(c)
Disclaimer Clause AIRBUS HEREBY EXPRESSLY DISCLAIMS ANY AND ALL WARRANTIES, EXPRESSED OR IMPLIED, ORAL OR WRITTEN, ARISING BY LAW, COURSE OF DEALING, OR OTHERWISE, AND WITHOUT LIMITATION ALL WARRANTIES AS TO QUALITY, OPERATION, MERCHANTABILITY, FITNESS FOR ANY INTENDED PURPOSE, AND ALL OTHER CHARACTERISTICS WHATSOEVER, OF CUSTOMER ORIGINATED CHANGES INCORPORATED INTO THE TECHNICAL DATA ISSUED BY AIRBUS. THE FOREGOING DISCLAIMER SHALL ALSO APPLY TO ANY OTHER PORTION OF AIRBUS TECHNICAL DATA WHICH MAY BE AFFECTED BY SUCH CUSTOMER ORIGINATED CHANGES.
(a) COC Identification
COCs incorporated into the TSM at Customer request to reflect *
data or procedures originated by and peculiar to that specific *
customer, will be permanently identified by the COC reference *
number and by asterisks in the right hand margin on the *
indiviual pages (see example in the margin of this paragraph). *
The COC data incorporated into the Technical Data is shown *
in "POST" configuration only. *
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CES L. Requests for TSM Revision and Correspondence
(1)
An RFI/RFR (Request For Information/Request For Revision) form is provided to expedite AIRBUS responses to TSM questions. It is requested that this form be used for any questions concerning the TSM.
(2)
All communications concerning the TSM should be sent to:
AIRBUS S.A.S.
Technical Data Support and Services
1 Rond Point Maurice Bellonte
31707 Blagnac Cedex
France
M. Text Breakdown (AMTOSS) and Configurations
The fault isolation procedures can generally be considered as corrective maintenance tasks. Therefore, AMTOSS (Aircraft Maintenance Task Oriented Support System ) has been applied to the TSM for the functional arrangement of the data. This also has the advantage of consistency with the AMM (Aircraft Maintenance Manual). Consequently, the fault isolation procedures are broken down into AMTOSS tasks and subtasks. The Task numbers are printed in the TSM and the subtask numbers are omitted ( as an option, the subtask numbers can be printed ). A brief description of the structure of Task numbers follows, for further information please refer to the AMM introduction.
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CES
Task Elements/ TASK XX-XX-XX-XXX-XXX-XXX-XXX 1 2 3 4 5 6 7
-------------------------------------------------------------------------------ELEMENT FUNCTION -------------------------------------------------------------------------------1 to 3 ATA six digit number
4 This three digit numeric function code is used to indicate the particular function involved. For the TSM this is always 810.
5 This three digit numeral enables a unique identification task number to be allocated for all Tasks which are identically numbered throughout the preceding elements. Task idents begin at 801 and raise, in sequence, to 999 (maximum) within the P. Block. Illustrations and tables are considered as tasks.
6 This three digit alphanumeric indicator comprises of:
-First digit alpha to indicate a different configuration (modification, service bulletin(s), etc.).
-Second and third digit numerals to indicate alternative
methods/techniques of trouble shooting
Example:
-78-31-00-810-801-A 01
| |
| |
| |
This alpha digit-| |
identifies a |
configuration |
(SB etc.). |
|
|
These two numerical-|
digits identify a
configuration of
method/technique.
-Configurations due to different modification standard, Service Bulletin (SB) incorporation, etc.:
78-31-00-810-801-A
-|
|
--------------------------------
* this digit is blank when no
configuration exists
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CES -------------------------------------------------------------------------------ELEMENT FUNCTION -------------------------------------------------------------------------------
* when subsequent configurations of criteria are incorporated, this digit changes as follows: 78-31-00-810-801-A first configuration 78-31-00-810-801-B second configuration 78-31-00-810-801-C third configuration
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