Unit of competency Outline
Date retreived
22/07/2026 10:51 PM AWST
22/07/2026 10:51 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.
Remove and install avionic system components
Remove and install avionic system components
Unit of competency
National Code
MEA343B
MEA343B
State Code
D4462
D4462
TGA Status
Replaced
Replaced
DTWD Status
Replaced
Replaced
State Implementation and Classification
Approved Date
10/05/2012
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
10/05/2012
Nominal Hours
40
Description
This unit of competency is part of the B1 Mechanical Aircraft Maintenance Engineer licensing pathway under CASR Part 66, in accordance with the licensing provisions in Section 3, Assessment Guidelines. It covers the competencies required for the removal and installation of avionic system components and certification of tasks where system serviceability can be verified without the use of specialist off-aircraft test equipment.
Notes
Elements and Performance Criteria
1. Remove avionic system components
- 1.1 System is rendered safe and prepared in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety
- 1.2 Avionic component removal is carried out in accordance with the applicable maintenance manual
- 1.3 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
- 1.4 Removed components are tagged and packaged in accordance with specified procedures
2. Install avionic system components and verify system serviceability
- 2.1 Avionic components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life
- 2.2 Installation of avionic components is performed in accordance with the applicable maintenance manual and regulatory requirements
- 2.3 System is reinstated to correct operational condition and is tested for serviceability
- 2.4 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures and regulatory requirements
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 scope of this unit is restricted to removing and installing avionic components from systems whose serviceability can be established and certified through the use of built-in test equipment or any other on-board system that can verify correct system operation. The use of off-aircraft test equipment is limited to items that provide a simple go/no go decision
Application
Application of this unit may relate to:
scheduled or unscheduled maintenance
individual or team-related activities
Procedures and requirements
Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise
Avionic components
Avionic components include:
components/line replaceable units from electronic instrument systems
components/line replaceable units from engine indication systems
communication system components
navigation system components
software updates to avionic systems where serviceability can be determined by a simple test
Tested for serviceability
Tested for serviceability means:
confirming system serviceability through the operation of built-in test equipment or any other on-board system that can confirm correct operation
using only off-aircraft test equipment that provides a simple go/no go decision regarding system serviceability
Note
The scope of this unit is restricted to removing and installing avionic components from systems whose serviceability can be established and certified through the use of built-in test equipment or any other on-board system that can verify correct system operation. The use of off-aircraft test equipment is limited to items that provide a simple go/no go decision
Application
Application of this unit may relate to:
scheduled or unscheduled maintenance
individual or team-related activities
Procedures and requirements
Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise
Avionic components
Avionic components include:
components/line replaceable units from electronic instrument systems
components/line replaceable units from engine indication systems
communication system components
navigation system components
software updates to avionic systems where serviceability can be determined by a simple test
Tested for serviceability
Tested for serviceability means:
confirming system serviceability through the operation of built-in test equipment or any other on-board system that can confirm correct operation
using only off-aircraft test equipment that provides a simple go/no go decision regarding system serviceability
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 remove and install avionic components and verify system serviceability through the use of built-in test equipment or similar on-board systems and/or off-aircraft test equipment that provides a simple go/no go decision while observing all relevant safety and component handling precautions.
Critical aspects for assessment and evidence required to demonstrate competency in this unit
It is essential that cleanliness requirements and safety precautions applicable to the system being maintained are fully observed, understood and complied with, as well as work practices associated with electrostatic sensitive devices.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This is to be demonstrated by application across a range of aircraft avionic system components as listed in the Range Statement. An understanding of the attachment methods, connection of hardware, and system test requirements as they relate to the work must be demonstrated before undertaking any action.
The work plan should take account of applicable safety and quality requirements in accordance with the industry and regulatory standards. 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 routine supervision on a representative range of avionic components, as 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 workplace or simulated workplace using tools and equipment specified in 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
Overview of assessment
A person who demonstrates competency in this unit must be able to remove and install avionic components and verify system serviceability through the use of built-in test equipment or similar on-board systems and/or off-aircraft test equipment that provides a simple go/no go decision while observing all relevant safety and component handling precautions.
Critical aspects for assessment and evidence required to demonstrate competency in this unit
It is essential that cleanliness requirements and safety precautions applicable to the system being maintained are fully observed, understood and complied with, as well as work practices associated with electrostatic sensitive devices.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This is to be demonstrated by application across a range of aircraft avionic system components as listed in the Range Statement. An understanding of the attachment methods, connection of hardware, and system test requirements as they relate to the work must be demonstrated before undertaking any action.
The work plan should take account of applicable safety and quality requirements in accordance with the industry and regulatory standards. 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 routine supervision on a representative range of avionic components, as 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 workplace or simulated workplace using tools and equipment specified in 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
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| W8441 | MEA343A | Remove and install avionic system components | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| AUE67 | MEA343 | Remove and install avionic system components | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| S748 | MEA40710 | Certificate IV in Aeroskills (Mechanical) | Qualification |
| S754 | MEA50210 | Diploma of Aeroskills (Mechanical) | Qualification |
| D751 | MEA50211 | Diploma of Aeroskills (Mechanical) | Qualification |