Unit of competency Outline

Date retreived
22/07/2026 8:22 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.

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
MEA302C
State Code
D4417
TGA Status
Replaced
DTWD Status
Replaced
Current Release Number
2.00
Current Release Date
23/01/2012
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 is part of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathway and may also be part of a Structures Certificate IV training pathway. It covers the competencies required to remove and install aircraft hydro-mechanical system and landing gear components. This 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 hydro-mechanical system components
  • 1.1. Hydro-mechanical system is rendered safe and prepared in accordance with the applicable maintenance manual, including fitment of isolation tags, where necessary, to ensure personal safety
  • 1.2. Removal of hydro-mechanical components is carried out in accordance with the applicable maintenance manual
  • 1.3. Required maintenance documentation is accurately completed and correctly processed
  • 1.4. Removed components are tagged, sealed and packaged in accordance with specified procedures
2. Remove landing gear components
  • 2.1. The aircraft is jacked as specified in the maintenance manual for landing gear component removal
  • 2.2. Removal of components is carried out in accordance with the applicable maintenance manual
  • 2.3. Required maintenance documentation is accurately completed and correctly processed
  • 2.4. Removed components are tagged, sealed and packaged in accordance with specified procedures
3. Install hydro-mechanical system components
  • 3.1. Components to be installed are checked to confirm correct part numbers, serviceability and modification status
  • 3.2. Component installation is carried out in accordance with the applicable maintenance manual
  • 3.3. Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
4. Install landing gear components
  • 4.1. Components to be installed are checked to confirm correct part numbers, serviceability and modification status
  • 4.2. Component installation is carried out in accordance with the applicable maintenance manual
  • 4.3. 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
Hydro-mechanical systems and components
Hydro-mechanical systems include:
1. Hydraulic systems
2. Fuel systems
Components of hydro-mechanical systems include:
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
Landing gear components
Landing gear components include:
6. Wheel assemblies or skids
7. Brake units
8. Struts/oleos
Electrical interface
The work can include associated electrical loom terminations and/or plugs
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 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 OHS 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 - preparation of a system for safe component removal and replacement of at least one component from each of hydro-mechanical system components 3 and 5
Fuel systems - preparation of a system for safe component removal and replacement of 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.
Method of assessment

Guidance information for assessment
Replaces
State Code National Code Title Type
W8401 MEA302B Remove and install aircraft hydro-mechanical and landing gear system components Unit of competency
Replaced By
State Code National Code Title Type
AUE56 MEA302 Remove and install aircraft hydro-mechanical and landing gear system components Unit of competency