Unit of competency Outline
Date retreived
22/07/2026 6:03 AM AWST
22/07/2026 6:03 AM 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 engines and engine system components
Remove and install engines and engine system components
Unit of competency
National Code
MEA306C
MEA306C
State Code
D4421
D4421
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
60
Description
This unit of competency is part of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathway. It covers the competencies required for the removal and installation of both fixed and rotary wing aircraft engines and engine system components. The unit is used in workplaces that operate under the airworthiness regulatory systems of the ADF and CASA.Where a CASA licensing outcome is sought this unit forms part of the CASA requirement for the granting of the chosen Aircraft Maintenance Engineer Licence under CASR Part 66, in accordance with the licensing provisions in Section 3, Assessment Guidelines.
Notes
Elements and Performance Criteria
1. Remove engine
- 1.1. Aircraft is prepared and supported and rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure the safety of personnel and freedom from damage during engine removal
- 1.2. Removal is carried out in accordance with the applicable maintenance manual
- 1.3. Engine is tagged and prepared for transport or storage in accordance with the specified procedures
- 1.4. Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
2. Remove engine system components
- 2.1. Aircraft and/or engine system is prepared and rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure the safety of personnel
- 2.2. Removal is carried out in accordance with the applicable maintenance manual
- 2.3. Engine system component is tagged and prepared for transport or storage in accordance with the specified procedures
- 2.4. Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
3. Install engine
- 3.1. Engine to be installed is checked to confirm correct part or model numbers, modification status and serviceability
- 3.2. Installation is carried out in accordance with the applicable maintenance manual
- 3.3. Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage
- 3.4 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
4. Install engine system components
- 4.1. Engine components to be installed are checked to confirm correct part or model numbers, modification status and serviceability
- 4.2. Installation is carried out in accordance with the applicable maintenance manual
- 4.3. Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage
- 4.4. Required maintenance documentation is completed and processed in accordance with standard 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
Range statements listed below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide
Engines and engine system components:
Engines and engine system components may include:
1. Engine change unit or auxiliary power unit (turbo-prop, turbofan, turboshaft, turbojet and piston)
2. Fuel, oil and air system (or induction and super/turbo charger systems in the case of piston engine) components
3. Engine control system components
4. Ignition or igniter system components
5. Starting system components
6. Fire protection system components
7. Accessories and associated drives
Application
Application of this unit may relate to:
scheduled or unscheduled maintenance activities
individual or team-related activities
Procedures and requirements
Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise
Note
Range statements listed below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide
Engines and engine system components:
Engines and engine system components may include:
1. Engine change unit or auxiliary power unit (turbo-prop, turbofan, turboshaft, turbojet and piston)
2. Fuel, oil and air system (or induction and super/turbo charger systems in the case of piston engine) components
3. Engine control system components
4. Ignition or igniter system components
5. Starting system components
6. Fire protection system components
7. Accessories and associated drives
Application
Application of this unit may relate to:
scheduled or unscheduled maintenance activities
individual or team-related activities
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 remove and install engines and engine system components on fixed or rotary wing aircraft 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 units that require similar techniques. It is essential that safety precautions applicable to engines and engine systems being maintained are fully observed, understood and complied with, including allowance for the effect on aircraft centre of gravity when engines are removed. Awareness must be demonstrated of dual inspection requirements associated with work on engine control systems.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through removal and installation of a representative range of engines and engine system components. An understanding of component attachment methods and the need for adjustment, rigging and system operation as it relates 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 at least one item from each of Groups 1 to 7 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, or by the use of simulated activities, using tools and equipment specified in 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
Individuals being assessed who have already attained MEA353A Maintain basic light aircraft engines and propellers, will have satisfied the requirements of this unit with regard to common Range Statement variables. Log of Industrial Experience and Achievement records relating to MEA353A Maintain basic light aircraft engines and propellers, may be accepted as also meeting the evidence requirements for this unit in the applicable common areas.
Overview of assessment
A person who demonstrates competency in this unit must be able to apply hand skills and use maintenance publications to remove and install engines and engine system components on fixed or rotary wing aircraft 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 units that require similar techniques. It is essential that safety precautions applicable to engines and engine systems being maintained are fully observed, understood and complied with, including allowance for the effect on aircraft centre of gravity when engines are removed. Awareness must be demonstrated of dual inspection requirements associated with work on engine control systems.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through removal and installation of a representative range of engines and engine system components. An understanding of component attachment methods and the need for adjustment, rigging and system operation as it relates 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 at least one item from each of Groups 1 to 7 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, or by the use of simulated activities, using tools and equipment specified in 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
Individuals being assessed who have already attained MEA353A Maintain basic light aircraft engines and propellers, will have satisfied the requirements of this unit with regard to common Range Statement variables. Log of Industrial Experience and Achievement records relating to MEA353A Maintain basic light aircraft engines and propellers, may be accepted as also meeting the evidence requirements for this unit in the applicable common areas.
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| W8405 | MEA306B | Remove and install engines and engine system components | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| AUF81 | MEA306 | Remove and install engines and engine 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 |
| D744 | MEA40711 | Certificate IV in Aeroskills (Mechanical) | Qualification |
| D741 | MEA30211 | Certificate III in Aeroskills (Mechatronics) | Qualification |
| D746 | MEA41011 | Certificate IV in Aeroskills (Mechatronics) | Qualification |