Unit of competency Outline

Date retreived
22/07/2026 11:33 PM AWST

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Remove and install basic aircraft electrical system components

Remove and install basic aircraft electrical system components

Unit of competency
National Code
MEAAVI0002
State Code
OEH05
TGA Status
Current
DTWD Status
Approved
Current Release Number
1.00
Current Release Date
22/11/2022
View on TGA
State Implementation and Classification
Approved Date
28/03/2023
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
28/03/2023
Nominal Hours
40
Description
This unit describes the skills and knowledge required to apply hand skills and use maintenance documentation and publications to remove and install aircraft direct current (DC) electrical system components of fixed and rotary wing aircraft that have only DC electrical systems during scheduled or unscheduled maintenance. Work 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 Civil Aviation Safety Authority (CASA) and the Defence Aviation Safety Authority (DASA).Any other relevant legislation, industry standards and codes of practice within Australia must be applied.
Notes
Elements and Performance Criteria
1. Remove DC aircraft electrical system components
  • 1.1 Render system safe and prepare it in accordance with maintenance manual, fitting required isolation tags to ensure personnel safety
  • 1.2 Remove electrical components in accordance with maintenance manual while observing all relevant work health and safety (WHS) requirements
  • 1.3 Complete and process required maintenance documentation relating to removal in accordance with standard enterprise procedures
  • 1.4 Tag and pack removed components in accordance with specified procedures
2. Install DC aircraft electrical system components
  • 2.1 Confirm correct part numbers, modification status, serviceability and shelf life of electrical components to be installed against maintenance manual
  • 2.2 Perform physical installation including connection of electrical components in accordance with the applicable maintenance manual, and ensure appropriate adjustment or alignment with mechanical interface is carried out
  • 2.3 Reinstate system to operational condition and prepare for required testing in accordance with maintenance manual
  • 2.4 Complete and process required maintenance documentation relating to installation in accordance with standard enterprise procedures
No information
No information
Replaces
State Code National Code Title Type
AUF80 MEA202 Remove and install basic aircraft electrical system components Unit of competency