Catia V5 Guidelines
Short Description
Concurrect Engineering, Methods & processes, deployment....
Description
CATIA V5 Methods Guidelines
September 2005 V1.7
DMS 67941
Concurrent Engineering Methods & Processes, Processes, Deployment Deployment - OAM OAMII
Guideline Guidelines s for for Methods Methods - CATIA CATIA V5
Methods & Processes, Deployment Deployment - OAMI: Guidelines for Methods - CATIA V5
Preface 4The
following document provides an overview of the available methods using CATIA V5, and presents a compact guideline to the essential and most important procedures and methods.
4In
this manual, priority is placed on those methods indispensable to the process. The remarks are to be understood as short explanations only.
4For
more detailed information, the User Instructions, AM’s and AP’s referenced in this document are to be consulted.
4This
functionality in this manual has been validated with CATIA V5 R14.
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Contents Title
4
Part Numbering File Management
4 6
4
Part Design
8
4
Sheet Metal Design
9
4
Assembly Design
10
4
Composite Design
13
4
Drawings
16
4
Layers & Colours
19
4
Standard Parts / Airbus Catalog
20
4
Opposite Hand Geometry
22
4
Flexible Components
24
4
‘Made From’ & ‘Drawn On’ Parts
25
4
Working with the Airbus Vault
28
4
Data Quality
31
4
CATDUA V5
36
4
Reference Documents
37
4
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Page
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Part Numbering 4General 4Naming 4Part
Rules
and Numbering should always follow AM2215.
Name = Filename.
4Filenames 4No
AM2215
are always in Uppercase. Uppercase.
spaces are allowed.
4Always 4Never
change part numbers within CATIA V5 using Save Management.
rename or overwrite CATIA documents with UNIX or Windows file managers.
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Part Numbering 4Large
AM5018.6
Components with Sub-Element Parts
4Large
components, such as ribs, skins and spars, can be created as a series of individual sub-element parts, represented in the DMU as a single, linked model.
4Naming 4Final 4
Convention
Model:
M57P5432120000
4Sub-Element 4
Parts:
M57P5432120000-01, -02, -03, etc. Copy with Link
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4PRIMES
3
4On
first vaulting, it is important that the final model and all sub-element parts are vaulted together to maintain issue status. It is recommended recommended that the maximum number of sub-element parts are created created (as empty CATParts) because further iterations cannot be added after this initial vaulting.
4Drawings
are linked to the final model and not the sub-element parts.
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File Management 4Correct
AM5012 / UI186
File Management while Maintaining Links
4The
following method must be followed to ensure that renamed parts, assemblies and drawings update successfully. 4
Open the assembly (or part) required for change.
4
If the assembly has an associated drawing, this must be opened in the same CATIA session for the links to update correctly.
4
Use Save Management to change the assembly and parts filenames.
4
Modify the assembly, part, and instance numbers within Properties. Properties.
4
Save the assembly.
4
Swap CATIA window to the drawing(s) and rename as required. – (The (The asse assemb mbly ly must still be open).
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File Management 4Maintaining 4A
AM2252 / UI227
& Managing UUID Links
UUID is a unique identifier recorded inside all CATIA documents.
4When
CATIA opens a reference document (i.e. sub-assembly) both its name and UUID are checked. If the UUID number has changed it will not open correctly, and any existing links will be broken. This condition can be caused if the original sub-assembly had been deleted and restarted, creating a new UUID number.
4General 4Always
Rules
preserve the original vaulted CATIA document.
4Never
delete and restart an existing CATIA document with File + New, New , File + New From or File + Save as New document. document. This creates a new UUID number.
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4Never 4
overwrite CATIA documents with new versions using UNIX or Windows.
Use File File + Save Save Manag Manageme ement nt / Save Save As to renumber existing CATIA documents. – Keeps Keeps the same UUID number. number. – Maintains assembly and drawing drawing links (User Instruction Instruction 186). 186).
4
Only use File File + New From From to create a new, unique part based on an existing part. – Creates Creates a new UUID UUID numb number. er. – Links Links to existing existing assembli assemblies es and drawing drawings s are not not required.
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Part Design 4General 4Part
Rules
Name = Filename.
4Parts 4Only
are modelled about a local axis system. one PartBody per CATPart. (Exceptional (Exceptional conditions can apply).
4Multi-Model
4PartBody 4Special 4Delete 4Isolate . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
AM2259 / AM5018
links are only permitted to Master Geometry and published elements.
placed on correct Master Model Layer (See Layers & Colours).
characters (i.e.commas) are not allowed as element names.
any redundant wireframe and surface geometry. all non-essential external references.
4Only
the PartBody should be shown. Hide all other geometry.
4Only
approved Material Attributes are allowed.
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Sheet Metal Design 4General
AM2263
Rules
4Sheet
Metal Parts should be created with the following workbenches: Hydro-formed and and Bent Parts Parts. 4 Aerospace Sheet Metal Design (ASL) - Hydro-formed 4
(straight fold line line without joggle). joggle). Generative Sheet Metal Design (GSMD) - Bent Parts only (straight
4
not supported in the sheet sheet metal workbenches. workbenches. Part Design - Unique Parts not
4All
parts should contain both a folded and unfolded solid representation.
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Sheet Metal Part Process Flow with Aerospace Sheet Metal Design
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Assembly Design 4General 4Assembly 4All
AM5012 / UI198
Rules
Name = Assembly Instance Name.x = Filename. Filename.
Parts and Assemblies should have a Product Description Product Description (Properties Menu).
4Parts
or products must only be added or deleted from a sub-assembly when it is open in its own window (at root level).
4Broken
links should be immediately reattached with File + Desk and Edit + Links or by using Replace Component. Component.
4Constraints 4Fix
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are permitted between parts within a single assembly.
all Assembly Components that are not constrained.
4Parts
should not be hidden in the assembly structure.
4Performance
4Only 4
can be improved by configuring the CATIA V5 Search Order (UI243).
use DMU Navigator Cumulative Snap with the Rotation Option.
(Never use the symmetry option).
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Assembly Design 4Design
AM5012 / UI198
Tree
4The
Design Tree is the Designers Working Assembly.
4The
Design Tree number is the first 9-Digits 9-Digits of the Production (14-Digit) Assembly.
4It
can hold Design Principle, SAM, GRM, Frontier, Interface and Installation Assemblies; Zoned Environments and Reference Geometry.
4The
content of the Design Tree is not managed in PRIMES, and as such, the completeness and validity of the environment data should always be checked.
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Assembly Design 4Using
AM2252
Cut / Copy & Paste (Special)
4Copy
+ Paste should be used in preference to Cut. Cut. The original component is deleted after the Copy operation. Example: SUBASSY3 is SUBASSY3 is copied into SUBASSY2 . (Note: Original is deleted after paste).
Paste Special
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As specified in Product Structure
Break Link
Creates a new instance of SUBASSY3
Creates a Copy of SUBASSY3
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Composite Design 4Design
AM5034
Methodology
4Composite
Parts are designed on reference surfaces using wireframe geometry to define the composite entities.
4Composite
4There 4Zone
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are three design methodologies that can be adopted: and Taper
4
Discrete zones of constant thickness and the ramp areas between these zones are designed. Solid and ply creation can be automatically performed.
4
Automatic design method method – recommended for simple components.
4Zone . t n e
Design uses the Composite Part Design Workbench.
and Limit Contour
4
Discrete zones of constant thickness are designed but ramps between zones are not designed. Solid and ply creation require some interaction with the workbench in order to complete definition.
4
SemiSemi-Automatic Automatic design method.
4Ply-by-Ply 4
Each ply contour is individually defined by the designer.
4
Manual design method method – recommended for complex components and sandwich panels.
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Composite Design 4Composite
AM2215
Part Structure Basic Laminate M57110322 010 00
Basic laminate (rough solid) M57110322 010 00 – – CSL00 CSL00
CI
Basic laminate (Engineering plies) M57110322 010 00 – – CD000 CD000
DS
Machined Panel M57110321 200 00
Basic laminate (Manuf (Manuf designed plies) plies) M57110322 010 00 – CM000 – CM000 Ply Shape (Production) M57110322 010 00 – CP000 – CP000
Bonded Panel M57110322 000 00
Stitching M57110322 010 00 – CST00 – CST00 . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
Stiffener M57110322 020 00 CA CATP TPro rodu duct ct
CATP CATPar artt Stiffener (rough solid) M57110322 020 00 – – CSL00 CSL00 …
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Composite Design 4Naming 4A
and Numbering
Top Level assembly is created for the whole panel (as required).
4Each
component in the panel is treated tr eated as an assembly of 5 different different CATParts.
4Composite
Parts are named M57...-C####.
4
The First 14-Digits represent the Part Number.
4
-C#### suffixes the 14-Digit number, with numbers increasing incrementally with each new iteration.
4Part
Extensions
4Solids 4Design . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
AM2215
Data
4Manufacturing 4Production 4Stitching
Data
Data
Data
-CSL##
Solid Model for the DMU
-CD###
Design Plies
-CM### Manufacturing Plies -CP###
Production Plies (flat patterns)
-CST##
Stitching Information (included where required)
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Drawings 4General
AM2264 / AM2255
Rules
4Drawings
are numbere numbered d with the first nine digits digits of the assembly assembly or part number number with a suffix indicating the drawing sheet number -01, 02, etc. (i.e. M57P54321-01).
4One 4All
sheet per CATDrawing. (No limit on the number of detail sheets per drawing).
Drawings should be created with the Airbus Title Block Application .
4Picture
Drawings can be used in specific circumstances. (AM2255). (AM2255).
4Views 4All
views should be locked prior to filing or vaulting.
4View
frames should be turned off prior to vaulting.
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Views should not be pasted across drawings. The section should be generated from a front view which is scaled down, moved off the drawing sheet, and hidden.
4Dimensions 4All
dimensions should be compliant with Airbus ISO Standard. Standard.
4Dimensions
should be fully associative on exact views.
4Dimensions
are not permitted on Isometric Views or picture drawings.
4Avoid
Fake dimensions.
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Drawings 4Drawing 4All
AM2264 / AM2255
Links
drawings should be created with valid links to 14-Digit CATParts/ CATProducts.
4The
only exception to this rule is drawings that include reference geometry, which are generated generated from a 9-digit 9-digit Design Tree Assembly. (See Table). 4
The Design Tree Assembly contains reference geometry, and all views should be only. considered as snapshots only.
4
Before updating any views, it is important that content of the reference geometry in the Design Tree Assembly is validated.
Drawing Type
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14-Digit
Elementary/ Detail Part
P
Definition (Master Geometry)
P
Assembly
P
9-Digit
Frontier
P
Installation
P
Interface
P
Required CATDrawing Links for Drawing Types
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Drawings View Generation / Definition No
Large Assembly Drawing?
Exact-Mode View •Overload Properties •Zone by DMU Section Box •Generative View Styles
Yes
Fillet Radii, Hole-Centres? Hole-Centres?
Yes
Part Feature Driven Dress-up
No
Does View Require All of Assembly? (Filtered Views)
Picture Drawing
AM2264
Yes No
Approximate-Mode Approximate-Mode View •View Quality Options->Mechanica ->Options->Mechanicall Design->Drafting->View Methods & Processes Deployment - OAMI: Guidelines for Methods - CATIA V5
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Layers & Colours 4Rules 4The
AM2232 / UI181
for Layers and Colours
Master Model Layer is applied to the PartBody only. only. (Mandatory)
4Layering
convention as per the Sub Domain Master Model Allocation (Airbus Allocation (Airbus Product Handbook AP 1-018-01).
4In
addition, any entity (Part Body / Geometrical Set) placed on a layer (1-999) will be assigned assigned a colour colour via the Colour By Layer automation tool. Layers Distributed By Master Model 81-109
110
P
Design Principle P
Frontier Model . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
121-245
SAM Model
P
Definition Model
P
Master Geometry
P
Master Lining
P
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Standard Parts 4General
AM5012
Rules
4Fasteners
created with automated assembly techniques should not be included in assemblies and are represented as a point and vector.
4Definition Phase: 4
A & B Maturity Maturity - STD parts are included included only in areas of potential clash or to prove concept.
4
C Maturity - All STD parts are included with the exception of fasteners, which are shown only in areas of potential clash or to prove concept.
4Development 4
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4All
Phase:
All STD parts and applicable fasteners are included.
standard parts should be positioned correctly in assemblies.
4Large
numbers of Standard Parts can be grouped in a component collector node.
4
The first 14-Digits (L57…) use the assembly number.
4
-STD## suffixes the 14-Digit number, increasing increasing incrementally incrementally with each node.
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Standard Parts / Airbus Catalog 4Catalog 4Open
Brower
the Catalog Browser
4Select
AM2369 / UI202
and browse
(1)
for STANDARD_PARTS_CATALOG
the appropriate catalog:
4
Skill Domain Catalogs Catalogs
- AIRBUS_CATALOG.Catalog .
4
Standard Parts Master Catalog
- StandardParts.Catalog.
4
All sub-catalogs can be opened independently.
4Find
the required Part and double-click to double-click to select or MB3 + MB3 + Instantiate Component. Component.
Roughl ghly y 4Rou
position position the the part in the assemb assembly ly and selec selectt OK. OK.
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Opposite Hand Geometry 4Symmetrical 4Create
AM2259 / UI196
Parts
a new right hand part M57P5346620100
.
4Open
in the same session the file of the left hand part M57P5346620000
4Copy
the PartBody from the ...200 part.
4Paste
the PartBody into the
4In
.
...
201 part (Paste Special > AsResultWithLink).
Part Design, use the Symmetry feature in relation to a symmetry symmetry plane.
4Change 4Delete
the default PartBody : Body > Body.2 Object > Change PartBody > OK.
empty Body.1.
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Opposite Hand Geometry 4Symmetrical 4The
AM5012 / UI196
Assemblies
creation of RH Wing data is mandated as a Design Data deliverable.
4It
is the responsibility of the designer to ensure that the opposite hand assembly and parts are always kept up to date.
4The Assembly Design
Insert Symmetry tool must not be used as it does not produce an opposite hand assembly applicable to current Airbus processes.
4Basic
. t n e
Methodology
4
Create the OH Parts using the Symmetrical Part Methodology.
4
Add OH Parts to an OH assembly.
4
Position the OH parts with snap and constraints as necessary. 4 (Please
refer to User Instruction 196 for 196 for part positioning guidelines).
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Flexible Components 4General
components, when deformed, can be located in multiple positions (e.g. Spring).
4Flexible
components are named L57...-FLX L57... -FLX01 01 (-02,-03, etc, then A1-9, B1-9, etc).
4
The first 14-Digits (L57…) always use the parent assembly number.
4
-FLX## suffixes the 14-Digit number, increasing incrementally with each iteration.
4For
iteration of a flexible component must be a separate Part or Assembly.
reference, the Master Part number is added to the Properties Definition field.
4Flexible 4Each
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Rules
4Flexible
4Each
. t n e
AM5012 / UI276
Parts
flexible part must reference a master CATPart.
4Flexible
Assemblies
4The
content content of a flexible flexible assembly assembly is always identical identical to the content of its reference assembly.
4Only
part positions are modified.
Reference
4Warning: Do not use the Flexible Assembly feature.
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‘Made From’ & ‘Drawn On’ Parts 4‘Made
AM2296 / UI251
From’ Parts & Assemblies
4During
the creation of a ‘flying’ ‘flying’ part, several manufacturing manufacturing processes/stage processes/stages s may be required (e.g. billet / forging / extrusion) before the machining machining or formed part is created.
4Each
stage will have a different 9-digit stem number. Manufactured From
Modelled & Drawn
Manufactured From
Modelled & Drawn
Modelled Modelled & Drawn Drawn
Assembly and Drawings
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Billet, Forging, Extrusion L5741234820000
Machined Part L5741234720000
Formed Part L5741234620000 Formed Assembly L5741234500000 Bracket L5791235020000
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‘Made From’ & ‘Drawn On’ Parts 4‘Drawn
AM2296 / UI251
On’ Parts & Assemblies
4These
include items such as fabricated assemblies, where the parts that make up an assembly are separately modelled, but are only detailed on a single drawing sheet.
4The
component parts and assembly drawing have the same 9-Digit stem number.
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Typical BOM – produced in PRIMES 2.0 (similar in PRIMES 3.3.3)
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‘Made From’ & ‘Drawn On’ Parts 4Machining’ 4The
AM2296 / UI251
Made from Casting
machining and casting carry the same 9-Digit stem number.
4The
casting model model is created in PRIMES only and is numbered numbered with a component part number (i.e. ...200 part).
4No
CATPart or drawing exists for a casting.
4The
solid model represents represents the final machined component component as found on the aircraft.
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Typical BOM produced in PRIMES 3.3.3 (similar in PRIMES 2.0)
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Working with the Airbus Vault 4General
UI227 / UI243
Rules
4Assemblies
and parts parts should not be open in CATIA when storing to the vault. vault.
4When
working in an assembly with sub-assemblies, all affected CATProducts must be vaulted in the same session and not at different times. This ensures that all links are synchronised.
4Do
not work on an assembly, then reset the check-out in check-out in the vault and overwrite the assembly with its old version.
4All
CATIA documents, which have a UUID number that is different from the originally vaulted document, document, will be rejected by the PRIMES PDM system.
4Read . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
4Never
Only Areas (ROAs)
attempt to add or delete geometry from a read-only assembly.
4Select
only the minimum number of projects required in the Set Project / wsconfig / wsconfig Tool. Tool. This will improve performance as it reduces the number of CATIA search paths.
4The
SP-Resolved and SP-Resolved and Equipment DLNames Equipment DLNames should be moved to the bottom of the CATIA Search Order to improve performance.
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Working with the Airbus Vault 4Vaulting
(PRIMES 3)
UI194
Design Tree Assemblies
49-Digit
Design Tree assemblies can be vaulted but all Zone and Scenery Components must be deactivated before storing. This is mandatory. mandatory.
4Checking-Out
Design Tree Assemblies
4
From the Windchill Browser select Windchill tab and search for the Design Tree assembly.
4
From the menu select Tools + Transfer. Transfer. The transfer panel appears in the bottom half of the Windchill Browser. Select Checkout & Download. Download.
4
Select the Transfer Tab. Transfer Tab. Enter your password; enter a job name and submit. submit .
4
The batch process will store the assembly in the users active Workspace Browser .
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September 2005 V1.7
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Working with the Airbus Vault 4Vaulting
(PRIMES 3)
UI194
Drawings linked to Design Tree Assemblies
4Drawings
generated from 9-Digit Design Tree assemblies can only be vaulted with a 14-Digit production assembly. (Which uses the same 9-Digit stem number).
4Frontier,
interface, interface, and installation installation drawings - An empty 14-Digit assembly assembly may have to be created and vaulted for this purpose.
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4
Initial Vaulting
1.
From the EPD Data Browser create a CAD doc.
2.
Check-in the Production (14-Digit) CATProduct first. first.
3.
Associated drawings are transferred automatically.
4
Updating
4.
Check-out the Production (14-Digit) CATProduct.
5.
Drawings are checked-out into /epd/parts/. into /epd/parts/.
6.
Repeat steps 2 & 3 for all subsequent vaulting operations.
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September 2005 V1.7
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Data Quality
AM2266
4Q-Checker 4Q-Checker
is a mandatory data quality requirement for CATIA V5 documents.
Q-Checker 4Q-Checker
is ran interactively from the icon icon in the selected CATIA CATIA document: document:
1. From the Main Panel select the applicable Airbus Environment and Environment and the Start icon, or 2. A new option checks and creates creates reports for CATProducts and selected sub-components. 3. Check report results: Erro rror 4 Red Warn Warnin ing g 4 Blue 4 Green
OK
Corr Co rrec ecti tion on is mand ndat ato ory ; mod model el will will be reje ejecte cted. Correc Correctio tion n by user user is reco recomm mmend ended ed but but not not mand mandato atory. ry. No correction required; quality of criterion are OK. 11
33
Activate Q-Checker . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
Analysis Viewer
22
Not Used
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September 2005 V1.7
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Data Quality 4CATPart
Checklist
AM2266
Checked by Q-Checker
CATPart Checklist
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1
Part Name conforms to naming/numbering procedure.
2
Filename an d Part number have same name.
3
Unit length is in mm.
4
Part defined using local axis system.
5
Only one PartBody exists.
6
Relevant reference elements published.
7
Features, Elements and various bodies renamed.
8
All Geometry hidden except for the PartBody. PartBody.
9
No deactivated features.(Except for external references)
10
Unnecessary elements removed.
11
Red Re d colour not used for entities, part bodies.
12
Part updated updated..
13
Layers/Colours (Macro)
14
Part stored to vault as a CATPART type.
15
Airbus standard CATSetting file is used.
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September 2005 V1.7
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Data Quality 4CATProduct Checklist
AM2266
Checked by Q-Checker
CATProduct Checklist 1
Prod Pr oduc uctt Name Name conf confor orms ms to nam namin ing/ g/nu numb mber erin ing g proce procedu dure re
2
Co r r es es po nd en c e be bet w ee n Filename and Product number
3
Airb Ai rbus us Stan Standa dard rd CA CATS TSet etti ting ngs s file file use used d
4
Alll inst Al instan ance ces s of of Prim Primar ary y and and Se Seco cond ndar ary y par parts ts constrained (Optional)
5
Alll ins Al insta tanc nces es ex expl plic icit itly ly re rena name med d
6
Product Stored to vault as a CATPRODUCT type
CATProduct Links Checklist
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1
Reference Element (in External References Open Body) linked, loaded an and d synchronised
2
No Out Of Context or broken links (If present, are they intentional?)
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September 2005 V1.7
Page 33
Data Quality 4CATDrawing Checklist
AM2266
Checked by Q-Checker
CATDrawing Checklist
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1
Drawing Name conforms to naming/numbering procedure.
2
Airbus Drawing Standard used used,,
3
First Angle Projection is used.
4
Only one sheet per CAD drawing.
5
Drawing sheet uses default name.(Sheet.1)
6
Title Block Applic Application ation used.
7
All generative views associated with 3D geometry.
8
All views /Drawing updated updated..
9
No empty views
10
All views Locked.
11
Tolerance as per Airbus ISO std.
12
Font type an d size as per std.(Please refer to AM 2264 Main module).
13
No fake dimensions.
14
All dimensions associative.
15
No dimensions on isometric view.
16
Drawing stored in vault as a CATDRAW type
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September 2005 V1.7
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Data Quality Checklist
AM2266 / UI206
4CATProduct 4The
following checklist should be followed before a 14 digit CATProduct is vaulted:
4
Ensure the assembly has a product description.
4
Delete or correct broken or broken or ghost links. ghost links. (CATDUA can remove these errors if necessary).
4
Check that constraints are valid and up-to-date.
4
Run CA CATD TDUA UA V5 to check and clean the data as necessary.
4CATPart 4The
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following checklist should be followed before a CATPart is vaulted:
4
Ensure the part has a description.
4
The PartBody is placed on the correct layer with the correct colour associated.
4
Delete any redundant wireframe and surface geometry. – Part Part Design/ Design/ GSD workbenc workbench: h: Tools + Delete Useless Elements. Elements. (Take care not not to delete the absolute axis system or any valid isolated geometry when using Delete Useless Elements). Elements).
4
Delete all non-approved Material Attributes.
4
Isolate non-essential external references.
4
Run CA CATD TDUA UA V5 to check and clean the data as necessary.
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September 2005 V1.7
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CATDUA V5 4CATIA
AM2266 / UI206
Data Upward Assistant
4CATDUA
is a utility for ensuring ensuring the integrity integrity of CATIA V5 data. It is primarily used for healing, removing broken and ghost links, resolving update errors, and data cleaning.
4CATDUA
Report Return Codes (P1: Most Severe)
4
Priority 1: Upgrading action may lead to data deletion.
4
Priority 2: Upgrading action may lead to data modification (without deletion).
4
Priority 3: Upgrading action without data deletion or modification (no impact on data).
4Guidelines 4Do . t n e m u c o d y r a t e i r p o r p d n a l a i t n e d i f n o C . d e v r e s e r s t h g i r l l A . D T L K U S U B R I A ©
not overwrite data before validating the results of P1 and P2 errors.
4Only
use the clean option if you are satisfied with the results from fr om the report file.
4CATProducts
should be updated after cleaning.
4Always
check any healed data before vaulting.
4Known
Issues
4CATDUA
should not used on Kinematic and Tubing CATProducts.
4Drawings
using formats larger that A0 will be resized to A0 (Batch Mode).
Methods & Processes Deployment - OAMI: Guidelines for Methods - CATIA V5
September 2005 V1.7
Page 36
Reference Documents 4A-UK 4
UI148
CATIA V5 Update Information and Known Issues
4
UI181
CATIA V5 Colours
4
UI185
Minimising Ghost & Broken Links in CATIA V5
4
UI186
Renumbering CATIA V5 Documents while Maintaining Links
4
UI194
Checking-in CATIA V5 Drawings into PDMfDP
4
UI195
Creating Large Assembly Drawings in CATIA V5
4
UI196
CATIA V5 Symmetrical Parts & Assemblies (Right Hand Wing)
4
UI198
CATIA V5 Assembly Rules (SAM, Design Principles & GRM)
4
UI202
CATIA V5 Standard Parts
4
UI206
CATDUAV5 Utility
4
UI227
Managing CATIAV5 UUID Document Links
4
UI243
CATIA V5 Search Order Process
4
UI251
CATIA V5 ‘Made From’ and ‘Drawn On’ Parts and Assemblies
4
UI276
CATIA V5 Flexible Parts and Assemblies
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User Instructions (UI)
Methods & Processes Deployment - OAMI: Guidelines for Methods - CATIA V5
September 2005 V1.7
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Reference Documents 4Airbus 4
AM2215
Identification of Product Models, Parts and Assemblies
4
AM2232
Layering for Legacy CAD Tools
4
AM2252
CATIA V5 Multi-Model Links
4
AM2255
Picture Drawings with CATIA CATIA V5
4
AM2259
3D Modelling Rules for CATIA V5
4
AM2263
Sheet Metal Part Modelling in CATIA V5
4
AM2264
Drafting with CATIA V5
4
AM2266
Quality Control of CATIA V5 Data by Q-Checker
4
AM2296
PRIMES Methods
4
AM5012
CATIA V5 Assembly Rules
4
AM5018
Machined Part Modelling in CATIA V5
4
AM5034
Composite Parts Modelling with CATIA V5
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Methods (AM)
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This document and all information contained herein is the sole property of AIRBUS UK LTD. 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 UK LTD. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS UK LTD LTD will be pleased to explain the basis thereof.
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