Unit of competency Outline

Date retreived
22/07/2026 3:43 PM AWST

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Remove and install aircraft electrical/avionic components during line maintenance

Remove and install aircraft electrical/avionic components during line maintenance

Unit of competency
National Code
MEA264
State Code
AUF63
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
40
Description
This unit of competency requires application of hand skills and the use of maintenance documentation/publications in the removal and installation from fixed and rotary wing aircraft of a limited range of aircraft electrical and avionic system components that are within the privileges of the Aircraft Maintenance Engineer A Licence during scheduled or unscheduled maintenance. Work may be performed individually or as part of a team.It is one of the units required for the granting of the chosen Aircraft Maintenance Engineer A 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 aircraft electrical system components
  • 1.1 System is rendered safe and prepared in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety
  • 1.2 Electrical component removal is carried out in accordance with the applicable maintenance manual while observing all relevant work health and safety (WHS) requirements
  • 1.3 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
  • 1.4 Removed components are tagged and packaged in accordance with specified procedures
2. Remove avionic system components
  • 2.1 System is rendered safe and prepared in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety
  • 2.2 Avionic component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements
  • 2.3 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
  • 2.4 Removed components are tagged and packaged in accordance with specified procedures
3. Install aircraft electrical system components
  • 3.1 Electrical components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life
  • 3.2 Physical installation of electrical components is performed in accordance with the applicable maintenance manual ensuring appropriate adjustment/alignment with mechanical interface is carried out
  • 3.3 System is reinstated to correct operational condition in preparation for testing, as necessary
  • 3.4 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
4. Install avionic system components
  • 4.1 Avionic components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life
  • 4.2 Physical installation of electrical components is performed in accordance with the applicable maintenance manual ensuring appropriate adjustment/alignment with mechanical interface is carried out
  • 4.3 System is reinstated to correct operational condition in preparation for testing, as necessary
  • 4.4 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
No information
No information
Replaces
State Code National Code Title Type
W8394 MEA264A Remove and install aircraft electrical/avionic components during line maintenance Unit of competency