Unit of competency Outline

Date retreived
23/07/2026 6:22 PM AWST

Whilst all efforts are made to provide accurate and timely information from the relevant source/documentation, please be aware that the information supplied may not be the most current version. The accuracy of the detail has not been confirmed by the Department and therefore should not be relied upon without first confirming the contents.

Perform basic repair of aircraft internal fittings during line maintenance

Perform basic repair of aircraft internal fittings during line maintenance

Unit of competency
National Code
MEA418A
State Code
W8466
TGA Status
Replaced
DTWD Status
Replaced
Current Release Number
2.00
Current Release Date
23/01/2012
State Implementation and Classification
Approved Date
08/05/2012
Field of Education
031599 - Aerospace Engineering And Technology, N.e.c.
Original Release Date
08/05/2012
Nominal Hours
40
Description
This unit covers the competencies required to repair aircraft internal fittings that are within the privileges of the Aircraft Maintenance Engineer A Licence. It is one of the units required for the granting of the chosen Aircraft Maintenance Engineer A Licence under CASR Part 66, in accordance with the licensing provisions in Section 3, Assessment Guidelines.
Notes
Elements and Performance Criteria
1. Prepare to perform routine repairs and minor modifications to aircraft internal fittings
  • 1.1. Applicable repair scheme is determined in accordance with applicable maintenance publications and enterprise procedures
  • 1.2. All required materials and equipment are selected and organised in accordance with enterprise procedures and maintenance publications
2. Perform routine repairs to aircraft internal fittings
  • 2.1. Sheetmetal repairs and non-metallic material repairs are performed in accordance with approved repair scheme, ensuring that aircraft standard practices are used and standard process requirements are carried out
  • 2.2. Work area is cleaned of all waste material
  • 2.3. Adjustments are made, where necessary, for components to operate within prescribed specifications
3. Complete routine repair activities
  • 3.1. Required documentation is accurately completed and correctly processed in accordance with enterprise procedures
The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance. Bold italicised wording, if used in the performance criteria, is detailed below. Essential operating conditions that may be present with training and assessment (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) may also be included.
Note
The Range Statements below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide
Repairs
Sheetmetal repairs may include:
1. Removing corrosion by chemical and mechanical methods
2. Restoring protective coatings to repaired areas
3. Freehand precision hole generation
4. Removing and installing fastening devices
5. Routine repairs to sheetmetal internal fittings
Non-metallic material repairs may include:
6. Repairs to fibreglass, sandwich honeycomb, nylon, perspex, nomex core materials and matrix resins
7. Restoring protective coatings to repaired areas
8. Freehand precision hole generation
9. Removing and installing fastening devices
Application
Application of this unit may relate to:
scheduled or unscheduled maintenance activities
repair of metallic or non-metallic interior fittings, including interior trim panels (sidewalls, galleys, toilets, roof panels, floor panels), overhead lockers, cargo lining and internal doors that are not part of the aircraft pressure hull
Procedures and requirements
Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise
The Evidence Guide provides advice on assessment and must be read in conjunction with the performance criteria, required skills and knowledge, range statement and the Assessment Guidelines for the Training Package.
Overview of assessment
A person who demonstrates competency in this unit must be able to apply hand skills and use maintenance publications to repair aircraft internal fittings made from sheet metal and non-metallic materials while applying all relevant safety precautions.
Critical aspects for assessment and evidence required to demonstrate competency in this unit
The underlying skills inherent in this unit should be transferable into other areas that require similar techniques. It is essential that procedures take into account all safety precautions and quality requirements, standards and practices, and processes associated with repair and assembly.
Evidence of knowledge about enterprise procedures relating to basic repair techniques and the use of the standard repair manual/practices in a range of different routine repair situations will be necessary to supplement evidence of ability to plan and undertake internal fitting repairs.
A person cannot be assessed as competent until it can be demonstrated to the satisfaction of the workplace assessor that the relevant elements of the unit of competency are being achieved under supervision but without intervention on a representative range of tasks involving Groups 1 to 9 listed in the Range Statement. This shall be established via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry Evidence Guide.
Context of and specific resources for assessment
Competency should be assessed in the work environment, using tools and equipment specified by aircraft maintenance manuals. It is also expected that general purpose tools, test and ground support equipment found in most routine situations would be used where appropriate.
Method of assessment

Guidance information for assessment
Replaced By
State Code National Code Title Type
AUE46 MEA418 Perform basic repair of aircraft internal fittings during line maintenance Unit of competency