Google Links

Follow the links below to find material targeted to the unit's elements, performance criteria, required skills and knowledge

Elements and Performance Criteria

  1. Inspect twin engine aircraft electrical systems and components
  2. Test/adjust twin engine aircraft electrical systems
  3. Troubleshoot twin engine aircraft electrical systems
  4. Remove and install twin engine aircraft electrical system components

Range Statement

This field allows for different work environments and conditions that may affect performance. Essential operating conditions that may be present (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) are included.

DC electrical systems include:

DC multi-generator and alternator/rectifier generator regulation and distribution systems and components

Electrical propeller control systems, such as feathering systems (where applicable to the enterprise)

Batteries in dual battery installations and associated mounting equipment, including related anti-vibration aids

Fire warning and extinguishing systems, including handling of halogen fire extinguishers (where applicable to the enterprise)

Combustion heating systems (where applicable to the enterprise)

Equipment cooling and ventilation

Fuel storage and distribution systems

Master and central warning systems (where applicable to the enterprise)

Electrical components include:

Components of multi-generator regulation and distribution systems

Electrical propeller control system components (where applicable to the enterprise)

Batteries in dual battery installations and associated mounting equipment, including related anti-vibration aids

Fire warning and extinguishing system components (where applicable to the enterprise)

Combustion heaters and associated components (where applicable to the enterprise)

Equipment cooling and ventilation components

Fuel storage and distribution system electrical components

Master and central warning system components (where applicable to the enterprise)

Procedures and requirements include:

Industry standard procedures specified by manufacturers, regulatory authorities or the enterprise


Performance Evidence

Evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria under the specified conditions of assessment, and must include:

applying relevant WHS practices

using approved maintenance documentation and aircraft publications relating to twin engine aircraft electrical systems

identifying/locating:

DC multi-generator power generation, regulation, distribution and control systems and components, i.e. regulators and bus bars

electrical propeller control systems and components, such as feathering and synchronising systems

batteries in dual battery installations and associated mounting equipment, including related anti-vibration aids

fire warning and extinguishing systems and components

identification of halogen (e.g. BCF) fire extinguishers

combustion heating systems

equipment cooling and ventilation

fuel storage and distribution system electrical components

master and central warning systems

correctly connecting DC generators and alternator/rectifier generators in multi-generator systems and paralleling generator output

recognising system and component defects/external damage, correct installation, connection of plugs, terminations, attaching hardware (including cabling/harnesses) and security in the above systems and system components

applying logic processes, taking and interpreting electrical measurements, using test equipment and appropriate wiring diagrams and manuals to isolate malfunctions in the above systems

performing system functional tests and checks to isolate system faults and assess post-maintenance serviceability.

It is essential that system testing procedures, cleanliness requirements and safety precautions applicable to the electrical system being maintained are fully observed, understood and complied with. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice across a range of inspection, testing and troubleshooting applications (including the timely involvement of supervisors or other trades) is critical.

Evidence of transferability of skills and knowledge related to inspection, testing and troubleshooting and component removal and installation is essential. This is to be demonstrated through application across a range of aircraft electrical systems and components listed in the Assessment Conditions.


Knowledge Evidence

Evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria and include knowledge of:

system testing procedures and paralleling of generator output

the basic layout (block diagram level), function and operation of:

DC multi-generator and alternator/rectifier generator regulation and distribution systems and components

electrical propeller control systems, such as feathering and synchronising systems and system components

dual battery systems and associated mounting equipment, including related anti-vibration aids

fire warning and extinguishing systems and system components, including regulatory requirements relating to halogen (e.g. BCF) fire extinguishers

combustion heating systems and system components

equipment cooling and ventilation systems and system components

fuel storage and distribution systems and system components

master and central warning systems and system components

maintenance requirements and troubleshooting procedures for the above electrical systems

relevant WHS practices

relevant maintenance manuals

relevant regulatory requirements and standard procedures.