Unit of competency Outline

Date retreived
22/07/2026 5:46 AM AWST

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Inspect, test and troubleshoot aircraft fixed wing flight control systems and components

Inspect, test and troubleshoot aircraft fixed wing flight control systems and components

Unit of competency
National Code
MEA312
State Code
AUE73
TGA Status
Current
DTWD Status
Approved
Current Release Number
1.00
Current Release Date
12/02/2015
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
60
Description
This unit of competency requires application of hand skills and the use of maintenance publications and knowledge of system theory to inspect, test and troubleshoot fixed wing aircraft flight control system components during the performance of scheduled or unscheduled maintenance. Maintenance may be performed individually or as part of a team.This unit is part of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathway. 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. Inspect fixed wing flight control systems and components
  • 1.1 Isolation tags already attached to the system or related systems are checked and aircraft configured for safe system inspection and operation in accordance with applicable maintenance manual
  • 1.2 Fixed wing flight control systems and components are visually or physically checked for signs of defects in accordance with the applicable maintenance manual while observing all relevant work health and safety (WHS) requirements
2. Test fixed wing flight control systems
  • 2.1 Powered controls of the aircraft and system are prepared in accordance with maintenance manual for the application of electrical and hydraulic power
  • 2.2 Power is applied, if necessary, and system is functionally tested in accordance with applicable maintenance manual for malfunction or evidence of incorrect rigging
  • 2.3 System rigging is performed in accordance with applicable maintenance manual
3. Prepare for troubleshooting
  • 3.1 Relevant maintenance documentation and modification status, including system defect reports, where relevant, are interpreted to identify an unserviceability
4. Troubleshoot fixed wing flight control systems
  • 4.1 Available information from maintenance documentation and inspection and test results is used, where necessary, to assist in fault determination
  • 4.2 Maintenance manual fault diagnosis guide and logical processes are used to ensure efficient and accurate troubleshooting to line replacement level
  • 4.3 Specialist advice is obtained, where required, to assist with the troubleshooting process
  • 4.4 Fixed wing flight control system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required
  • 4.5 Fault rectification requirements are determined to assist in planning the repair
No information
No information
Replaces
State Code National Code Title Type
D4428 MEA312C Inspect, test and troubleshoot aircraft fixed wing flight control systems and components Unit of competency