Viewing conditional effectivity for the MCR
This page allows you to view the conditional effectivity details for the MCR. Tell me more
Select the “View Conditional Effectivity” link at the bottom of the “View Maintenance Change Request” page.
The “View Conditional Effectivity” page appears.
The system displays the following fields in the “MCR Details” group box:
MCR # |
The number identifying the MCR for which the conditional effectivity details are displayed. |
Revision # |
The revision number of the MCR. |
Subject |
The textual description of the MCR. |
Source Doc Type |
The type of the source document to which the MCR belongs. |
The system displays the following fields in the “Component Effectivity” group box:
On-Wing |
If this checkbox is selected, it indicates that the MCR execution can take place when the component is fitted to the aircraft. |
Inventoried |
If this checkbox is selected, it indicates that the MCR execution can take place only when the component is not fitted to the aircraft. |
The system displays the following fields in the “Parameter Details” multiline:
Parameter |
The code identifying the consumption parameter. |
Parameter Description |
The textual description of the consumption parameter. |
UOM |
The unit of measurement for the consumption parameter. |
Relational Operator |
The relational operator that calculates the permissible range of values that the consumption parameter can take. The system displays one of the following: |
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Parameter Value |
The value of the consumption parameter. |
The system displays the following field:
Other Conditions |
Any other condition pertaining to the execution of MCR. |
Viewing conditional effectivity for the MCR - An overview
This page allows you to view the conditional effectivity details for the MCR.
The execution of MCR might depend on certain conditions that are defined as conditional effectivity in the “Create MCR” activity. For example, there may be a condition that the MCR can be executed only when the aircraft flight hours exceed 10,000. Such conditions are displayed in this page.
You can view the details such as whether the MCR execution must be performed when the component is fitted to the aircraft (In-Situ) or not (Inventoried). The consumption parameter that determines the condition for MCR execution, the parameter description, and the relational operator to calculate the permissible range of values that the consumption parameter can take and the value of the parameter are displayed in the multiline. If there are any other conditions specified for the execution of the MCR, you can view those details in this page.