Creating direct engineering document
This page enables you to create a direct engineering document. Tell me more.
Select the “Create Direct Engineering Document” link under the “Engineering Document” business component.
The “Create Engineering Document” page appears.
The system displays the following field:
Date Format |
The format in which the date fields must be entered 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. |
Enter the following fields in the Eng. Doc. Details:
Eng Doc # |
A unique number identifying the engineering document (Alphanumeric, 16). This can be a combination of characters and digits.
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Numbering Type |
Use the drop-down list box to select the numbering type in which the engineering document number must be generated. The system lists all the values defined in the “Create Numbering Type” activity of the “Document Numbering Class” business component for the “Engineering Document” transaction. |
Eng. Doc Category |
Use the drop-down list to select the category to which the engineering document belongs. The system lists all the active quick codes that are of type “Eng. Doc. - Category” as defined in the “Create Quick Codes” activity. Data entry in this field is mandatory if in the “Edit Document Type Attributes” page:
If you do not wish to specify the category, you can leave this field blank. |
Eng. Doc User Status |
Use the drop-down list box to assign a user-defined status for the engineering document. The system lists all the active quick codes that are of type “Eng. Doc. - User Status” as defined in the “Create Quick Codes” activity. If you do not wish to specify the user status, you can leave this field blank. |
Subject |
The textual description of the engineering document (Alphanumeric, 255). Data entry in this field is mandatory, if you do not wish to copy the details from the existing MCR or Engineering Document. |
ATA # |
The ATA chapter on which the engineering document must be executed (Alphanumeric, 16). Mandatory. The ATA chapter number should be in “Active” status in the “Aircraft” business component. Help facility available. |
Eng. Doc Type |
Use the drop-down list box to select the Eng. Doc. Type. The system lists the user defined "Document Types" in “Active” status for the "Eng. Doc Type" in the interacting “Configure Document Attributes” activity of the “Common Master” business component. The system leaves the field blank by default. However, if a default “Eng Doc Type” is set for the selected “Source Doc Type” in the interacting “Common Master” business component, the system considers the Eng. Doc. Type defaulted for the selected Source Doc Type value. Mandatory. |
Exe. Type |
Use the drop-down list box to select the execution type. The valid options are “Major” and “Minor”. The system displays the value “Minor” by default. |
Ref. Doc. Type |
Use the drop-down list box to select the Reference Document type. The system lists the Reference Document Type values of “Active” status as defined in the interacting “Common Master” business component. The system leaves the field blank by default. |
Ref. Doc # |
A number identifying the engineering reference document (Alphanumeric, 40). |
Enter the following in the “Reference Document Details” group box:
Process Ref. # |
The process reference number applicable for a MCR # and Revision # combination (Alphanumeric, 40). Help facility available. |
Process Ref. Date |
The date on which the process reference number was generated.(Date Format). |
MCR # |
The number identifying the Maintenance Change Request (MCR) from which the details must be copied (Alphanumeric, 18). The maintenance change request should have already been defined in the “Create MCR” activity of the “Maintenance Change Request” business component and the status of the MCR should be “Confirm”. Data entry in this field is mandatory, if the “Copy From” field is set to “MCR”. Help facility available. |
Revision # |
The revision number of the MCR. (Alphanumeric, 40). |
Source Doc Type |
Use the drop-down list box to select the type of the modification document or the source document. The system lists all the ‘active’ MCR document types for which the “Applicable For” is set as “Direct Eng Doc” in the interacting “Common Masters” business component. Ensure the following if this field is left blank: The source document type created is valid for the MCR # - Revision # entered in the “Copy Details” group box. |
Note: For a particular Eng. Doc Type, if on creation of an engineering document, the ‘MCR # / Rev #' or 'Source Doc Type' or both are not specified, but are included for “Configured numbering generation”, the system displays an error message.
If you include ‘MCR # / Rev #' or 'Source Doc Type' or both for numbering generation, but specify only one of the values, then the system generates a number based on the given value only. However, if Category is also included for numbering generation, it is mandatory to enter a value in the “Category” field.
Eff. From Date |
The date from which the MCR is effective (Date format). |
Enter the following in the “Copy Details” group box:
Copy From |
Use the drop-down list box to specify whether the details are to be copied from “MCR” or “Engineering Document”. The system leaves the field blank by default. |
Note: If ”MCR” is selected, the system copies the details pertaining to effectivity, concurrent requirements, references, publications affected, tasks, configuration changes, resources, kits, kits composition and periodicity, to the Engineering Document that is being defined. The details are copied from the MCR specified in the “MCR #” field. The system also copies the “Effective From Date” for the MCR number. If the user has entered a value in the “Eff. From Date” field, the system overwrites the value with the copied value. Refer to the topic “Copying details from MCR to Engineering Document” for more information.
Eng. Doc # |
The engineering document number from which the details are to be copied into the engineering document that is currently being defined (Alphanumeric, 30). The engineering document should have already been defined, and the status of the engineering document should be “Released”. The system allows you to selectively copy the main details, tasks, effectivity details, concurrent requirements, reference details, publications changed, configuration changes, periodicity details from the engineering document entered in this field. |
Revision # |
The revision number of the engineering document from which the details must be copied (Alphanumeric, 40). |
Check one or more of the following boxes, to copy the details selectively:
All |
Check this box to copy all the details pertaining to the engineering document.. Details include tasks, parts and kit composition, resources, effectivity, concurrent requirements, references, publications changed, configuration changes, schedule details and aircraft modification details. Note that the Warranty Information would be copied only when the Warranty Coverage is set as “Non-Claimable”. |
Schedule |
Check this box to copy the schedule details. Note that the Warranty Information would be copied only when the Warranty Coverage is set as “Non-Claimable”. |
Main |
Check this box to copy the main details of the engineering document excluding tasks, effectivity, parts and kit composition, resources, effectivity, concurrent requirements, references, publications changed, configuration changes and periodicity. |
Effectivity |
Check this box to copy the effectivity details. |
Tasks |
Check this box to copy tasks. |
Note: The system copies the effectivity details based on the applicability of the engineering document.. |
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Concurrent Requirements |
Check this box to copy the concurrent requirements. |
Publications Changed |
Check this box to copy the publications changed details. |
Reference Details |
Check this box to copy the reference details. |
Configuration Changes |
Check this box to copy the configuration changes. The details are copied in the “Edit Aircraft Configuration Change Information” and “Edit Component Configuration Change Information” pages. |
If the applicability of the Engineering Document is aircraft, component or engine |
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Mod # Effectivity |
Check this box to copy the aircraft modification details. |
Enter the following in the “Other Details” group box:
Applicability |
Use the drop-down list box to specify whether the engineering document is applicable for “Aircraft”, “Engine” or “Component”. By default this field is set to “Aircraft”. |
Priority |
Use the drop-down list box to set the priority for the engineering document. This indicates the level of urgency. For example, in a set of priority descriptions "Critical", "High", "Medium" and "Low", the priority description "Critical" will be treated as of highest priority. The system lists all the priority descriptions defined in the “Create Priority Numbers” activity of the “Common Masters” business component. On selecting the Source Doc Type, the system defaults the Priority field with the value set for the corresponding Source Doc Type in the interacting “Common Master” business component. |
Exe. Action ? |
Use the drop-down list box to select the execution action. The valid options are "Required" and "Not Required". The system displays the value “Required” by default. |
Eng. Doc Type |
Use the drop-down list box to specify the type of the engineering document. The system provides the following options: |
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The system leaves the field blank by default. |
Schedule Type |
Use the drop-down list box to specify whether the engineering document. that needs to be executed on a “One-Time” or “Recurring” or “As Required” or “Perpetual” basis |
The system sets the field to “One-Time” by default. |
Note: The system ensures the Schedule Type is set to “One Time”, if the Eng. Doc. Type Attribute for "Tracking Required" is set to "No" in the interacting “Common Master” business component for the “Eng. Doc. Type”.
Back Ground |
The textual description of the background information such as the prerequisites for the current change (Alphanumeric, 2000). |
Reason
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The textual information detailing the reason for which the engineering document has been created (Alphanumeric, 255). |
Enter the following field in the “Eng. Doc. Execution Details” group box:
Primary Work Center # |
Use the drop-down list box to select the work center where the change has to be performed. The system lists all the work centers that have been defined in the “Create Work Center” activity of the “Work Center” business component. |
The system displays the following field on clicking the “Create Eng. Doc.” pushbutton:
Work Center Description |
The textual description of the work center. |
Enter the following fields:
Est. Elapsed Time |
The total time estimated for completing the Engineering Document (Decimal). Data entry in this field is mandatory, if the estimated elapsed time is not copied from any of the existing MCR or Engineering Document. Use the drop-down list box provided alongside, to specify the unit of measurement for the time allotted for the Engineering Document. The system provides the options “Minutes”, “Hours” and “Days”, and sets the field to “Hours” by default. |
Est. Man Hrs. |
The total man-hours estimated for “Skill” type resources to execute the engineering document (Decimal). Data entry in this field is mandatory, if the estimated man hours is not copied from any of the existing MCR or engineering document. |
On-Wing |
Check this box to indicate that the change can be performed when the part is fitted to the aircraft. |
Direct Execution |
This option is to identify whether to generate work order or not after the release of engineering document. The system sets this option only if “Eng.Doc Type Attribute” for "Tracking Required" is set as "No" in the interacting “Common Master” business component for the selected “Eng.Doc Type”. However, the checkbox is deselected if “Tracking Required” value is set to “Yes”. |
Follow Up Action Reqd. |
Check this box to indicate that follow-up action is required after performing the engineering document. |
Generate PR Automatically |
Check this box to generate the purchase request during the release of the engineering document, for the part specified in the “Plan Material Requirements” page. |
If this box is checked, the system copies the following details to the “Plan Material Requirement” page on clicking the “Create Eng. Doc.” pushbutton: |
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Note: The system calculates the required quantity of parts, by multiplying the number of maintenance objects (maintained by individual maintenance bases) and the quantity identified for each part in the engineering document.
Regularization |
Check this box, if the changes suggested in the engineering document can be complied, while closing the engineering document. Uncheck the box, if the changes suggested in the engineering document can be complied, while closing the work orders. |
Mod Status # |
The modification status number of the engineering document. (Alphanumeric, 15). |
Test Flight Required |
Use the drop-down list box and set the field to “Yes”, if a trial run is required for the aircraft, after the changes are carried out. |
The system displays the following in the “Budgetary Information” group box:
Base Currency |
The base currency defined in the interacting “Organization Set Up” business component. |
Enter the following in the “Budgetary Information” group box:
Part Cost |
The cost of the part (Integer). Ensure that the value entered in this field is positive. |
Resource Cost |
The cost of resource (Integer). Ensure that the value entered in this field is positive. |
Kit Cost |
The cost of kit (Integer). Ensure that the value entered in this field is positive. |
Other Cost |
Any other cost details pertaining to the budgetary information (Integer). Ensure that the value entered in this field is positive. |
Total Cost |
The system displays the Total Cost as the sum of part cost, resource cost, kit cost and other cost, if no value is entered (Integer). Ensure that the value entered in this field is positive. |
Recurring Cost |
The recurring cost incurred for the engineering document (Integer). Ensure that the value entered in this field is positive. |
Budget Remarks |
Any remarks pertaining to the budgetary information (Alphanumeric, 40). |
Enter the following fields in the “Warranty Information” group box:
Warranty Coverage |
Use the drop-down list box to specify the warranty coverage of the Component, Engine or Aircraft The system lists the options “Claimable” or “Non-Claimable”.
By default, the system displays the value “Non-Claimable” on page launch. |
Warranty Applicability |
Indicates the applicability of the warranty. The system provides the following check boxes:
By default, the system leaves all these check boxes unchecked. Ensure that at least one check box is selected, if the “Warranty Coverage” value is selected as "Claimable". |
Warranty Details |
The details of warranty for the Component, Engine or Aircraft (Char 2000). By default, the system displays the blank value on page launch. |
Enter the following fields in the “Weight & Balance Details” group box:
Change in Weight |
The change in the weight of the aircraft after the execution of the engineering document (Decimal). |
Change in Moment |
The change in moment of the aircraft after the execution of the engineering document (Decimal). |
Note: The system retrieves the corresponding parameters UOM for the above fields. The parameters for the aircraft weight and moment are identified in the “Set Base Parameters” activity of the “Aircraft” business component.
Change in Electrical Load |
The change in the electrical load of the aircraft after the execution of the Eng. Doc. (Decimal). |
HAZMAT |
Use the drop-down list box and select "Applicable", if the execution of the engineering document involves working on hazardous materials. Select "Not Applicable" otherwise. The system displays “Not Applicable” by default. |
Additional Information |
The additional information pertaining to the change in the electrical load of the aircraft on execution of the Engineering Document (Alphanumeric, 2000). |
Enter the following field in the “Document Attachment Details” group box:
File Name |
The file name of the document attached to engineering document (Alphanumeric, 30). Help facility available. |
Select the "View File" link to view the file details.
Click the “Create Eng. Doc.” pushbutton to create the engineering document.
The system assigns “Fresh” status to engineering document.
Note: This action is workflow-enabled. Notification messages can be sent as per the settings you have defined in the "Workflow Management" business component.
The system ensures the following:
If “Direct Execution” check box is selected, you must have selected the value as “Required” from the “Exe Action ?” drop-down list box for the Eng. Doc # and Revision # combination.
The system performs the following:
If you have chosen automatic generation of the engineering document number and “Allow Num Type Change” has been set to “Yes”, the system generates the Eng. Doc # based on the Numbering Type selected. However, if the Numbering Type is not selected, the system generates the Eng. Doc # based on the default Numbering Type defined in “Eng. Doc. Type Attributes”.
If you have chosen automatic generation of the engineering document number and “Allow Num Type Change” has been set to “No”, the system generates Eng. Doc # based on the default Numbering Type defined in “Eng. Doc. Type Attributes” irrespective of the value selected by the user.
If you have chosen “Numbering Logic” as “Configured” and “Allow Num Type Change” has been set to “Yes”, the system generates the Eng. Doc # based on the Numbering Type selected in ‘Create Eng Doc ‘ Page. However, if the Numbering Type is not selected, the system generates the Eng. Doc # based on the attributes selected for number generation and the sequence of the numbers as defined in “Eng. Doc. Type Attributes” activity.
If the part identifier is “Internal”, the part number and the serial number details belonging to the part are copied, if they exist in the “Part Administration” business component. If the part identifier is “Supplier”, the system copies all the part numbers whose ‘Other Part Numbers’ are identified for the MCR. For a given other part number, if more than one internal part number exists, the system copies the first part number.
If the “Copy From” is set as “MCR”, the system updates the periodicity details to the engineering document as defined in the “Maintenance Change Request” business component.
The system calculates and updates the compliance date as the earliest date among the schedule dates computed for the date based and usage based work units.
Updates the schedule date and triggering parameter for the work units, based on the date and/or time based schedules defined for the work units. If the schedule date is calculated based on the usage based schedules, then the system considers the threshold value / threshold interval.
The system updates the calculated schedule date and the triggering parameter in the central planning / component pending tray, if the “Direct Execution” is marked as “Yes”.
Copying details from MCR to Engineering Document
General details such as subject, ATA, priority, source doc type, schedule type, background, reason, estimated elapsed time, estimated man-hours and applicability, are copied from the MCR specified in the “MCR #” and “Revision #” fields.
Effectivity Details |
The effectivity details are copied, based on the applicability of the engineering document. |
Model and Aircraft Effectivity |
The models and the tab numbers belonging to the models are copied only if they exist in the “Active” status in the “Aircraft” business component. |
Part and Serial Effectivity |
The part number and the serial number details are copied. The system copies all the 'active' parts identified in the MCR. |
Conditional Effectivity |
Conditional effectivity is copied depending on the conditional effectivity filters. For example, if the conditional effectivity filter is defined as “Parameter flight hours greater than 500”, all the models and the aircrafts or components with flight hours greater than 500, are copied. |
Concurrent Requirements |
The system copies the Engineering Documents that are already identified as concurrent requirements for the MCR in the “Edit Concurrent Requirement Information” page of the “Create MCR” activity of the “Maintenance Change Request” business component. |
Task Details |
The details of the task, such as description, time UOM, estimated elapsed time, estimated man-hours, access panels, work area and zone information, piece parts, resources, sub tasks, notes and document references are copied to the Engineering Document. |
If the tasks in MCR are defined in the “Maintenance Task” business component, the system copies the details from the same and updates the “Task Classifier” as “Existing”.
If the tasks in MCR are not defined in the “Maintenance Task” business component, the system copies the details from the “Maintenance Change Request” business component and updates the “Task Classifier” as “New”.
Note: Only “Improvised” or “New” tasks can be modified in this page. You cannot modify the tasks with the “Task Classifier” set as “Existing”.
Configuration Change details |
The configuration change details are copied in the “Edit Aircraft Configuration Change Information” and “Edit Component Configuration Change Information” pages. If the part identifier is “Internal”, the system copies the existing parts and the new parts as defined in the “Part Administration” business component. If the part identifier is “Vendor”, the system copies the existing parts and the new parts as defined in the “Maintain Other Part Nos” activity of the “Part Administration” business component. |
If the Engineering Document is applicable for aircraft, component or engine,
The system checks the availability of the existing part in the aircraft configuration or component configuration for which the Engineering Document is applicable. If available, the system copies the respective level code, position code, corresponding part serial number, NHA and corresponding new part against each aircraft or component.
For parts of type “Piece Part”, the position codes are not copied.
The resource and the tool requirement details are copied to the “Edit Resource Requirement” page.
The kits and the kit composition details specified in “MCR” are copied to the “Edit Part Requirements” and “Edit Kit Part Details” pages.
The Net Change in Weight, Net Change in Moment and the Change in Electrical Load details specified in “MCR” are copied to the Change in Weight, Change in Moment and Change in Electrical Load fields respectively.
The reference documents, publications affected and periodicity details are copied to the “Edit References Information”, “Edit Publications Changed” and “Edit Schedule Information” pages for the Engineering Document.
The system displays the following field:
Link info |
Indicates whether task, aircraft effectivity, part effectivity, concurrent requirement, reference information, affected publication, configuration change, confirm new part, material plan and periodicity details are entered for the engineering document. The system displays one of the following: |
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To proceed, carry out the following:
Select the “Edit Aircraft Effectivity” link at the bottom of the page to enter the aircraft effectivity details for the Engineering Document.
Refer to the topic “Entering aircraft effectivity for Engineering Document – An overview” for more details.
Select the “Edit Part Number Effectivity” link at the bottom of the page to modify the part effectivity details of the Engineering Document.
Refer to the topic “Entering part effectivity for Engineering Document – An overview” for more details.
Select the “Edit Aircraft Mod # Effectivity” link at the bottom of the page to record the details of modification done to the aircraft.
Select the “Edit Task Details” link at the bottom of the page to modify the details of the tasks to be performed for Engineering Document execution.
Refer to the topic “Modifying Engineering Document task information – An overview” for more details.
Select the “Edit Schedule information” link at the bottom of the page to modify the periodicity details for the Engineering Document.
Refer to the topic “Entering schedule details for Engineering Document – An overview” for more details.
Select the “Initialize Eng. Doc. Schedules” link at the bottom of the page to initialize engineering schedules.
Select the “Edit Configuration Change Details” link at the bottom of the page to enter the configuration change information for the Engineering Document.
Refer to the topic “Entering configuration changes due to Eng. Doc. execution – An overview” for more details.
Select the “Confirm New Parts Requirements” link at the bottom of the page to specify the new parts that are required for executing the Engineering Document.
Refer to the topic “Confirming New Part Requirements for Engineering Document – An overview” for more details.
Select the “Plan Material Requirements” link at the bottom of the page to specify the parts for which the purchase request must be generated.
Refer to the topic “Entering material requirements for Engineering Document – An overview” for more details.
Select the “Edit MCR Reference Details” link at the bottom of the page to modify MCR reference details.
Select the “Edit Notes” link at the bottom of the page to modify the additional notes for the engineering document.
Select the “Edit Reference Details” link at the bottom of the page to specify the reference documents that are needed for executing the Engineering Document.
Refer to the topic “Modifying Engineering Document task information – An overview” for more details.
Select the “Edit Publications Changed” link at the bottom of the page to enter the publications affected because of the Engineering Document execution
Refer to the topic “Entering publications affected details for Engineering Document – An overview” for more details.
Select the “Edit Eng. Doc” link at the bottom of the page to modify the engineering document.
Refer to the topic “Selecting engineering document for modification – An overview” for more details.
Select the “Release Eng. Doc.” link at the bottom of the page to release the engineering document.
Select the “Upload Documents” link at the bottom of the page to upload documents.
Refer to the topic “Object Attachments” online help for more details.
Select the “View Associated Doc. Attachments” at the bottom of the page to view information regarding the associated document attachments.
Refer to the topic “Object Attachments” online help for more details.
Select the “View MCR Reference Details” link at the bottom of the page to view maintenance change request.
Creating direct engineering document – An overview
This page enables you to create a direct engineering document. A unique number identifies the engineering document. Based on the option settings, the system generates the engineering document number automatically, or enables you to enter it manually, or generates based on predefined attributes (Configured).
You can specify the category to which the engineering document belongs, user status, description and the ATA chapter, to indicate the system on which the engineering change must be performed.
Reference document details such as the Modification Committee Meeting (MCM) number, date on which the MCM took place, Maintenance Change Request (MCR) number, revision number of the MCR and the source document type can be specified.
You can also provide a reference to the engineering document or MCR that is already defined, and copy the details such as the tasks, effectivity, concurrent requirement, references, publications affected, configuration changes, and periodicity.
You can specify whether the engineering document is applicable for the aircraft, component or the engine, and the priority and type of the engineering document. You can indicate whether the engineering document should be executed on one-time or recurring basis.
The execution details of the engineering document, such as the work center in which the engineering document has to be performed, estimated time and man-hours required for the execution of the engineering document must be defined.
You can also indicate whether,
the engineering change has to be performed in the original place of the part,
follow-up action is required after executing the engineering document,
the work order is to be generated after the release of engineering document
the planning can be done while releasing the engineering document
purchase request must be generated for the parts required for executing the engineering document.
You can record the change in weight, moment and the electrical load after executing the engineering document.
The system assigns the “Fresh” status as soon as the engineering document is created, and sets the creation date and time to the server date and time.
Specify the reference document details
Create engineering document applicable for aircraft, engine or component
Set the priority for engineering document
Identify the type of engineering document
Identify the work center fore engineering document
Specify engineering document execution details
Create work order directly from engineering document
Generate PR automatically for an engineering document
Enter the weight and balance details
Copy details from an existing engineering document
Specify the applicability of working on hazardous materials
Specify the reference document details
The details of the reference document that triggered the creation of engineering document can be entered.
Enter the MCR number and the corresponding revision number in the “MCR #” and “Revision #” fields.
Select the appropriate source document type in the “Source Doc Type” drop-down list box.
Create Engineering Document applicable for aircraft, engine or component
You can create an engineering document applicable for aircraft, engine or component.
Set the “Applicability” field to “Aircraft” if the engineering document must be executed on aircraft.
Set the “Applicability” field to “Engine” if the engineering document must be executed on engine.
Set the “Applicability” field to “Component” if the engineering document must be executed on component.
Set the priority for engineering document
Priority is a number identifying the level of urgency. For example, in a set of priority descriptions "Critical", "High", "Medium" and "Low", the priority description "Critical" will be treated as of highest priority. You can specify the priority based on which the Engineering Document will be executed.
Set the “Priority” drop-down list box to the priority that you wish to assign to the engineering document.
Identify the type of engineering document
Based on their purpose, Engineering Documents can be classified under the following types: Replacement, Retrofitment, Task Improvisation, Task schedule related and Informative.
Set the “Eng.Doc Class” drop-down list box to “Replacement”, to indicate that the Engineering Document is generated for replacement of part.
Set the “Eng.Doc Class” drop-down list box to “Retrofitment”, to indicate that the Engineering Document c is generated for servicing the existing part.
Set the “Eng.Doc Class” drop-down list box to “Task Improvisation”, to indicate that the Engineering Document c is generated for revising the existing task details.
Set the “Eng.Doc Class” drop-down list box to “Task Schedule Related”, to indicate that the Engineering Document is generated for changing the schedule details of the task.
Set the “Eng.Doc Class” drop-down list box to “Informative”, to indicate that the Engineering Document is informational and need not be executed.
Identify the work center for engineering document
The primary work center that is responsible for engineering document execution can be identified.
Select the primary work center in the “Primary Work Center #” drop-down list box.
Specify engineering document execution details
You can specify the following details based on which engineering document execution will take place:
Check the “On-Wing” box in the “Eng Doc Execution Details” group box, if you wish to perform the engineering change when the part is fitted to the aircraft.
Check the “Follow-Up Action Reqd” box in the “Eng Doc Execution Details” group box, to indicate that follow-up action is required after executing the Eng Doc.
Create work document directly from engineering document
You can create a work order directly from an emergency Eng Doc.
Check the "Direct Execution" box in the "Eng Doc Execution Details" group box, if you wish to create a work order directly from Engineering Document.
Generate PR automatically for an engineering document
The system can automatically generate a purchase request for the parts required for an engineering document.
Check the “Generate PR Automatically” box in the “Eng Doc Details” group box, if you wish to generate PR automatically for the parts required for the Engineering Document.
Enter the weight and balance details
The change in weight and balance details after the engineering document execution, can be entered.
Enter the change in weight, moment and electrical load, in the “Weight & Balance Details” group box.
Copy details from an existing engineering document
You can copy details from MCRs or engineering documents that are already defined. Details such as the tasks, periodicity, effectivity, concurrent requirements, affected publications, reference documents and the configuration changes can be copied.
Select “Engineering Document” in the “Copy From” drop-down list box, to copy the details from an Engineering Document that is already defined.
Select “MCR” in the “Copy From” drop-down list box, to copy the details from an MCR that is already defined.
Enter the number of the engineering document in the “Eng. Doc #” field.
Enter the revision number of the engineering document to be copied.
Check one or more of the boxes “All”, “Periodicity”, “Main”, “Effectivity” “Tasks”, ”Concurrent Requirements”, “Publications Changed”, ”Reference Details” and “Configuration Changes”, to specify the details to be copied.
Click “Create Eng Doc” pushbutton to copy the details.
A new engineering document is created with the copied details.
Specify the applicability of working on hazardous materials
You can specify whether the execution of the engineering document involves working on hazardous materials.
Set the “HAZMAT” drop-down list box field to "Applicable", to indicate that the execution of the engineering document involves working on hazardous materials. Else set the field to “Not Applicable”.