Unit of competency Outline
Date retreived
22/07/2026 9:06 PM AWST
22/07/2026 9:06 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 aircraft hydro-mechanical and landing gear system components
Remove and install aircraft hydro-mechanical and landing gear system components
Unit of competency
National Code
MEA302B
MEA302B
State Code
W8401
W8401
TGA Status
Replaced
Replaced
DTWD Status
Replaced
Replaced
State Implementation and Classification
Approved Date
22/06/2011
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
22/06/2011
Nominal Hours
60
Description
Notes
Elements and Performance Criteria
No information
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.
The work can include associated electrical loom terminations and/or plugs
1. Hydraulic systems
2. Fuel systems
3. Hydraulic accumulators, filters, reservoirs, valves, pumps, motors, actuators, regulators, direct reading gauges
4. Fuel system filters, valves, pumps, rigid and flexible storage cells/tanks
5. Rigid and flexible pipelines, hoses and fittings
6. Wheel assemblies or skids
7. Brake units
8. Struts/oleos
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.
The work can include associated electrical loom terminations and/or plugs
1. Hydraulic systems
2. Fuel systems
3. Hydraulic accumulators, filters, reservoirs, valves, pumps, motors, actuators, regulators, direct reading gauges
4. Fuel system filters, valves, pumps, rigid and flexible storage cells/tanks
5. Rigid and flexible pipelines, hoses and fittings
6. Wheel assemblies or skids
7. Brake units
8. Struts/oleos
Overview of assessment
A person who demonstrates competency in this unit must be able to remove and install a range of hydraulic and fuel system and landing gear components in accordance with relevant maintenance manual instructions while applying all relevant OH&S procedures and standard processes.
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 system cleanliness requirements and safety precautions applicable to the system being maintained are fully observed, understood and complied with.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through application across a number of aircraft systems or aircraft types, but must cover a sufficient range of tasks to demonstrate familiarity with attachment methods, connection hardware and couplings peculiar to each type of system, and of safe handling of heavy components. An understanding of 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 this Unit of Competency are being achieved under routine supervision on each type of system and on at least one component of each group listed in the Range Statement, as follows:
Hydraulic systems - a system and at least one component from each of hydro-mechanical system components 3 and 5
Fuel systems - a system and at least one component from each of 4 and 5
Landing gear components - one each of 6 to 8. Coverage of brakes and struts/oleos are not required where the aircraft is rotary wing and is fitted with skids or floats.
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 simulated work environment, using procedures, tools and equipment specified in maintenance documentation. It is also expected that general purpose tools, test and ground support equipment found in most routine situations would be used where appropriate.
A person who demonstrates competency in this unit must be able to remove and install a range of hydraulic and fuel system and landing gear components in accordance with relevant maintenance manual instructions while applying all relevant OH&S procedures and standard processes.
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 system cleanliness requirements and safety precautions applicable to the system being maintained are fully observed, understood and complied with.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through application across a number of aircraft systems or aircraft types, but must cover a sufficient range of tasks to demonstrate familiarity with attachment methods, connection hardware and couplings peculiar to each type of system, and of safe handling of heavy components. An understanding of 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 this Unit of Competency are being achieved under routine supervision on each type of system and on at least one component of each group listed in the Range Statement, as follows:
Hydraulic systems - a system and at least one component from each of hydro-mechanical system components 3 and 5
Fuel systems - a system and at least one component from each of 4 and 5
Landing gear components - one each of 6 to 8. Coverage of brakes and struts/oleos are not required where the aircraft is rotary wing and is fitted with skids or floats.
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 simulated work environment, using procedures, tools and equipment specified in maintenance documentation. It is also expected that general purpose tools, test and ground support equipment found in most routine situations would be used where appropriate.
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| W1119 | MEA302A | Remove and install aircraft hydro-mechanical system components | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| D4417 | MEA302C | Remove and install aircraft hydro-mechanical and landing gear system components | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| W492 | MEA40707 | Certificate IV in Aeroskills (Mechanical) | Qualification |
| W496 | MEA50207 | Diploma of Aeroskills (Mechanical) | Qualification |
| W493 | MEA40807 | Certificate IV in Aeroskills (Structures) | Qualification |
| W494 | MEA40907 | Certificate IV in Aircraft Surface Finishing | Qualification |