IMPORTANT |
If you are a student, it is extremely important that you set up and work within your own site to maintain your data integrity. If you work within any other site, you will compromise your own exercise data as well as the data of other students. Predictable exercise results require that your data be isolated in your own site |
Note: Throughout this document, please replace any occurrences of XX with your initials, group ID, user ID or other unique prefix, in order to separate your training data from that of other students.
Purpose: The purpose of this exercise is to verify that the VIM serial structure template definition is ready to be transferred.
Windows:
Serial Structure Template
Purpose: The purpose of this exercise is to verify whether alternative part definitions exist for installed components.
Windows:
Template Alternates
Template Part Number | Installed Part Number | Alternate Part Number | Interchangeability Description |
XX_ENG | XX_C | XX_C_ALT1 | Two way interchangeable |
Note: If you have not had these alternate definitions already set in VIM, you still can continue the transfer process.
Purpose: The purpose of this exercise is to verify whether modification definitions exist in VIM.
Windows:
Affected Parts
Modification Code | Modification Part Number | Affected Part Number |
XX_100 | XX_ENG | XX_A |
XX_100 | XX_ENG | XX_A13 |
XX_200 | XX_C | XX_C |
Note: If you have not had these modification definitions already set in VIM, you still can continue the transfer process and may transfer the modification definition separately.
Purpose: The purpose of this exercise is to create a new revision of assembly and disassembly structures and to transfer the modifications information.
Windows:
Template Part
Part
Transfer Template Structure
Inventory Parts
Product Structure
Modification Repair Code
You have to transfer XX_ENG Engine structure all levels from IFS/VIM
serial structure template definitions to IFS/Manufacturing. You have already had
these template structures defined in IFS/Vehicle Information Management. In
order for these structures to be available for use in the MRO Manufacturing
site for assembly and disassembly orders you need to prepare the transfer and
then confirm the transfer to your site.
Data to create allocations and operations is not present in IFS/VIM and
would only be used by shop orders. Therefore you need to transfer modification
details defined
for parts XX_ENG and XX_C in IFS/VIM to IFS Manufacturing. Then you can associate repair codes
with modifications to point out the allocations and operations needed to do the work.
You have the VIM serial structure template with alternates and modifications already defined in IFS/VIM. You need to prepare these structures for transfer to IFS Manufacturing and creating position parts.
Structure Level | Structure Address | (Actual) Part Number | Part Revision | Part Description | Position Part No |
+ .1 | TEMPLATE | XX_ENG | * | Engine, Jet Turbine | PP/XX_ENG |
+ ..2 | 100 | XX_A | * | Module A, Fan | PP/XX_A |
+ ...3 | 103 | XX_A1 | * | EMU, Fan | PP/XX_A1 |
+ ....4 | 105 | XX_A11 | * | Fan Blade | PP/XX_A11 |
+ ....4 | 106 | XX_A12 | * | Shaft | PP/XX_A12 |
+ ....4 | 107 | XX_A13 | * | Hub | PP/XX_A13 |
+ ...3 | 104 | XX_A2 | * | EMU, Compressor | PP/XX_A2 |
+ ..2 | 101 | XX_B | * | Module B, Combustion | PP/XX_B |
+ ..2 | 102 | XX_C | * | Module C, Turbine | PP/XX_C |
The above table shows the position part number created during the prepare transfer process, using the format: Transfer Prefix + Delimiter + Catalog Number (CSN).
Transfer all levels of the XX_ENG Engine structure to your site.
Errors, warnings and information messages are created when transferring the structure from the holding table to a manufacturing site. You have to verify whether the transfer was successful or not. If there are problems on transfer you have to resolve them.
Site | Transfer Result | Position Part No | Transfer Phase In Date | Transfer Date | Evaluation Session Id |
XX90 | Success | PP/XX_ENG | Today's site date (system date) |
Today's site date (system date) |
A unique number |
Verifying assembly and disassembly product structures.
Level | Part No | Component Part | Qty Per Assembly |
1 | XX_ENG | PP/XX_ENG | 1 |
2 | XX_A | PP/XX_A | 1 |
3 | XX_A1 | PP/XX_A1 | 1 |
3 | XX_A11 | PP/XX_A11 | 4 |
3 | XX_A12 | PP/XX_A12 | 1 |
3 | XX_A13 | PP/XX_A13 | 1 |
2 | XX_B | PP/XX_B | 1 |
2 | XX_C | PP/XX_C | 1 |
2 | XX_C_ALT1 | PP/XX_C_ALT1 | 1 |
Verify that your actual engineering parts are transferred to your site.
The actual inventory part records for prime/installed parts:
Site | Part No | Part Description | Inventory U/M | Planner | Part Type |
XX90 | XX_ENG | Engine, Jet Turbine | PCS | As defined | Manufactured |
XX90 | XX_A | Module A, Fan | PCS | As defined | Manufactured |
XX90 | XX_A1 | EMU, Fan | PCS | As defined | Manufactured |
XX90 | XX_A11 | Fan Blade | PCS | As defined | Manufactured |
XX90 | XX_A12 | Shaft | PCS | As defined | Manufactured |
XX90 | XX_A13 | Hub | PCS | As defined | Manufactured |
XX90 | XX_A2 | EMU, Compressor | PCS | As defined | Manufactured |
XX90 | XX_B | Module B, Combustion | PCS | As defined | Manufactured |
XX90 | XX_C | Module C, Turbine | PCS | As defined | Manufactured |
The actual inventory part records for alternate parts:
Site Part No Part Description Inventory U/M Planner Part Type XX90 XX_C_ALT1 Module C, Alternate Turbine PCS As defined Manufactured
Verifying Modification Transfer Result.