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.
| Author: | Vusho Mezikinos |
| Country: | Tunisia |
| Language: | English (Spanish) |
| Genre: | Video |
| Published (Last): | 15 July 2015 |
| Pages: | 22 |
| PDF File Size: | 8.28 Mb |
| ePub File Size: | 6.89 Mb |
| ISBN: | 467-6-70893-163-9 |
| Downloads: | 35867 |
| Price: | Free* [*Free Regsitration Required] |
| Uploader: | Tygolkree |
Description of the initial configuration, description of the actions, wording of the questions to which the operator must respond. The breakdown of each procedure is as follows: Maintenance functions 1 First group: For systems which are in standby and which fail, the fault message is immediately available in the PFR but the associated cockpit event is shown in the cockpit only when a manual switching activates this system example ADIRU3.
There are two general divisions of monitored and non-monitored faults. The fault symptoms are sorted alphanumerically to facilitate location within the priority classifications. The other maintenance messages related to the same fault are called external by the other systems. The Fault Symptom pages in each section are divided into the following three main columns: This trouble shooting guide to faults monitored and aircraft systems. Fault Isolation – 5. In order to be able to launch the proper maintenance actions, all faults: Types of systems Systems have been divided into three categories in order to limit the complexity: The list does not give details of wiring to be checked.
In certain multiple fault cases, the test may only indicate the first fault encountered. For these reasons the CFDS makes a detailed analysis to identify the responsible LRUs; this is also to confirm that the event was actually due to a hardware failure and not an intermittent fault.
If a fault appears and disappears several times during the same flight leg, the corresponding fault message is transmitted only at the first detection, but the ECAM warning for a Class 1 fault or the Maintenance Status for a Class 2 fault is displayed every time in the cockpit and transmitted every time to the Aa320.
Class 2 maintenance messages are presented in the Post Flight Report at tdm end of the flight.
Non-monitored faults are not displayed by the aircraft systems and can be of a general nature, such as: Please copy and paste this embed script to where you want to embed Embed Script. Faults not monitored by the are also covered. This means that one fault symptom is effective for at least one aircraft in the fleet.
However, only the temporary revisions deleted by the highlights of a normal revision must be removed. PFR, test result, trouble shooting data if available.
Airbus A TSM( Trouble shooting manual )
These sections are also sub-divided into various types of warnings or malfunctions in order to correspond with the divisions of the Fault Symptom pages P. This implies that the operator action must be performed before this time out.

This is detailed in the procedure and only mentioned in the list eg: All faults present on ground and actually detected by the system will be analyzed and reported by this test. It may also be an aid in relation to the corresponding warning message and with the GMT. Please fill this form, we will try to respond as soon as possible. Most systems are provided with this type of interface. The test function shall be used in this case.
To achieve its purpose, the CFDS has several major functions which supply: TO Power up to 80 kts Some of these faults have consequences on the system safety objective and are NO GO items i. It is a user-friendly monitoring device providing direct access to system menus which detect a fault for example, flag displayed on the PFD. 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.
For the TSM this is always The aircraft may be dispatched. Then there is a limited time out so as not to stop in this configuration when the monitored signals are blocked.
airbus a320 TSM
Faults detected on ground may be due to maintenance actions on the aircraft and therefore are 3a20 to be taken into account e. All faults can be divided into three groups: This is the reason why the aircraft systems have 2 types of memorization: These tests can also be menu-guided tests.
These warning messages are associated with their ATA reference aid for cross referencing with the maintenance message. The fault messages are sorted alphanumerically on the message text to facilitate location in the index. Some faults can be detected only during a specific test. This section may be consulted to check the interrogated computer standard. Microfilm cartridges are also available. Class 1 maintenance messages are presented in the Post Flight Report at the end of the flight.
Task idents begin at and raise, in sequence, to maximum within the P. This is a configuration management aid. In such a case the indexes are useful to direct the trouble shooter to the correct chapter. Block contain the information required to isolate and correct each fault symptom Ref.
Some systems do not have class 3 reports. 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. This does not necessarily mean that an effective failure is present. The remaining are ignored.
