Viewing MCR details

This page allows you to view the details of the MCR selected in the “Selection of Maintenance Change Request” page . Tell me more

Select the hyperlinked MCR number in the multiline of the "Select Maintenance Change Request" page.

The “View Maintenance Change Request ” page appears.

The system displays the following field:

Date Format

The format in which the date field is displayed in this page. This format is displayed from the "User Preferences" business component based on the login user id. In case the format is not defined, the system displays the date format from the "Enterprise Modeling" business component by default.

The system displays the following fields in the “MCR Identification Details” group box:

MCR #	The number identifying the MCR number for which the details must be viewed.
Revision #	The revision number of the MCR.
Subject	The textual description of the MCR.
Status	The status of the MCR, or the MCR and revision number combination, for which the details are to be viewed. The system displays one of the following:
	Fresh – When the MCR is created.
	Confirmed - When the MCR is confirmed.
	Revised – When the MCR is revised.
	Processed – When the MCR is processed into Engineering document in the “Engineering Document” business component.
Issue Date	The date on which the MCR is issued.
Receipt Date	The date on which the MCR is received into the airline operator’s records.
Eff. From Date	The level at which the From Date is effective which could be ‘Eng. Doc. Level’ or ‘Maint. Obj. Level’.
	The date from which the maintenance change request is effective.
User Status	The user status of the MCR.
Reason for Revision	The reason for the revision of MCR.
External Ref. #	The reference assigned to the MCR based on the external source document, such as SB or AD.

The system displays the following fields in the “MCR Details” group box:

Applicability	The applicability of the MCR which could be “Aircraft” or “Engine” or “Component”.
MCR Class	The nature of execution of the MCR.
Effectivity Type	The type of the effectivity of MCR.
	Direct – Indicates that the execution of the MCR is not bound by any condition.
	Conditional – Indicates that the execution of the MCR is bound by specific conditions. The conditions are specified in the “Edit Conditional Effectivity” page.
Part Identifier	The identifier of the part as defined in the “Create Maintenance Change Request” activity, which could be one of the following:
	Internal – Indicates that the MCR must be executed on the part that is available with the operator and is defined in the "Part Administration" component.
	Supplier – Indicates that the MCR must be executed on the part supplied by the supplier. This part can be new or already defined as an alternate part in the "Part Administration" business component.
ATA #	The ATA chapter number on which the MCR must be executed.
Reason Category	The user-defined reason category of the MCR.
Reason	The reason for the issue of the MCR.
Back Ground	The textual description of the conditions that led to the issue of the MCR.
Consequences	The consequences that may result on the execution of the MCR.
Action	The actual action or change that must be performed as recommended in the MCR.
Terminating MCR	The system displays either “Yes” or “No” to indicate whether the current MCR terminates one or more existing MCRs:
Mandatory?	Indicates whether the issue of the MCR is mandatory or not.
Reliability Impact?	Indicates whether the MCR has reliability impact or not.
Impact Assessment?	Indicates whether the engineering change will affect / upgrade the component, such as Not Required and Required.
User Defined 1	A user-defined value for the MCR.
User Defined 2	A user-defined value for the MCR.
User Defined 3	Additional details on the MCR.
User Defined 4	Additional details on the MCR.

The system displays the following fields in the “Source Document Details” group box:

Manufacturer #

The code of the manufacturer who issued the MCR (Alphanumeric, 45). Ensure the following while entering this field:

The manufacturer is defined as a supplier of the supplier class "Manufacturer" in the "Supplier" business component if the option "Allow Supplier as Manufacturer Reference" field is set as "Yes" in the "Set Purchase Options" activity of the "Logistics Common Master" business component

The manufacturer is defined in the "Create Manufacturer Information" activity of the "Aircraft" business component if the option "Allow Supplier as Manufacturer Reference" field is set as "No" in the "Set Purchase Options" activity of the "Logistics Common Master" business component.

Help facility available.

Manufacturer Name	The name of the manufacturer who issued the MCR (Alphanumeric, 80).
Approval Authority	The name of the regulatory authority who issued or approved the MCR.
Source	The source from where the MCR is released which could be “Internal” or “External”.
Source Doc Type	The type of the source document to which the MCR belongs.

The system displays the following fields in the “Execution Details” group box:

Est. Elapsed Time

The total time estimated for the execution of MCR.

The time unit is displayed alongside.

Est. Man Hrs.

The total man-hours estimated for the execution of MCR.

Priority

The description of the priority set for the MCR.

The system displays the following fields in the “Warranty Information” group box:

Warranty Coverage

The warranty coverage of the “component”, “Engine” or “Aircraft”, which could be either “Claimable” or “Non-Claimable”.

Warranty Details

The warranty details pertaining to the “Component”, “Engine” or “Aircraft.

Warranty Applicability

Indicates the applicability of the warranty. The warranty applicability could be for any one of the following options:

“Material” – Indicates that the warranty claim is applicable for the material.
“Labor” – Indicates that the warranty claim is applicable for the labor.
“Facilities” – Indicates that the warranty claim is applicable for the facility.
“Miscellaneous” – Indicates that the warranty claim is applicable for options other that “Material”, “Labor” and “Facilities”.

The system displays the following fields in the “Contact Details” group box:

Source Category	The category to which the source that issued the MCR belongs.
Reg. Authority’s Address	The address of the regulatory authority who issued / approved the MCR.
Manufacturer Address	The address of the OEM or the supplier who issued the MCR.
Contact Person	The name of the person responsible for the MCR issued by the OEM / Supplier / Regulatory authority.
Work Phone #	The phone number of the contact person.
Email	The email ID of the contact person.

The system displays the following fields in the “Model Effectivity” multiline:

Aircraft Model #	The number identifying the aircraft model on which the MCR must be executed.
Reference Date Basis	The Reference Date basis for the effective from date of the Aircraft Model which could be “Induction Date”, “Operational Date” or “Manufactured Date”.
Eff. From Date	The date from which the Aircraft Model # is effective.

Note: The “Reference Date Basis’ and ‘Eff. From Date’ fields appear only if the ‘Eff. From Date’ is at “Maint. Obj. Level”.

Manufacturer #	The manufacturer of the aircraft.
Model Description	The textual description of the aircraft model.

The system displays the following field in the "Document Attachment Details" group box:

File Name

The file name of the source document.

The system displays the following field:

Link Info	Indicates whether aircraft effectivity, part effectivity, conditional effectivity, regulatory directive details, compliance, concurrent requirement, reference information, affected publication, task, configuration change, weight and balance, kit requirement, new tool requirement, resource requirement details, customer list, notes and aircraft modification details are recorded, and documents uploaded for the MCR. The system displays the following:
	Ac Eff – If aircraft effectivity details are available.
	Part Eff – if part effectivity details are available.
	Cond Eff – if conditional effectivity details are available.
	Dir – if regulatory directive information is available.
	Compl – if compliance details are available.
	Concurr – if concurrent requirements details are available.
	Ref – if references information is available.
	Pub – if affected publications details are available
	Tsk – if task information is available.
	Cnfg –if configuration change information is available.
	Wt & Bal – if weight & balance information is available.
	Kit – if kits requirement information is available.
	Res – if resource requirement details are available.
	New Tool – if tools requirement information is available.
	Cust – if customer list is available.
	Notes – if notes details are available.
	File Att – if documents are attached to the MCR.
	Mod Eff – if aircraft modification details are available.
	Emp – If an employee has been assigned to the MCR #
	Adv Prt EFF – if advanced part effectivity has been recorded for the MCR #.
	If more than one of the above indicators is applicable for the MCR, they are separated by “\”.

The system displays the following fields in the “Record Statistics” group box:

Created by	The name of the user who created the MCR.
Created Date	The date on which the MCR was created.
Last Modified by	The name of the user who last modified the MCR.
Last Modified Date	The date on which the MCR was last modified.
Confirmed by	The name of the user who confirmed the MCR.
Confirmed Date	The date on which the MCR was confirmed.
Comments	Any remark or comment pertaining to the MCR.

To proceed, carry out the following

Select the “View Recommended Aircraft Effectivity” link at the bottom of the page to view the aircraft effectivity details of the MCR.
Select the “View Recommended Part Effectivity” link at the bottom of the page to view the part effectivity details of the MCR.
Select the “View Conditional Effectivity” link at the bottom of the page to view the conditional effectivity details of the MCR.
Select the “View Task Information” link at the bottom of the page to view the details of the tasks to be performed for MCR execution.
Select the “View Schedule Details” link at the bottom of the page to view the compliance details of MCR.
Select the “View Configuration Changes” link at the bottom of the page to view the configuration change information for the MCR.
Select the “View Concurrent Requirements” link at the bottom of the page to view the concurrent requirement details of the MCR.
Select the “View Weight & Balance Details ” link at the bottom of the page to view the weight and balance details of MCR.
Select the “View Kit Information” link at the bottom of the page to view the kit requirement details of the MCR.
Select the “View Resource Requirements” link at the bottom of the page to view the resources required for MCR execution.
Select the “View New Tooling Requirements” link at the bottom of the page to view the new resource requirement details of the MCR.
Select the “View Customer List” link at the bottom of the page to view the customer list.
Select the “View Reference Details” link at the bottom of the page to view the reference documents that are needed for executing the MCR.
Select the “View Regulatory Directive Details” link at the bottom of the page to view the directive details of the MCR.
Select the “View Publications Affected” link at the bottom of the page to view the publications affected as a result of the MCR execution.
Select the “View Notes” link at the bottom of the page to view the general notes pertaining to MCR.
Select the “View MCR Processing Details” link at the bottom of the page to view the MCR processing details.
Select the “Upload Documents” link at the bottom of the page to attach documents with the change request.
Select the “View Associated Doc. Attachments” link at the bottom of the page to view documents associated with the change request.
Select the “View Aircraft Mod # Effectivity” link at the bottom of the page to record the details of modification done to the aircraft.
Select the "Edit Advanced Part Effectivity" link at the bottom of the page to view enhanced part effectivity details for MCR. See Process Parameter dependency

Note: The Edit Advanced Part Effectivity page and the Edit Recommended Part Effectivity page are mutually exclusive of each other. The value set for the process parameter ‘Enable Advanced Part Effectivity for MCR?’ under the entity type Eng. Doc. Type and the entity All Eng. Doc in the Define Process Entities activity of Common Master will decide which of the two links is available in the Create Maintenance Change Request, Edit Maintenance Change Request, Revise Maintenance Change Request and View Advanced Part Effectivity pages. The following table illustrates the condition in which the links will appear in the aforesaid pages. Further, the Edit Advanced Part Effectivity page, if accessed from the View Advanced Part Effectivity page will be a display-only page with no active pushbuttons.

Refer to "Engineering Document" online help for more details.

Select the “Manage Task Part MOD Details” link at the bottom of the page to update details of part modification driven by the engineering documents (SBs & ADs).

Note: The “Manage Task Part MOD Details” page will appear in the Display-only mode.

Viewing MCR details – An overview

This page allows you to view the details of the MCR selected in the “Selection of Maintenance Change Request” page. You can view the MCR identification details such as MCR number, revision number of the MCR (if any), subject, user status, issue date and receipt date. The other details such as the applicability of the MCR, effectivity type, part identifier, the nature of execution of MCR, the ATA chapter number, priority, reason, background details, consequences, and the action to be performed can be viewed.

You can also view the details of the source document, such as the name of the original equipment manufacturer, the regulatory authority, source that issued the MCR and the type of the source document. The execution details such as the estimated time and man-hours required for the execution of the MCR are also displayed. In this page, you can view the contact information such as the source category, OEM address, name, phone number and email ID of the contact person responsible for the MCR.

The details of the aircraft models for which the MCR is applicable can also be viewed in this page.