Unit of competency Outline
Date retreived
23/07/2026 12:43 AM AWST
23/07/2026 12:43 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 aircraft hydro-mechanical and landing gear system components
Remove and install aircraft hydro-mechanical and landing gear system components
Unit of competency
National Code
MEA302
MEA302
State Code
AUE56
AUE56
TGA Status
Replaced
Replaced
DTWD Status
Replaced
Replaced
State Implementation and Classification
Approved Date
22/07/2015
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
22/07/2015
Nominal Hours
60
Description
This unit of competency 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 requires application of hand skills and standard trade practices in the removal and installation of aircraft hydro-mechanical system and landing gear components fitted to both fixed and rotary wing aircraft during the performance of scheduled or unscheduled maintenance. Maintenance may be performed individually or as part of a team.The unit is used in workplaces that operate under the airworthiness regulatory systems of the Australian Defence Force (ADF) and the Civil Aviation safety Authority (CASA). Where a CASA licensing outcome is sought this unit forms part of the CASA requirement for the granting of the chosen maintenance certification licence under Civil Aviation Safety Regulation (CASR) Part 66, in accordance with the licensing provisions in the Companion Volume Implementation Guide.
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 while observing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE)
- 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 while observing all relevant WHS requirements, including the use of MSDS and items of PPE
- 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 while observing all relevant WHS requirements, including the use of MSDS and items of PPE
- 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 while observing all relevant WHS requirements, including the use of MSDS and items of PPE
- 4.3 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
No information
No information
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| D4417 | MEA302C | Remove and install aircraft hydro-mechanical and landing gear system components | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| OAD17 | MEA398 | Remove and install aircraft hydro-mechanical and landing gear system components | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| AVO6 | MEA50215 | Diploma of Aeroskills (Mechanical) | Qualification |
| AVP0 | MEA40715 | Certificate IV in Aeroskills (Mechanical) | Qualification |
| AVP4 | MEA30215 | Certificate III in Aeroskills (Mechatronics) | Qualification |
| AVN4 | MEA41015 | Certificate IV in Aeroskills (Mechatronics) | Qualification |
| AVN6 | MEA41315 | Certificate IV in Aeroskills (Structures) | Qualification |
| AVO9 | MEA30315 | Certificate III in Aircraft Life Support and Furnishing | Qualification |
| AVP1 | MEA41115 | Certificate IV in Aircraft Life Support and Furnishing | Qualification |
| AVP5 | MEA40915 | Certificate IV in Aircraft Surface Finishing | Qualification |