Unit of competency Outline
Date retreived
22/07/2026 11:06 PM AWST
22/07/2026 11:06 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.
Lay out avionic systems
Lay out avionic systems
Unit of competency
National Code
MEA270A
MEA270A
State Code
W8396
W8396
TGA Status
Replaced
Replaced
DTWD Status
Replaced
Replaced
State Implementation and Classification
Approved Date
30/06/2011
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
30/06/2011
Nominal Hours
120
Description
This unit is part of Diploma and Advanced Diploma training pathways. It covers the basic design and layout to block diagram level of avionic systems.
Notes
Elements and Performance Criteria
1. Lay out to block diagram level an aircraft electrical system
- 1.1. The functions of aircraft electrical systems are identified
- 1.2. Aircraft electrical system components are identified
- 1.3. A typical aircraft electrical system is sketched at block diagram level
- 1.4. Aircraft electrical system maintenance requirements are identified
2. Lay out to block diagram level an instrument measuring system
- 2.1. The various instrument measuring systems are identified
- 2.2. Measuring system components are identified
- 2.3. A typical instrument measuring system is sketched at block diagram level
- 2.4. Measuring system maintenance requirements are identified
3. Lay out to block diagram level a pressurisation control system
- 3.1. Pressurisation control system components are identified
- 3.2. A typical pressurisation control system is sketched at block diagram level
- 3.3. Pressurisation control system maintenance requirements are identified
4. Lay out to block diagram level an aircraft oxygen system
- 4.1. The various types of oxygen system are identified
- 4.2. Oxygen system components are identified
- 4.3. A typical oxygen system is sketched at block diagram level
- 4.4. Oxygen system maintenance requirements are identified
The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance. Bold italicised wording, if used in the performance criteria, is detailed below. Essential operating conditions that may be present with training and assessment (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) may also be included.
Application
Application of this unit may relate to individual or team-related activities
Functions of aircraft electrical systems
Functions of aircraft electrical systems may include:
power generation, control and distribution
lighting
electrically operated systems, such as doors, flap and landing gear systems
system control (e.g. hydraulic, pneumatic, air conditioning, propeller control and anti-skid)
warning systems
ice and rain protection
engine systems
Aircraft electrical system components
Aircraft electrical system components may include:
the major components of each of the above systems that would be shown in a block diagram or schematic
Instrument measuring systems
Instrument measuring systems may include:
engine indication
transmitter/indicator measuring (pressure, temperature and position)
fuel quantity indication and flow indication
Measuring system components
Measuring system components may include:
the major components of each of the above systems that would be shown in a block diagram or schematic
Pressurisation control system components
Pressurisation control system components may include:
the major components of a pressurisation control system that would be shown in a block diagram or schematic
Types of oxygen system
Types of oxygen system may include:
gaseous
liquid
chemical
Oxygen system components may include:
Oxygen system components may include:
the major components of each of the above systems that would be shown in a block diagram or schematic
Application
Application of this unit may relate to individual or team-related activities
Functions of aircraft electrical systems
Functions of aircraft electrical systems may include:
power generation, control and distribution
lighting
electrically operated systems, such as doors, flap and landing gear systems
system control (e.g. hydraulic, pneumatic, air conditioning, propeller control and anti-skid)
warning systems
ice and rain protection
engine systems
Aircraft electrical system components
Aircraft electrical system components may include:
the major components of each of the above systems that would be shown in a block diagram or schematic
Instrument measuring systems
Instrument measuring systems may include:
engine indication
transmitter/indicator measuring (pressure, temperature and position)
fuel quantity indication and flow indication
Measuring system components
Measuring system components may include:
the major components of each of the above systems that would be shown in a block diagram or schematic
Pressurisation control system components
Pressurisation control system components may include:
the major components of a pressurisation control system that would be shown in a block diagram or schematic
Types of oxygen system
Types of oxygen system may include:
gaseous
liquid
chemical
Oxygen system components may include:
Oxygen system components may include:
the major components of each of the above systems that would be shown in a block diagram or schematic
The Evidence Guide provides advice on assessment and must be read in conjunction with the performance criteria, required skills and knowledge, range statement and the Assessment Guidelines for the Training Package.
Overview of assessment
A person who demonstrates competency in this unit must be able to identify avionic systems and their components, lay out typical systems at block diagram level and identify related maintenance requirements. Competency in this unit cannot be claimed until all prerequisites have been satisfied.
Critical aspects for assessment and evidence required to demonstrate competency in this unit
Assessors must be satisfied that the candidate can competently and consistently perform all elements of the unit as specified by the criteria, including required knowledge, and be capable of applying the competency in new and different situations and contexts.
Assessors should gather a range of evidence that is valid, sufficient, current and authentic. Evidence can be gathered through a variety of ways including direct observation, supervisor's reports, project work, samples and questioning. Questioning techniques should not require language, literacy and numeracy skills beyond those required in this unit of competency.
Context of and specific resources for assessment
This unit may be assessed off the job in a training environment equipped to provide exposure to the range of system types and components. The candidate must have access to all tools, equipment, materials and documentation required and must be permitted to refer to any relevant workplace procedures, product and manufacturing specifications, codes, standards, manuals and reference materials. The assessment environment should not disadvantage the candidate.
Method of assessment
Guidance information for assessment
Overview of assessment
A person who demonstrates competency in this unit must be able to identify avionic systems and their components, lay out typical systems at block diagram level and identify related maintenance requirements. Competency in this unit cannot be claimed until all prerequisites have been satisfied.
Critical aspects for assessment and evidence required to demonstrate competency in this unit
Assessors must be satisfied that the candidate can competently and consistently perform all elements of the unit as specified by the criteria, including required knowledge, and be capable of applying the competency in new and different situations and contexts.
Assessors should gather a range of evidence that is valid, sufficient, current and authentic. Evidence can be gathered through a variety of ways including direct observation, supervisor's reports, project work, samples and questioning. Questioning techniques should not require language, literacy and numeracy skills beyond those required in this unit of competency.
Context of and specific resources for assessment
This unit may be assessed off the job in a training environment equipped to provide exposure to the range of system types and components. The candidate must have access to all tools, equipment, materials and documentation required and must be permitted to refer to any relevant workplace procedures, product and manufacturing specifications, codes, standards, manuals and reference materials. The assessment environment should not disadvantage the candidate.
Method of assessment
Guidance information for assessment
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| AUD66 | MEA270 | Lay out avionic systems | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| S755 | MEA50310 | Diploma of Aviation Maintenance Management (Avionics) | Qualification |
| J368 | MEM60112 | Advanced Diploma of Engineering | Qualification |
| J367 | MEM50212 | Diploma of Engineering - Technical | Qualification |