Viewing maintenance information of part

This page allows you to view the details of the selected part. Tell me more.

Select the “View Part Information” link at the bottom of the “Select Part” page.

The “View Maintenance Info. for Part” page appears.

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

Part #	The part selected in the main page for which the details are to be viewed.
Click the hyperlinked part number to view the part information.
Status	The status of the part, which could be “Active” or “Inactive”.
Part Description	The textual description of the part.
Base Part #	The base part to which the selected part belongs.
Mod Status #	The modified part number (dash number) or the engineering order reference number due to which the part has been changed.
Component ID Generation	The mode in which the component ids are generated. The system displays “Auto” or “Manual”.
Component ID Numbering Type	The numbering type based on which component ID is generated.

The system displays the following details in the “Part Classification Details” group box:

Component Family #	The component family to which the part belongs.
Component Type	The component type to which the part belongs, which can be “Engine”, “APU”, “Landing Gears” or “Others”
Part Classification	The classification of the part, which can be “Rotables”, “Repairables” or “Controllables”. Leave this field blank if you wish to retrieve details of all parts irrespective of their classification.
ATA #	The ATA chapter to which the part belongs.
Config. Control Basis	The basis for attachment of the part during component replacement/aircraft maintenance, which could be Config. Rules or Part Effectivity. By default, the system displays Config. Control Basis as Part Effectivity, if this attribute has not been defined for the aircraft/model yet.
LLP?	Indicates whether the part has a definite lifetime. Displays “Yes”, if the part has a preset life and “No”, if the part is not a component. Note: LLP is the acronym for Life Limited Part.
Maintenance Process	The maintenance process of the part, which could be one of the following: “Hard-Time” – Indicates that the maintenance needs to be performed so that the items are restored to a suitable condition within a fixed period, such as number of cycles, landings or calendar time. “On-Condition” – Indicates that the maintenance needs to be performed such that the items are inspected or tested at specific periods to an appropriate standard in order to determine whether they can continue in service. It is not a philosophy of “use until failure”. “Condition Monitored” – Indicates that the maintenance needs to be performed such that the items remain in service until a functional failure occurs and the overall reliability is monitored by analysis and surveillance programs, such as “Built-In Test Equipment” (BITE).
Replacement Type	The type of replacement that the part can undergo. The replacement type could be one of the following: LRU – Indicates the part can be replaced in the “Line Replacement Unit”. The part can be replaced in the aircraft itself. SRU – Indicates the part can be replaced in the “Shop Replacement Unit”. The part has to be taken to the shop for replacement.
PMA?	Indicates whether the part can be sourced from manufacturers other than OEM (Original Equipment Manufacturer). Note: PMA is the acronym for Part Manufacturer Approval.
OEM Part #	The part # of the part as allotted by the original equipment manufacturer (OEM), Mandatory. Note: This field is displayed only if you have selected “Yes” in the “PMA?” drop-down list box.
DER?	Indicates whether modifications to the part as maintained by DER are approved by the regulatory authorities Note: DER is the acronym for Design Engineering Requirement.
Cargo	If this box appears checked, it indicates that the part can be fitted in a cargo aircraft.
RVSM	If this box appears checked, it indicates that the part can be fitted in aircraft that can fly at a height lesser than the reduced vertical separation minimum limit.
MEL	If this box appears checked, it indicates that the selected part is a part of the minimum equipment list of an aircraft.
ETOPS	If this box appears checked, it indicates that the selected part is a part of ETOPS (Extended Twin Operations Performance).-
Lifed?	The system displays “Yes” if the part has a specific lifetime. Else the system displays “No”.

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

Planning Base	The organizational unit in which the part details were defined.
Default Maint Base	The organizational unit in which the maintenance activities of the part can be carried out.
Default Work Center #	The default work center in which the maintenance activities of the part can be carried out.
Work Center Description	The textual description of the work center
Planner Code	The code of employee who plans the maintenance activities of the part.
Planner Name	The name of the planner.
Std. Repair Task #	The standard repair task, such as Refurbishment or Bushing to be automatically added to a SWO for the part.
Execution Facility	The location where the part can be repaired. The system displays one of the following: “In-house” – Indicates that the part can be repaired in the operator’s shop. “Outsource” – Indicates that the part can be repaired in the third party's location such as authorized repair shop of the supplier. “In-house & Outsource” – Indicates that the part can be repaired in the operator’s shop or in the third party’s location. “None” – Indicates the part can be repaired at multiple locations.
Preferred Repair Agency	The preferred repair agency in which the part is repaired.
Phase-Out Policy	The policy based on which the part can be phased out. The phase-out policy could be any one of the following options: “Not Permitted” – Indicates that the phasing out of part is not allowed. “All Work Centers” – Indicates that the part can be phased out in all the work centers. “Specific Work Centers” – Indicates that the part can be phased out only in specific work centers.
Lower Landing Minimum	The system displays the lower landing minimum of the part.
SOS Applicability	The system displays “Yes” if the part has the SOS applicability. Else the system displays “No”.
Default Exec. Doc for Int. Repair Routing	The system displays the default execution document required for internal repair routing.
TAT(Days)	The time required for the execution of the maintenance program on the part. Note: TAT is the acronym for Turn Around Time.
Consolidate Exec. Order?	Indicates whether multiple maintenance tasks for the part can be merged into a single execution document, such as shop work order. A “Yes” in this field implies a shop work order for the part can comprise many tasks, while a “No” disallows shop work orders from executing more than one task.

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

Lead Parameter	The consumption parameter that has been identified as the lead parameter, for its importance in determining the life of the part.
Average Daily Utilization	The average daily utilization of the lead parameter based on which the maintenance activity is forecasted.

Select the “Effectivity Details” tab to view the aircraft effectivity details.
Select the “Phase Out Restrictions” tab to view the phase out restriction details for the part.

The system displays the following details in the “Part Supplier Details” group box:

Supplier #	The code identifying the supplier of the part.
Supplier Name	The name of the supplier.
OEM Name	The name of the original manufacturer.
Per Asset Value	The cost of the part per unit.

The system displays the following details in the “User Defined Details” group box:

User Defined Detail – 1	Any additional information about the part pertaining to the maintenance activities.
User Defined Detail – 2	Any additional information about the part pertaining to the maintenance activities.
User Defined Detail – 3	Any additional information about the part pertaining to the maintenance activities.
Component Detail – 1	The quick code of type “Component Detail – 1”.
Component Detail – 2	The quick code of type “Component Detail – 2”.
Component Detail – 3	The quick code of type “Component Detail – 3”.

To proceed, carry out the following:

Select the “View Technical & Attribute Parameters” link at the bottom of the page to view the technical and attribute parameters of the part.
Select the “View Consumption & Range Parameters” link at the bottom of the page to view the consumption and range parameters of the part.
Select the “View Part Configuration” link at the bottom of the page to view the part configuration details.
Select the “View Warranty Details” link at the bottom of the page to view the warranty agreement details.

Viewing maintenance information of part– An overview

The following details of the part are displayed:

The details that uniquely identify the part such as its number, description and status. The base part number, along with the mode of component ID generation are also displayed.
The component family to which the part is associated. The component type and ATA chapter to which the part belongs, is displayed along with the details regarding the component category to which the part belongs. The various component categories are:
- Cargo - Indicates that the part can be fitted only in cargo aircraft.
- RVSM - Indicates that the part can be fitted to aircraft that can fly at a height lesser than the minimum vertical separation limit of the aircraft.
- MEL - Indicates that the part belongs to the minimum equipment list of the aircraft.
The administrative details of the part such as the planning base, maintenance base in which the maintenance activities of the part can be carried out and the planner who plans the maintenance activities.
The usage of the part along with the lead parameter and the average daily utilization.
The vendor details such as the supplier, the original equipment manufacturer and the per unit cost of the part.
Indicates whether multiple maintenance tasks for a part can be consoliated and executed through a single shop work order.