Unit of competency Outline

Date retreived
22/07/2026 7:01 AM AWST

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Inspect aircraft electrical systems and components

Inspect aircraft electrical systems and components

Unit of competency
National Code
MEA223C
State Code
D4439
TGA Status
Replaced
DTWD Status
Replaced
Current Release Number
1.00
Current Release Date
15/11/2010
State Implementation and Classification
Approved Date
06/05/2011
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
06/05/2011
Nominal Hours
40
Description
This unit is part of the Avionic AME Certificate IV training pathways and is also part of the Mechanical Aircraft Maintenance Engineer licensing pathway. It covers the competencies required to inspect electrical systems and components of fixed and rotary wing aircraft. Where a CASA licensing outcome is sought this unit forms part of the CASA requirement for the granting of the chosen B1 or the B2 Aircraft Maintenance Engineer Licence under CASR Part 66, in accordance with the licensing provisions in Section 3, Assessment Guidelines.
Notes
Elements and Performance Criteria
1. Inspect electrical systems and components
  • 1.1. Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual.
  • 1.2. Electrical system components and hardware are visually or physically checked for external signs of defects in accordance with applicable maintenance manual.
  • 1.3. Defects are correctly identified and recorded in accordance with standard enterprise procedures.
RANGE STATEMENT
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.
Note
Range statements listed below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide.
Electrical systems and components
Electrical systems and components may include:
1. AC and/or DC power generation, regulation and distribution systems
2. Battery installations and bus ties/interlocks
3. Rotary and static inverters and TR units
4. Air cycle air conditioning and pressurisation systems
5. Flight, and engine control systems
6. Ignition and starting systems
7. Fire/smoke detection and extinguishing
8. Lighting
9. Master and caution warning systems
10. Equipment and furnishing
11. Equipment cooling and ventilation
12. Position indicating systems
13. Fuel storage and distribution
14. Propeller control systems
15. Landing gear indication and antiskid
16. Ice and rain protection
17. Waste water
Application
Application of this unit may relate to:
Scheduled or unscheduled maintenance activities
Individual or team related activities
Procedures and requirements
Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise
EVIDENCE GUIDE
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 inspect aircraft electrical systems and components while observing all relevant safety precautions.

Critical aspects for assessment and evidence required to demonstrate competency in this unit
The underlying skills inherent in this unit should be transferable across a range of inspection applications (including the timely involvement of supervisors or other trades) associated with aircraft electrical systems and components. It is essential that cleanliness requirements and safety precautions applicable to the system being maintained are fully observed, understood and complied with. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical.
Evidence of transferability of skills and knowledge related to inspection is essential. This is to be demonstrated through application across a range of aircraft electrical systems, components and hardware listed in the Range Statement. The work plan should take account of applicable safety and quality requirements in accordance with the industry and regulatory standards.
A person cannot be assessed as competent until it can be demonstrated to the satisfaction of the workplace assessor that the relevant elements of the Unit of Competency are being achieved under routine supervision on a system and related components in each Group 1 to 13 inclusive (Groups 14 to 17 may be omitted where they are not applicable to the enterprise) in the Range Statement. This shall be established via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry .

Context of and specific resources for assessment
Competency should be assessed in the workplace or simulated workplace using tools and equipment specified in the maintenance manuals. It is also expected that general and special purpose tools, test and ground support equipment would be used where appropriate.

Method of assessment

Guidance information for assessment
Replaces
State Code National Code Title Type
W8365 MEA223B Inspect aircraft electrical systems and components Unit of competency
Replaced By
State Code National Code Title Type
WC003 MEA223D Inspect aircraft electrical systems and components Unit of competency
State Code National Code Title Type
S753 MEA50110 Diploma of Aeroskills (Avionics) Qualification
S754 MEA50210 Diploma of Aeroskills (Mechanical) Qualification