Viewing configuration change information for engineering document

This page allow you to execution might affect the configuration of the aircraft or the component. Tell me more.

Select the “View Configuration Change Information” link at the bottom of the “View Engineering Document” page.

The “View Configuration Change Information” page appears.

The system displays the following field in the “Eng. Doc. Details” group box:

Eng. Doc #	The engineering document for which the configuration change details are displayed.
Revision #	The revision number of the engineering document.
Subject	The textual description of the engineering document.
MCR Part Identifier	The MCR identifier of the part, which could be “Internal” or “Supplier”.
Update Model / Part Configuration	Indicates whether the engineering change should update the model and the part configuration. The system displays one of the following options:
	Not Applicable – indicates that configuration need not be updated.
	After Release – indicates that the configuration must be updated after the release of the engineering document.
	After Execution – indicates that the configuration must be updated after the execution of the engineering document.
Base Line?	Indicate that the engineering change should update the baselined configuration.

The system displays the following fields in the “Configuration Change Details” multiline:

Existing Part #	The part that must be replaced.
Part Description	The textual description of the part.
MCR Part #	The part number identified in the “Edit Configuration Change Information” page of the “Create MCR” activity.
UOM	The unit of measurement for the part.
Quantity	The number of parts that must be changed.
Part Type	The type of the part as defined in the “Part Administration” business component.
New Part #	The part number that will replace the existing part.
New Part Description	The textual description of the new part.
Quantity	The number of parts that will replace the existing parts.
Recommended Use	The action recommended for the part that is replaced. The system displays one of the following:
	Discard – indicates that the part can be discarded.
	Rework – indicates that the part can be reworked.
	Others – indicates that the part can be kept for other uses.
Interchangeability	The interchangeability rule defined for the part. The system displays one of the following:
	One Way – indicates that the part numbers are not interchangeable in the same position code. For example, if the part number “P2” has replaced part “P1” in the position code “PC1”, then “P1” cannot replace the part “P2” subsequently in the same position code.
	Two Way – indicates that the part numbers are interchangeable in the same position code. For example, the part numbers “P1” and “P2” can replace each other in the same position code subsequently.
	None – indicates that the existing part cannot be replaced by the new part.

To proceed, carry out the following

Select the “View Model Configuration Change Details” link at the bottom of the page to view the model configuration changes.
Select the “View Aircraft Configuration Change Details” link at the bottom of the page to view the aircraft configuration changes.
Select the “View Part Configuration Change Details” link at the bottom of the page to view the part configuration changes.
Select the “View Component Configuration Change Details” link at the bottom of the page to view the component configuration changes.
Select the “View Part Description” link at the bottom of the page to view the part details.

Viewing configuration change information for engineering document – An overview

The engineering document execution might affect the configuration of the aircraft or the component. This change in configuration might result in the change of the part number itself, resulting in a new part number, change in the interchangeability rules for a particular position in the aircraft or component, addition of a new position code, etc.

The configuration change details such as the part number that must be changed, the recommended action for the changed part number and the number of parts that must be changed, are displayed in the multiline. The new part number, its description, number of parts that would replace the previous parts and the part interchangeability are also displayed.

The details of the level numbers at which the existing part must be changed, can be viewed for the model, aircraft, part and component configurations, in the “View Model Configuration Change Information”, “View Aircraft Configuration Change Information”, “View Part Configuration Change Information” and “View Component Configuration Change Information” pages.