Unit of competency Outline

Date retreived
23/07/2026 7:15 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.

Maintain airframe systems of basic light fixed wing aircraft

Maintain airframe systems of basic light fixed wing aircraft

Unit of competency
National Code
MEA351
State Code
AUD63
TGA Status
Replaced
DTWD Status
Replaced
Current Release Number
2.00
Current Release Date
31/08/2018
View on TGA
State Implementation and Classification
Approved Date
22/07/2015
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
22/07/2015
Nominal Hours
90
Description
This unit of competency requires application of hand skills and the use of system/component knowledge and applicable maintenance publications and test equipment to inspect, test and troubleshoot, and replace components of airframe systems of fixed wing aircraft that have fixed undercarriage and a normally aspirated engine driving a fixed pitch propeller, or a small gas turbine engine. This may be done during the performance of scheduled or unscheduled maintenance. Maintenance may be performed individually or as part of a team.The unit is part of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathway. Where a Civil Aviation Safety Authority (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. Inspect basic light fixed wing airframe systems
  • 1.1 Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements
  • 1.2 Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual
  • 1.3 Airframe system components are visually or physically checked for external signs of defects in accordance with 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)
  • 1.4 Defects are correctly identified and reported
2. Test/adjust basic light fixed wing airframe systems and components
  • 2.1 Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation
  • 2.2 Airframe system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction
  • 2.3 System adjustment/rigging is performed in accordance with maintenance manual
3. Troubleshoot basic light fixed wing airframe systems
  • 3.1 Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination
  • 3.2 Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting to line replacement level
  • 3.3 Specialist advice is obtained, where required, to assist with the troubleshooting process
  • 3.4 Airframe system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures
  • 3.5 Rectification requirements are determined
4. Remove and install basic light fixed wing airframe system components
  • 4.1 System is rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety
  • 4.2 Airframe system component removal 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 accurately completed and correctly processed
  • 4.4 Removed components are tagged, sealed and packaged in accordance with specified procedures
  • 4.5 Components to be installed are checked to confirm correct part numbers, serviceability and modification status
  • 4.6 Mass balance of control surfaces to be installed is checked in accordance with the applicable maintenance manual, if required
  • 4.7 Installation is carried out in accordance with the applicable maintenance manual
  • 4.8 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
No information
No information
Replaces
State Code National Code Title Type
D4463 MEA351A Maintain airframe systems of basic light fixed wing aircraft Unit of competency
Replaced By
State Code National Code Title Type
OEH98 MEAMEC0040 Maintain airframe systems of basic light fixed wing aircraft Unit of competency