![]() Before you get access for a wiring check, make sure that you obey the applicable warning s: Some systems do not have class gsm reports. ![]() The LEP lists all pages valid for the a3220 and their issue dates. The general rule is that an even suffix identifies a component on the right hand side and an odd suffix identifies a component on the left hand side. 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.Ĭase related to Type 2 systems: This trouble shooting guide to faults monitored and aircraft systems. The list of faults in the Fault Symptoms P. To limit BITE complexity all these tm are assumed to be correctly applied by the operator. Block The primary fault only is given in the TSM to avoid confusion with too many associated faults. These messages are recorded in each system BITE class 3 report. It is necessary to confirm all faults of the ground report by activating a test or a procedure described in the TSM.Ĭlass 1 maintenance messages are presented in the Post Flight Report at the end of the flight. In order to limit the number of fault a3200 printed on the PFR and to give the line mechanic only the root cause of a fault, the CFDIU correlates the fault messages. The identifier s are the computers which have also reacted in relation to the fault by generating: These tests can also be menu-guided tam.Īdditional information is associated with each message. It will be used to confirm the presence of a fault or to eliminate any ambiguity. Everyday low prices and free delivery on eligible. COMPRESSOR AERODYNAMICS CUMPSTY PDF PDFIllustrations and tables are considered as tasks. DIRECTING THE DOCUMENTARY MICHAEL RABIGER PDF - Buy Directing the Documentary 6 by Michael Rabiger (ISBN: ) from Amazon's Book Store. 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 a3320 or class 2 fault message because it is already done by another system. This form of trouble shooting is not recommended. COMPRESSOR AERODYNAMICS CUMPSTY PDF PLUSThe flight condition is located between first engine start up plus three minutes or eighty txm plus thirty seconds if flight plan is not available in the FMS and eighty knots plus thirty seconds after touch down. This implies that the operator action must be performed before this time out. The test function shall be used in this case. It then realises the BITE function and therefore reports on behalf of all system computers. May 9th, – Podle zákona o evidenci.Īlternatively, if the user knows which system has generated the fault this step can be skipped and the trouble shooting started at the next text. BOOK ID: byku1lDmnQdq Airbus A Tsm DOWNLOAD Book Free. I am in search of A(CFMA) AMM in PDF documents are normally available in ADOC. Creating and updating the manual, maintenance procedures, troubleshooting (AMM, TSM). Technical documentation for the aircrafts. ![]()
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