Viewing engineering document details

This page allows you to view the details of the engineering document that is already created. Tell me more.

Select the “View Eng. Doc. Information” link at the bottom of the “Select Engineering Document” page.

The “View Engineering Document” 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 “Eng. Doc. Details” group box:

Eng. Doc #	The number identifying the engineering document, for which the details are displayed.
Status	The status of the engineering document, which could be one of the following:
	"Fresh" – When the engineering document is created
	"Cancelled" – When the engineering document is cancelled
	"Revised" – When the engineering document is revised
	"Released" – When the engineering document is released for execution
	"Closed" – When the engineering document is closed
Revision #	The revision number of the engineering document, that helps in tracking the changes made to the engineering document.
User Status	The user-defined status of the engineering document.
Subject	The description of the engineering document.
ATA #	The number identifying the ATA chapter on which the engineering document must be executed.

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

Applicability	Indicates whether the engineering document is applicable on an “Aircraft”, “Engine” or a “Component”.
Priority	The priority assigned to the engineering document.
Eng. Doc Class	The Engineering Document Class.. The system displays one of the following:
	"Replacement" – indicates that the engineering document is generated for part replacement.
	"Retrofitment" – indicates that the engineering document is generated for servicing the existing part.
	"Task Improvisation" – indicates that the engineering document is generated for revising the existing task details.
	"Task Schedule Related" – indicates that the engineering document is generated for changing the schedule details of the task.
	"Informative" – indicates that the engineering document is informational.
Schedule Type	The schedule type for the engineering document compliance. The system displays one of the following:
	"One Time" – indicates that the engineering document must be executed only once.
	"Repetitive" – indicates that the engineering document must be executed at repeated intervals.
Eng Doc Category	The category to which the engineering document belongs.
Action on Rev. Effectivity	Indicates the option for copying the aircraft or component effectivity details of the engineering document from the previous revision to the new revision number. The options could be “Re-Comply”, “Carryover Compliance”, "Revoke” or "None".
Back Ground	The textual description of the conditions that led to the creation of the engineering document.
Reason	The textual information, detailing the reason for which the engineering document has been created.

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

Work Center #

The work center in which the engineering document will be executed.

Work Center Description

The textual description of the work center.

Est. Elapsed Time

The total time estimated for completing the engineering document.

The unit of measurement for the estimated time, which could be “Minutes”, “Hours” or “Days”, is displayed alongside.

Est. Man Hrs.	The total man-hours estimated for “Skill” type of resources to complete the engineering document.
On-Wing	The system displays “Yes” or “No”, to indicate whether the change can be performed when the part is fitted to the aircraft.
Follow Up Action Reqd.	The system displays “Yes” or “No”, to indicate whether the follow-up action is required or not after performing the engineering document.
Test Flight Required	The system displays “Yes” or “No”, to indicate whether the testing is required for the flight, after the engineering changes have been carried out.
Generate PR Automatically	The system displays “Yes” or “No”, to indicate whether the purchase request must be generated automatically for the part specified in the “Plan Material Requirements” page, during the release of the engineering document.
Mod Status #	The number identifying the mod status.
Direct execution	Indicates that the work order can be directly created from engineering document.
Regularization	The system displays “Yes”, to indicate that the changes suggested in the engineering document can be complied, while closing the engineering document. The system displays “No”, to indicate that the changes suggested in the engineering document can be complied, while closing the work orders.
Pre – Load ?	Indicates whether the engineering document is a pre-loaded engineering document. The system displays “Yes” or No”.

The system displays the following in the “Budgetary Information” group box;

Base Currency	The base currency applicable for the budgetary information.
Part Cost	The cost of the part.
Resource Cost	The cost of resource.
Kit Cost	The cost of kit.
Other Cost	Any other cost details as recorded in the budgetary information.
Total Cost	The total cost incurred against the engineering document.
Recurring Cost	The recurring cost incurred for the engineering document.
Budget Remarks	Any remarks pertaining to the budgetary information.

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

Warranty Coverage

The warranty coverage of the Component, Engine or Aircraft, which may be “Claimable” or “Non-Claimable”.

The system displays the value saved for the “Engineering Document #” and “Revision #” combination on page launch.

Warranty Applicability

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

"Material" – This box would be checked if the warranty claim is applicable for the Material.
"Labour" – This box would be checked if the warranty claim is applicable for the Labour.
"Facilities" – This box would be checked if the warranty claim is applicable for the Facility.
"Miscellaneous" – This box would be checked if the warranty claim is applicable for options other than Material, Labour and Facilities.

The system displays the value saved for the “Eng. Doc #” and “Revision #” combination on page launch.

Warranty Details

The details of warranty for the Component, Engine or Aircraft.

The system displays the value saved for the “Eng. Doc #” and “Revision #” combination on page launch.

The system displays 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.
Change in Moment	The change in the moment of the aircraft after the execution of the engineering document.

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 engineering document.

HAZMAT

The system displays one of the following:

"Applicable" – Indicates that the execution of the engineering document involves working on hazardous materials.
"Not Applicable" – Indicates that the execution of the engineering document does not involve working on hazardous materials.

Additional Information

The additional information pertaining to the change in the electrical load after execution of the engineering document.

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

Process Ref. #	The number identifying the modification committee meeting (MCM) in which the change request was processed.
Process Ref. Date	The date on which the MCM took place.
MCR #	The number identifying the maintenance change request (MCR), from which the engineering document is generated.
Revision #	The revision number of the MCR.
Parent engineering document #	The number identifying the parent engineering document of the current engineering document.
Parent Revision #	The revision number of the parent engineering document.
Applicability Group #	The applicability group of the MCR.
Source Doc Type	The type of the modification document or the source document.
Eff. from date	The date from which the MCR is effective.

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

File Name

The name of the file that is attached to engineering document.

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

Cancellation Comments	Any comment pertaining to the cancellation of the engineering document
Release Comments	Any comment pertaining to the release of the engineering document
Closing Comments	Any comment pertaining to the closing of the engineering document

The system displays the following field in the “Link Info” group box:

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:
	"Tsk" – if task details are available.
	"Ac Eff" – If aircraft effectivity details are available.
	"Part Eff" – if part effectivity details are available.
	"Concurr" – if concurrent requirements details are available.
	"Ref" – if references information is available.
	"Pub" – if affected publications details are available.
	"Cnfg" –if configuration change information is available.
	"CnfPrt" – if confirm new part details are available.
	"PlnMtl" – if material requirement details are available.
	"Prd" – if periodicity details are available.
	"N" - if notes are available.
	"Mod Eff" – if aircraft modification details are available.

To proceed, carry out the following

Select the “View Aircraft Effectivity” link at the bottom of the page to view the aircraft effectivity details for the engineering document.
Select the “View Part No Effectivity” link at the bottom of the page to view the part effectivity details of the engineering document.
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 “View Task Details” link at the bottom of the page to view the details of the tasks to be performed for engineering document execution.
Select the “View Schedule Information” link at the bottom of the page to view the periodicity details for the engineering document.
Select the “View Configuration Change Information” link at the bottom of the page to view the configuration change information for the engineering document.
Select the “View New Part Requirements” link at the bottom of the page to view the new parts that are required for executing the engineering document.
Select the “View Material Procurement Plan” link at the bottom of the page to view the parts for which the purchase request must be generated.
Select the “View Eng. Notes” link at the bottom of the page to view the notes entered for the engineering document.
Select the “View References Information” link at the bottom of the page to view the reference documents that are needed for executing the engineering document.
Select the “View Publications Changed” link at the bottom of the page to view the publications that are affected due to the engineering document.
Select the “Track Maintenance Compliance History” link at the bottom of the page to retrieve compliance details.
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.

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

Created by	The name of the user who created the engineering document.
Created Date	The date on which the engineering document was created.
Last Modified by	The name of the user who last modified the engineering document.
Last Modified Date	The date on which the engineering document was last modified.
Released by	The name of the user who released the engineering document.
Release Date	The date on which the engineering document was released.

Viewing engineering document details – An overview

This page allows you to view the details of the engineering document that is already created. Details such as Engineering document number, status, revision number, user status, description of the engineering document, ATA chapter on which the engineering document must be executed, are displayed. The applicability of the engineering document, priority assigned to the engineering document, Eng. Doc Class, schedule type, background information and the reason for engineering document creation are also displayed.

You can view the engineering document execution details such as the work center in which the engineering document will be executed, its description, the total time and man-hours estimated for engineering document execution and the physical mark on the component after the execution of engineering document. You can perceive whether,

the engineering change can be performed when the part is fitted to the aircraft
follow-up action is required after engineering document execution
testing is required for the flight, after the engineering change has been carried out

The change in the weight, moment and the electrical load of the aircraft after the engineering document execution, is displayed. Reference document details such as the modification committee meeting (MCM) number, the date on which the meeting was conducted, the MCR number and the revision number of the MCR are displayed. If the current engineering document is created from an existing engineering document, the number of the parent engineering document is displayed along with its revision number. The comments pertaining to the cancellation, release or closing of the engineering document are also displayed.

You can also view the Budgetary Information pertaining to the engineering document like Part Cost, Resource Cost, Kit Cost, Other Cost, Total Cost and Recurring Cost, if any.