Unit of competency Outline

Date retreived
22/07/2026 12:47 PM 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 avionic system components

Remove and install avionic system components

Unit of competency
National Code
MEA343
State Code
AUE67
TGA Status
Current
DTWD Status
Approved
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
40
Description
This unit of competency requires application of hand skills and the use of maintenance documentation/publications in the removal, installation and task certification of avionic system components of fixed and rotary wing aircraft during the performance of scheduled or unscheduled maintenance where system serviceability can be established by a simple self-test facility, other on-board test systems/equipment or by simple ramp test equipment. Maintenance may be performed individually or as part of a team.The unit is part of the B1 maintenance certification licensing pathway 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 avionic 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 Avionic 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. Install avionic system components and verify system serviceability
  • 2.1 Avionic components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life
  • 2.2 Installation of avionic components is performed in accordance with the applicable maintenance manual and regulatory requirements while observing all relevant WHS requirements
  • 2.3 System is reinstated to correct operational condition and is tested for serviceability
  • 2.4 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures and regulatory requirements
No information
No information
Replaces
State Code National Code Title Type
D4462 MEA343B Remove and install avionic system components Unit of competency