Elements and Performance Criteria
- Remove DC aircraft electrical system components
- System is rendered safe and prepared in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety
- Electrical component removal is carried out in accordance with the applicable maintenance manual while observing all relevant work health and safety (WHS) requirements
- Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
- Removed components are tagged and packaged in accordance with specified procedures
- Install DC aircraft electrical system components
- Electrical components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life
- Physical installation of electrical components is performed in accordance with the applicable maintenance manual, ensuring appropriate adjustment/alignment with mechanical interface is carried out
- System is reinstated to correct operational condition in preparation for testing, as necessary
- Required maintenance documentation is completed and processed in accordance with standard enterprise procedures