to limit the number of fault messages printed on the W320 and to give the line mechanic only the root cause of a fault, the CFDIU correlates the fault messages.
Fault Confirmation – 4. Analysis of this data will be effectively useful in the study which may enable the identification of the cause of an event. As a general rule, the test of the system including the LRU incriminated by the maintenance message message ATA will be activated.
These tests can also be menu-guided tests. Size px x x x x We need your help! This is the reason why the aircraft systems have 2 types txm memorization: We need your help to maintenance this website. For the operator, the resulting consequences are minor: Alternatively, if the user knows which system has generated the fault this step can be skipped and the trouble shooting started at the next text. Furthermore, after aircraft power up, it enables to check that all computers have correctly satisfied the related power up tests.
The first four columns contain the fault message, ATA reference, source and class.
airbus a320 TSM
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. This z320 only causes minor consequences for maintainability of type 2 systems. It is the entry point to the technical documentation. Test names are related to the tested parts.
The deletion of one configuration does not change the three digit ttsm indicator of the remaining task s. They are similar in structure to the Aircraft Maintenance Manual AMM maintenance procedures and are considered as maintenance tasks.