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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 S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.
The same wizard is used to edit the invariant selection.
If the manual is loaded, the second step is displayed with the invariant selected in the
manual tree.
Otherwise the second step is displayed with the external reference.
4.2.1.2.5 View Document Unit
This pane is displayed if the user selects a document unit element in the tree view
A DU (Documentary Unit) (also called a solution) is a granule of information with a
technical content and effectivity relative to technical and operational criteria.
This is the smallest piece of information in a manual. A Document Unit is an XML
document.
If the “func-code” of the DU is not empty, it prefixes the DU title.
If a DU has no current effectivity but has a scheduled one then it is marked as Pre/post
SB DU. The scheduled effectivity will be loaded by the application and displayed in the
metadata tab.
All action modifying the Pre/post SB DU is possible.
It is possible to copy/paste, move, check-out, check-in, delete a Pre/post SB DU.
It shall be possible to copy/paste, delete an element containing the Pre/post SB DU.
The Pre/post effectivity cannot be modified via the “Effectivity” panel of the invariant.
4.2.1.2.5.1 View DU Metadata
The metadata tab displays the metadata of the document unit. The following
information is displayed:
Column Name Description
Code This field contains the solution code
Title This is the DU title.
« Flight Ops Doc
Manager »
User Guide
Reference: UG0600624
Issue: 7.1
PAGE 127/276
© AIRBUS S.A.S 2009. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS S.A.S. 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 S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.
Type
This is the type of solution:
DSC = DU Description
PAB = DU Abnormal Procedure
CDL = CDL Item
DIS = Dispatch Item
PEM = Emergency Procedure
BFR = Function Recovery Procedure
LIM = Limitation
MFA = Malfunction Assessment
BNP = Normal Procedure
POP= Ops Procedure
BPF = Performance
BEY = Proc synthesis
DWR = Weighing Report
Actual effectivity: List of MSN for this solution
Scheduled effectivity
Associated with this solution
Customized
Contains “Yes” if the document unit has been edited by someone,
otherwise: “No”
Last check-in
date
Date of the last check-in performed on this solution
Last check-in
author
Author of the last check-in performed on this document
Status
DU lifecycle status: Possible values: “In creation”, “Released”
Date status
Date when the solution status has been modified.
Content revision
date
Revision date of the DU, this is the date when the DU has been
integrated in a released version of the DU. This value can be
initialized by Airbus or by Flight Ops Doc Manager when creating
AI R manual.
For DU never released, the default value is 15.12.2005.
Content previous
revision date
Previous revision date of the DU, this is the previous date when
the DU has been integrated in a released version of the DU.
This value can be initialized by Airbus or by Flight Ops Doc
Manager when creating AI R-1 manual.
For DU never released, the default value is 15.12.2005.
Metadata revision
date Date when the solution metadata has been modified.
« Flight Ops Doc
Manager »
User Guide
Reference: UG0600624
Issue: 7.1
PAGE 128/276
© AIRBUS S.A.S 2009. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS S.A.S. 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 S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.
Metadata previous
　
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