User Guide
V 1.4
February 2019
PAGE 1/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Contents
ABBREVATIONS ..................................................................................................................... 3
1.
INTRODUCTION ....................................................................................................... 4
1.1 LIST OF AVAILABLE TECHNICAL DATA DOCUMENTATION ................................................... 4
1.2 LIST OF EFFECTIVE TECHNICAL DATA ............................................................................ 6
2. PRE-REQUISITES................................................................................................................ 8
3. TECHNICAL DATA NOTIFICATIONS ...................................................................................... 8
4. HOW TO ACCESS AIRNAVX .................................................................................................. 9
4.1 THROUGH AIRBUSW ORLD ............................................................................................ 9
4.2 THROUGH AIRBUSSUPPLY ............................................................................................ 9
5. AIRNAVX OVERVIEW ......................................................................................................... 10
5.1 AIRNAVX COMMON MAIN FEATURES .............................................................................. 11
5.2 DATA SEARCH ............................................................................................................ 29
5.3 MY LIBRARY ............................................................................................................... 39
5.4 TROUBLESHOOTING ................................................................................................... 44
5.5 ALLOWABLE PART CONFIGURATION (DEMO) ................................................................ 47
6 APPLICATION RELATED DETAILS ........................................................................................ 54
6.1
AIRNAVX TIMEOUT ......................................................................................................
54
6.2 PUBLICATION RULES FOR AIRNAVX ............................................................................... 54
6.3 SHIPPING INFORMATION .............................................................................................. 55
7. HELP CENTRE ................................................................................................................. 55
8. CONTACT US ................................................................................................................... 56
PAGE 2/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
ABBREVATIONS
UEA
User entity administrator
FIN
Functional Item Number
TF/IDF
MRO
Term frequency/inverse document frequency
Maintenance, Repair & Overhaul
A/A
Airworthiness Authority
M&E
Maintenance & Engineering
F.Ops
Flight Operations
MSN
Manufacturer Serial Number
FSN
Fleet Serial Number
FIN
Functional Item Number
A/C
Aircraft
UMC
ECAM
User and access Management tool
Electronic Centralized Aircraft Monitoring
PAGE 3/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
1. INTRODUCTION
X
airnav is a unique solution allowing Airline Customers, MRO’s, A/A, Leasing Companies, Airbus partners and Suppliers to list, download, browse and search complete Airbus technical documentation.
This new browser, available online, is:



Reliable : No more plug-in required (Java), Robust, based on state of the art technology
Efficient: Fast response time, Improved download features
Easy to use :Simple usability, Powerful instant search
1.1 LIST OF AVAILABLE TECHNICAL DATA DOCUMENTATION
X
Depending on the company access rights the technical data documents available in airnav are listed below:
Acronym
Doctype displayed to end user
Domain
Airtemporary / Associated Data
M&E
AirN@v / Associated Data B2/B4
M&E
AC
Aircraft Characteristics - Airport and Maintenance Planning
M&E
ACMFP
Aircraft Characteristics/Maintenance Facility Plan
M&E
ACMS Product Set
ACMS Alpha Call-up Parameters
Description
ACMS Report description
ACMS SAR Channels System Pages
and Servicing
ACMS ACARS Downlink Uplink
Aircraft Condition Monitoring System
Aircraft Condition Monitoring System - Alpha Call-up Parameters
Description
Aircraft Condition Monitoring System - Report description
Aircraft Condition Monitoring System - SAR Channels System Pages
and Servicing
Aircraft Condition Monitoring System - ACARS Downlink Uplink
M&E
ACRT
Additional Cross Reference Tables
M&E
ACT
Actual Configuration
M&E
ACTP
Preliminary Actual Configuration
M&E
AFM
Airplane Flight Manual
F. Ops
AMM
Aircraft Maintenance Manual
M&E
ARM
Aircraft Recovery Manual
M&E
ASM
Aircraft Schematic Manual
M&E
ATI
ATA Index
M&E
AWL
Aircraft Wiring List
M&E
AWM
Aircraft Wiring Manual
M&E
C@dets
Computer Assisted Documentation Education Tutorial
M&E
CCOM
Cabin Crew Operating Manual
Compliance Document Damage Tolerance Data for Repairs and Alterations
F. Ops
CDDTDRA
M&E
M&E
M&E
M&E
M&E
PAGE 4/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
CFM
Cable Fabrication Manual
M&E
CLS
Cargo Loading System
M&E
CML
Consumable Material List
M&E
CMM (CMMm)
Component Maintenance Manual Manufacturer
M&E
Line Maintenance
Line Maintenance for A350
M&E
CSDBP
Raw Data Line Planning
M&E
DFDRS
Digital Flight Data Recording System
M&E
DFPRM
Duct and Fuel Pipe Repair Manual
M&E
DRM
Duct Repair Manual
M&E
FLS - eBinder
FLS - eBinder
M&E
ESLD
ECAM System Logic Data
M&E
ESPM
Electrical Standard Practices Manual
M&E
FCOM
Flight Crew Operating Manual
F. Ops
FCOM Vol8 GE
Flight Crew Operating Manual
F. Ops
FCOM Vol8 PW
Flight Crew Operating Manual
F. Ops
FCTM
Flight Crew Techniques Manual
F. Ops
FDRPL
Flight Data Recording Parameters Library
M&E
AFM
Flight Manual (A300 & A310 only)
F. Ops
FPRM
Fuel Pipe Repair Manual
M&E
IPC
Illustrated Parts Catalog
M&E
LRE
List of Radioactive and Hazardous Elements
M&E
LTM
Livestock Transportation Manual
M&E
MFP
Maintenance Facility Planning
M&E
MMEL
Master Minimum Equipment List
F. Ops
MMP
MMEL Maintenance Procedure
F. Ops
MPD
Maintenance Planning Document
M&E
NTM
Non-destructive Testing Manual
M&E
OEB FCOM Vol 2
Operations Engineering Bulletins for FCOM Volume 2
F. Ops
OEB QRH
Operations Engineering Bulletins for QRH
F. Ops
PMS
Process and Material Specification
M&E
QRH
Quick Reference Handbook
F. Ops
RAG
Repair Assessment Guidelines
M&E
REG
Repair Evaluation Guidelines
M&E
FLS - Retrofit
Field Loadable Software - Retrofit
M&E
AirN@v / Line Maintenance
M&E
AirN@v / Maintenance
M&E
AirN@v / Planning
M&E
AirN@v / Repair
TR AirN@v onboard
M&E
M&E
PAGE 5/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
airnavX Standalone
airnavX Standalone software
M&E
airnavX Intranet Software
airnavX Intranet Software
M&E
SM
Standards Manual
M&E
SRM
Structural Repair Manual
M&E
STS
Spares Technical Specification
M&E
TEM
Tool and Equipment Manual
M&E
TM
Transportability Manual
M&E
TR AFM
Temporary Revision Airplane Flight Manual
F. Ops
TR AMM
Temporary Revision Aircraft Maintenance Manual
M&E
TR ASM
Temporary Revision Aircraft Schematic Manual
M&E
TR AWM
Temporary Revision Aircraft Wiring Manual
M&E
TR CSDBL
Temporary Revision Raw Data Line Maintenance
M&E
TR ESPM
Temporary Revision for Electrical Standard Practices Manual
M&E
TR FCOM
Temporary Revision Flight Crew Operating Manual
F. Ops
TR FCOM Vol 8 GE
Temporary Revision Flight Crew Operating Manual
F. Ops
TR FCOM Vol 8 PW
Temporary Revision Flight Crew Operating Manual
F. Ops
TR FIM
Temporary Revision Fault Isolation Manual
M&E
TR IPC
Temporary Revision Illustrated Parts Catalog
M&E
TR MMEL
Temporary Revision Master Minimum Equipment List
F. Ops
TR NTM
Temporary Revision Nondestructive Testing Manual
M&E
TR AirN@v On Board
Temporary Revision AirN@v On Board
M&E
TR QRH
Temporary Revision Reference Handbook
F. Ops
TR SRM
Temporary Revision Structural Repair Manual
M&E
TR TSM
Temporary Revision Trouble Shooting Manual
M&E
TSM
Trouble Shooting Manual
M&E
WBM
Weight and Balance Manual
F. Ops
This scope is available for all programs except for A300/A310 documentation.
1.2 LIST OF EFFECTIVE TECHNICAL DATA
The List of Effective Technical Data is also available under My Library. It is now called My LETD and can be downloaded in the form of a zip containing a PDF and CSV file (1).
Note: The LETD global planning can also be retrieved in CSV format under My Library (2).
PAGE 6/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 1 - List of effective Technical Data
PAGE 7/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
2. PRE-REQUISITES
X
airnav is available online on AirbusWorld and AirbusSupply. The user can access it from any device (PC/Laptop or
tablet devices).
X
This online version of airnav relies on the same prerequisites as the AirbusWorld Hardware and Software prerequisites.
X
The following internet browsers are compatible with airnav :

Google Chrome version 56 and above

Internet Explorer version 11 and above

Safari version 10 and above
For the Multi-Download, the following prerequisites are necessary:

Any java versions from 1.7 (32 bit only)

Proxy declaration has to be set
For Proxy declaration information, please contact the local IT team of your company.
3. TECHNICAL DATA NOTIFICATIONS
The means to be notified once a new technical data document is issued is detailed in the AirbusWorld How do I subscribe to notification FAQ.
PAGE 8/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
4. HOW TO ACCESS AIRNAVX
4.1 THROUGH AIRBUSWORLD
X
airnav can be accessed using its dedicated tile available in the “app catalogue” page of AirbusWorld.
Figure 2 - Fig: airnavX tile in AirbusWorld
4.2 THROUGH AIRBUSSUPPLY
X
For supplier entities airnav can be accessed using the direct link available on the homepage of AirbusSupply:
Figure 3 - Figure 2 - airnavX link in Airbus Supply
PAGE 9/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5. AIRNAVX OVERVIEW
X
There are 4 different entry points in airnav application. Each of them will be detailed further below.
Figure 4 - Entry points into airnavX
PAGE 10/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.1 AIRNAVX COMMON MAIN FEATURES
X
airnav offers a set of various features; some of them are common between the three sections and will be detailed
further below.
5.1.1 airnavX working context
X
The airnav working context is located on the left side of the application. It allows the users to apply various filters on
their library/search results for refinement purpose and can be accessed from every airnav
X
tab.
Figure 5 - airnavX working context
The filters differ from one section to another and therefore will be detailed further on each section chapters.
Note: Specific manuals such as the DFPRM contain a Part Number filter in the document view working context:
PAGE 11/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 6 - Part Number filter in the DFPRM document view working context
5.1.2 Pre-selecting the working context through AirbusWorld
X
airnav working context is already pre-filtered according to the AirbusWorld context selected by the user. The filter
X
thus created will be applied automatically upon launching airnav application.
However the user can update these filters afterwards.
Figure 7 - AW context replication on airnavX
PAGE 12/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.1.3 Consultation of technical data documentation (Document view)
The user can consult the manual or the attachments using the Browse button (
Browse button, the user will switch to document view.

) available. By clicking on the
While in Data search:
Figure 8 - Consulting manuals from Data Search

While in My Library:
Figure 9 - Consulting manuals in My Library
PAGE 13/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.

While in Troubleshooting
Figure 10 - Consulting manuals in Troubleshooting
Several features are available while browsing manual in Document view. They are detailed below:
Button
Function
Used to set the Data to hidden Mode based on the
X
effectivity / applicability set in the airnav context
Used to view a document in a new tab. Helps to view
the document and figures if any in two separate panes
side by side.
PAGE 14/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Used to open the manual in consultation mode (Document View). When this button is activated, the Document view opens in a new Tab.
Used to move from one figure / illustration to another.
Used to print the content currently being consulted.
Note: The “collapsed” sections (if any) will be expanded
and the illustrations (if any) will be printed at the end.
Used to open the images in a new tab. This would help
view the figures better and easy provides additional
options.
Add the consulted task to the Job Card basket
Next/previous search results highlighted word
Launch the MSN comparison view (see §5.2.5)
Launch the Allowed Part(s) consultation tab (see § 5.5)
PAGE 15/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Some additional functionalities are available for easy consultation of illustrations. This includes functions such as zoom
in, zoom out, rotate, highlight hotspots, etc.
Figure 11 - Additionnal image features
1
Previous illustration / Previous sheet
2
Next illustration / Next sheet
3
Move illustration (ctrl + left click can also be used)
4
Zoom in
5
Zoom out
6
Rotate left
7
Rotate right
8
Fit to window
9
Toggle global view
10 Toggle hotspots
Note: The
button allows the user to print the consulted illustration only.
Other additional functionalities are available for easy consultation of 3D illustrations:
Figure 12 - 3D illustration
PAGE 16/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Illustration Mode – 3D
Button
Function
The 3D illustration will fit to the screen
The 3D illustrations enlarges back to the selected
Zoom
Search any value displayed in the illustration. Using
this option helps you highlight in red the item in the
illustration
This option can be used to hide a selected part of the
illustration
This option can be used to restore visibility of a hidden
selected part of the illustration
This button restores the illustration into original size.
Selecting this option lets you adapt the font size. Once
select, the below prompt appears:
Saves the current illustration as a screenshot.
PAGE 17/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Saves the current illustration as a black and white
screenshot.
Usually the 3D illustrations have a blue back-ground
but if needed that can be changed to white using this
option.
Selecting this option shows the center of the illustration. Once selected the option will be highlighted:
Rotates the figure.
Create an annotation on the existing 3-D figure.
Delete the created annotation on the existing 3-D figure.
Edit the created annotations.
Delete all the created annotations on the existing 3-D
figure.
This button allows you to filter the parts illustrated using
the given menu.
PAGE 18/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Toggle the skin panels of the 3D figure.
Toggle the skin model of the 3D figure.
Note: The 3D navigation is detailed further in this video.
5.1.3.1 Display of illustrations:
In document view, while browsing a task it is possible to display an illustration while browsing the text by clicking on
the corresponding Ref. link:
PAGE 19/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 13 - Display of an illustration 1/3
This will display the illustration at the bottom at the test or open the sheet selection pop-up:
Figure 14 - Display of an illustration 2/3
PAGE 20/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 15 - Display of an illustration 3/3
The
button will open the illustration in a new dedicated tab:
Figure 16 - Open illustration in a new window
PAGE 21/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
The
button will open a new consultation tab divided in two sections, with the text on the left and the illustration on
the right:
Figure 17 - Text vs illustration
5.1.3.2 Caution while consulting a historic revision of a manual
If a user is consulting a historic revision of a manual, a warning message in bold orange color is displayed to alert the
customer that the revision is not the current one.
"Caution: This is not the latest document revision. Hyperlinks may lead to latest revision”
Figure 18 - Warning message displayed while viewing a historic revision of a document
PAGE 22/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.1.3.3 Consultation of a temporary revision
When a manual contains a temporary revision it is listed on the List of effective temporary revisions section located in
the Manual Front Matter:
Figure 19 - List of effective temporary revisions
While browsing the manual to the Temporary Revision location it will appear as follow:
PAGE 23/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 20 - Consult a Temporary Revision
5.1.3.4 Document View search
X
Currently airnav offers 4 different ways of searching:
1. Search at complete data base level (will be detailed in the Data search chapter)
2. Search at document level
PAGE 24/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 21 - Search at document level
PAGE 25/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
3. Search at fragment level in HTML
Using the web-browser search function (ctrl + f) as follow:
Figure 22 - Search at fragment level (HTML)
4. Search at fragment level in PDF
Using the web-browser PDF plugin search function as follow:
Figure 23 - Search at fragment level (PDF)
PAGE 26/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.1.3.5 URL and Bookmarks
X
With airnav it is now possible to bookmark favourite searches, filters or sections of a given manual (in this particular
case once a new revision is issued the bookmark may not work anymore i.e a suppressed task). The sections and
X
searches can be also shared among airnav users.
5.1.3.6 airnavX export function
5.1.3.6.1 P/N export
The list of P/N can be exported in csv format from the document view. The general P/N data list is located in the Manual Front Matter:
Figure 24 - General P/N Data List export
5.1.4 Job Card printing
Manuals such as the AMM and TSM offers the possibility to print tasks as Job Cards. While consulting a task a simple
click on the will reveal the Job Card menu:
PAGE 27/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 25 - Job Card menu
5.1.4.1 Job Card packages
The Job Card packages can be reached by clicking on the
right corner of the application.
button located next to the Help Centre button on the top
Figure 26 - Job cards packages
PAGE 28/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Once the package is named and ordered, the Job Card package can be generated:
Figure 27 - Job cards packages generation 1/2
Figure 28 - Job cards packages generation 2/2
5.2 DATA SEARCH
X
The Data search module of airnav allows the users to search within the content of the available technical data using
inbuilt filters (working context) and key words.
5.2.1 Data search working context
As explained in chapter 5.1.1 the working context filters differ from one section to another. In the data search module
the filters are listed as follow:

Customization

Aircraft types

Tail Number - MSN - FSN

Doc types

ATA

FIN
PAGE 29/56
© Airbus SAS, 2019. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of Airbus SAS. No intellectual property rights
are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 29 - Data Search working context
The following filters are interrelated on an up/down basis for the 3 first ones: Customisation  Aircraft type  MSN
hence:

Selecting a customization will automatically refine the Aircraft type list and/or the MSN list.

Selecting an Aircraft type will automatically refine the MSN list but not the customization one (however upon
selecting a wrong customization the A/C type and the MSN filters will be automatically removed).
On a down/up basis:

Selecting a given MSN will automatically apply the corresponding Aircraft type filter but not the customization one.
5.2.2 Data search function
X
The airnav Data Search function has been conceived to display the expected result within the first five hits of the list.
It will allow the user to search within the content of the available technical data using some predefined rules, the first
one being the working context (already detailed in the above chapter):
PAGE 30/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.

By default the search will look for exact words(s) including common extensions (such as …tion, …ed,
…al…).


The text entered in the search box is not key sensitive.


Ex: Install  Install, Installation, Installed.
Ex: Fuel  Fuel, FUEL, fuel…
No automatic correction on mistyping
The search function also offers advanced wildcards features such as:

The * will replace any placeholder (it is however impossible to use it in the middle of a term or at the beginning):


The “” will return the exact phrase between double quotes:


Ex: Landing -light  only the result with landing minus the one with light
The logical connecter OR cannot be used as such but with the “|” character in order to display results with either one of the words:


Ex: Fuel leak  only results with both Fuel AND leak will be displayed.
The “-“ operator can be used right next to a term (no space) to exclude it from the search results:


Ex: “Fuel leak”  only results having the exact phrase between double quotes.
Multiple word search will, by default apply an implicit “AND” or “+” connecter between each words:


Ex: GPA110*  GPA1102-00, GPA1103-00, GPA1104-00…
Ex: Fuel | leak  results with one of the words.
The parenthesis operator can be used to indicate the precedence of a word

Ex: landing + (gear | light)  signify precedence for gear | light
NOTE 1: The ? (question mark) for 1 missing character cannot be used
NOTE 2: These tips can be retrieved by clicking on the
button located on the left of the search box:
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 30 - airnavX search tips
5.2.3 Data search results
As explained above the search engine’s aim is to provide relevant results within the five first search hits. It combines
two scoring methods to rank the search results:
1. TF/IDF: This score represent the ratio of the term frequency in the document and the term relevancy.
2. Manual scoring: The search engine looks for the term(s) in various places within the technical data documentation, these places have been given a different scoring.
Note: Searching for a task/publication with its incomplete reference will not necessarily return the task/publication itself
but may return other items first because the search criteria is mentioned/called more time in these items. The search
results are displayed as follow:
Figure 31 - Search result example
PAGE 32/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.2.4 Search/filter by FIN reference
X
In airnav data search it is also possible to search directly for FIN. This search can be performed either on the text
(content of a given manual) or within the illustrations (Schematic/Wiring).
Figure 32 - FIN search/filter (text)
PAGE 33/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 33 - FIN search/filter (Schematics/Wiring)
Note: There’s a limitation with the FIN search, it does not search within the manuals illustrations (such as AMM,
IPC…) only in the Schematic/Wiring at the moment.
Figure 34 - FIN search/filter (FIN HOME)
PAGE 34/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
DATA SEARCH BEST PRACTICE
X
1. Filtering the search using airnav working context can reduce significantly the number of search results:
Figure 35 - Filtering the search using airnav
X
working context
PAGE 35/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
2. Using connecters and wildcards will also help refine the search:
Figure 36 - Using connecters and wildcards to refine the search
5.2.5 MSN comparison
This feature allows the end users to compare tasks between up to 3 MSNs. To do so user needs to proceed as follow:
1. While browsing a manual, click on the comparison tab after selecting the chapter. Below is an example for
TOWING AND TAXIING.
Figure 37 - MSN comparison 1/3
PAGE 36/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
2. Select the MSNs that needs to be compared
Figure 38 - MSN comparison 2/3
Figure 39 - MSN comparison 3/3
Note: Please note the maximum MSN that can be compared is 3. This can be done as shown in the figure above. Toward the right top corner there is a plus button to add one more comparison box.
PAGE 37/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 40 - Compare up to 3 MSNs
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.3 MY LIBRARY
My Library offers one single access point to list and download Airbus Technical documentation (Maintenance, Engineering and Flight Operations). Field Loadable Software (FLS), airnavX intranet and standalone software are also
available for download.
The list of technical data available correspond to the user’s company access rights as defined by the Airbus technical
data contracts or Airlines’ delegations (for non-airline customers).
5.3.1 My Library working context
As explained in chapter 5.1.1 the working context filters differ from one section to another. In My Library the filters are
listed as follow:

Customization

Aircraft types

Doctypes
Figure 41 - My Library working context
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.3.2 Technical Data Documentation consultation in My Library
5.3.2.1 Consultation of current and previous revisions
To consult the current revision of technical data documentation, user can click on the Browse button ( ) the selected
manual will then be opened in a new Document View tab.
Note 1: In the Document View tab, consultation is only possible at node level.
The previous revisions can be consulted using the history button (
).
Refer to the screenshot below for a detailed view:
Figure 42 - Browse a manual from My Library
Note 2: Some doctypes are not available for browsing (ex: AirN@v / XXX doctypes are only available to download).
PAGE 40/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 43 - New Document View tab opens up
5.3.3 Downloading manuals from My Library
The technical data documentation can be downloaded directly from My Library. However the user must be granted
with the “download right”. This right is not given “By Default” and shall be granted by the company User Entity Administrator (UEA) through the UMC tool.
5.3.3.1 Single download
To download a single item, the user has to click on the “download” button (
Refer the screenshot below for a detailed view.
) displayed along with the document.
PAGE 41/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 44 - Download of a single manual or an attachment
Note: The previous revision of a manual can also be downloaded by clicking on the history button.
Figure 45 - Download of previous revisions of a manual
5.3.2.2 Multi-Download
In order to download multiple items, users can launch the search from the Multi-download view, select and download
the required manuals/software/attachments in a single package.
Note: As explained in chapter 2 java 32 bit is required to use the multiple download feature.
Figure 46 - Download of manuals along with the attachments
5.3.2.3 Selecting the relevant file format before downloading
Some manuals come in different file format (such as pdf, xml, sgml…). In order to find out which format is available to
download user can use the menu button ( ) located next to the manual name to display the list of available formats.
Then upon clicking on the download button this list will also be displayed to allow the user to select the relevant format.
PAGE 42/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 47 - Downloading from several format types of a manual
5.3.4 My Library buttons detail
Button
Function
Expand publication details
such as the format, size, next
scheduled revision…
Download button
Expand doc history to display
previous revision(s) in order to
download/consult it
Expand the list of available
Temporary Revision(s)
PAGE 43/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Browse the selected Technical publication
Browse the latest available
revision of the selected Technical publication
5.4 TROUBLESHOOTING
The Troubleshooting module allows the user to find relevant fault isolation tasks using Fault codes, ECAM warning,
messages, etc. as inputs.
Note: An aircraft must be selected in the working context prior to launch any search.
5.4.1 Troubleshooting working context
In the Troubleshooting module the filters are listed as follows:

Customization

Aircraft types

Tail number – MSN - FSN
Figure 48 - Troubleshooting working context
Note: User can only select one aircraft applicability to use the troubleshooting function.
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.4.1 Looking for a troubleshooting task
In order to find the relevant troubleshooting task user can use the following fields (see Figure 30 and 31 below for details)

1  Type: Eg: Full search, ECAM alerts, local effect, Fault message, crew/maintenance obs

2  Fault code: A particular fault code can be entered to narrow down the search (For A350 and A380)

3  Description: This field is used to search fault messages effects from their titles or panel designations (for
local effects)

4  Source: This field is used to search fault messages effects from source designations (only for fault messages)

5  ATA Ref: A particular fault code can be entered to narrow down the search (For A320 family and
A330/A340 family)

6  Class: This field is used to search fault messages effects from class (only for fault messages)

7  The + button can be used to search a troubleshooting task based on correlated item (up to 4 items can
be correlated)
Clicking on the associated task reference will enable the users to consult the relevant troubleshooting task.
Figure 49 - Looking for a troubleshooting task A320 family and A330/A340 family
Figure 50 - Looking for a troubleshooting task A350/A380
PAGE 45/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Once the TSM task opens in Document View user can check the relevant Fault Symptoms by clicking on the related
button as follows:
Figure 51 - Fault symptom
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
TROUBLESHOOTING BEST PRACTICE
Using the relevant troubleshooting functions can reduce significantly the number of search results:
Figure 52 - Using the troubleshooting functions
5.5 ALLOWABLE PART CONFIGURATION (DEMO)
Allowable part configuration is a new airnavX online consultation service which provides a simple answer to customers
regarding parts allowed for installation on a given MSN, at a given position. It provides fresh data, updated on a
weekly basis for all aircraft family except the A300/A310. It can be accessed directly from its dedicated tab or by using its dedicated button (
) while browsing manuals such as the IPC, MIPD and SR IPD.
The current version of Allowable Part Configuration is only a Demo and therefore all data displayed in the Allowable consultation service are provided for test purpose. It shall NOT be used to
ensure aircraft continued airworthiness.
The Entry into Service is scheduled for the first semester of 2019, at the time dedicated communications will be sent.
PAGE 47/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.5.1 Allowed Part Configuration working context
As explained in chapter 5.1.1 the working context filters differ from one section to another. In Allowable Part Configuration the filters are listed as follow:

Customization

Aircraft types

Tail Number – MSN - FSN
Figure 53 - Allowed Part Configuration working context
Note: An aircraft must be selected in the working context prior to launch any search. Only one aircraft can be selected.
5.5.2 Allowed Part Configuration search
Allowable Part Configuration offers 3 search possibilities:

Search by FIN:
Figure 54 - Search by FIN
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.

Search by Figure-Item
Figure 55 - Search by figure item
Note: The source can be IPC, SRM, MIPD (A350) and SRIP (A350).

Search by Part Number
Figure 56 - Search by Part Number
Note: The search by Part Number is an intermediate search that will provide the list of location and Figure Item for a
given P/N. User can either click on the desired FIN or Figure Item to launch the corresponding search.
PAGE 49/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
5.5.3 Allowed Parts without operational conditions
Figure 57 - Allowed Parts without operational conditions
It is possible to reveal the related figure item by clicking on the
or
button:
Figure 58 - Related figure item 1/2
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 59 - Related figure items 2/2
5.5.4 Allowed Parts with operational conditions
Figure 60 - Allowed part with operational conditions
5.5.5 Allowed Parts with Conditional Spare Part(s)
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 61 - Allowed Part(s) with conditional Spare Parts
5.5.6 Simulate SB(s) embodiment:
With Allowed part configuration it is now possible to simulate SB(s) embodiment:
Figure 62 - Simulate SB(s) embodiment 1/2
PAGE 52/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
Figure 63 - Simulate SB(s) embodiment 2/2
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
6 APPLICATION RELATED DETAILS
X
6.1 AIRNAV TIMEOUT
X
The time-out of airnav is the same as AirbusWorld i.e. After 1 hours of inactivity; you will have to login again.
X
6.2 PUBLICATION RULES FOR AIRNAV
The number in the brackets tells us the number of publications available in a particular format.
For Maintenance & Engineering domain:
Before airnav
Consultation
Download
X
After airnav
X
PDF (1)
PDF (2)
AirN@v (1)
AirN@v (1)
SGML (5)
SGML (2)
XML (5)
XML (2)
AirN@v on ground (1)
AirN@v on ground (2)
Airn@v on board (1)
AirN@v on board (1)
airnavX intranet (2)
airnavX standalone (1)
PDF (1)
PDF (2)
For Flight Operations domain:
Before airnav
Consultation
Download
X
After airnav
PDF (1)
PDF (2)
OLB (1)
OLB (2)
SGML (5)
SGML (5)
XML (5)
XML (5)
OLB (5)
OLB (5)
PPFO (5)
PPFO (5)
CADOC (5)
CADOC (5)
X
PAGE 54/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
6.3 SHIPPING INFORMATION
Shipping information will be no longer provided with the product since there is no offline installation available. As per
ISI reference 00.00.00202, by the end of 2016, AIRBUS has stopped all Technical Data CD/DVD deliveries. Technical
Data delivery will be online only through AirbusWorld and Airbus Supply (Download and Consultation).In case of any
further queries, open a dossier in TechRequest; Domain: TD Operations Support / Category: TD Distribution.
7. HELP CENTRE
Located on the top right corner of the application the Help Centre provides users with up-to-date FAQs, videos, trainings…
Figure 64 - Accessing Help Centre
X
The airnav Help Centre is divided in two sections:

One dedicated to the end-user

One dedicated to IT and Technical Librarian (for the intranet version).
PAGE 55/56
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.
This Help Centre is also accessible via its direct URL:
https://w3.airbus.com/CRS/A233_Strategic_dev/airnavx/customer/index.html
Figure 65 - Help centre different sections
8. CONTACT US
X
In addition, for any question related to airnav application, open a dossier in TechRequest
X
Domain: Software and Services / Product: airnav / Sub product: My Library or Browser
Customers Services Helpdesk

Telephone no: (Support Level 1 CHINA): +861080475280

Telephone no: ( Support Level 1 All Customers): +33 (0)5 67 19 11 00
(24/7)
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are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of Airbus SAS.
This document and its content shall not be used for any purpose other than that for which it is supplied.