Unit of competency Outline
Date retreived
22/07/2026 7:48 AM AWST
22/07/2026 7:48 AM 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.
Evaluate aircraft gas turbine engine power plants
Evaluate aircraft gas turbine engine power plants
Unit of competency
National Code
MEA720
MEA720
State Code
AUF31
AUF31
TGA Status
Current
Current
DTWD Status
Approved
Approved
State Implementation and Classification
Approved Date
22/07/2015
Field of Education
031501 - Aerospace Engineering
Original Release Date
22/07/2015
Nominal Hours
70
Description
This unit of competency applies to aircraft gas turbine engines, engine control, lubrication, inlet anti-ice and propeller systems, and components thereof. It involves evaluation of power plants and components for compliance with design standards and with airworthiness regulatory requirements within both civil and military environments. Also covered is documentation of the evaluation process within management systems, such as configuration management (CM) and integrated logistic support (ILS).It is suitable for people working within aircraft design teams, within the engineering departments of aircraft maintenance organisations or employed within Continuing Airworthiness Management Organisations (CAMOs) and Approved Engineering Organisations (AEOs), and for those pursuing qualifications or careers in those fields.Where the engine is installed in a rotorcraft the integration of engine and rotor control is covered in unit MEA718 Evaluate rotorcraft flight control system.This unit is used in workplaces that operate under the airworthiness regulatory systems of the Australian Defence Force (ADF) and the Civil Aviation Safety Authority (CASA).
Notes
Elements and Performance Criteria
1. Prepare to evaluate gas turbine engine power plant
- 1.1 Confirm and apply safe working practices relating to aircraft structure
- 1.2 Determine parameters and context of applications and purpose of evaluation
- 1.3 Confirm personal functions and responsibilities, team and support functional group interdependencies and communications
- 1.4 Confirm that tasks and responsibilities are appropriate to qualifications and delegations and that appropriate support, including licensed technical and professional assistance, is available
- 1.5 Determine chain of responsibility for the activity evaluation, reporting arrangements and timelines
- 1.6 Identify work health and safety (WHS) and regulatory requirements with particular emphasis on safety, codes of practice and standards, including airworthiness regulatory requirements for aircraft gas turbine engine power plants, risk management and organisational procedures
2. Identify principles and techniques required for evaluation of aircraft gas turbine engine power plant
- 2.1 Identify features and functions of power plant and related systems
- 2.2 Review gas turbine engine and engine system operation, layout and performance
- 2.3 Review engine control system design and function, including interface with full authority digital engine control systems
- 2.4 Review propeller and propeller control system design and function, including coordination of pitch with fuel flow and engine power
- 2.5 Review engine inlet anti-ice system design and function
- 2.6 Review engine lubricating system design and function
3. Evaluate aircraft gas turbine engine power plant and components
- 3.1 Evaluate proposed modifications and repairs to power plant systems and components
- 3.2 Evaluate power plant maintenance requirements
- 3.3 Evaluate power plant reliability and defect history
- 3.4 Evaluate proposed component substitutions
- 3.5 Evaluate for compliance with WHS Acts, regulations, codes, directives and standards/specifications, including those related to risk management
4. Report results
- 4.1 Report results of scoping, principles and techniques identification and evaluation of gas turbine engine power plant systems and system components
- 4.2 Provide documentation, such as modification instructions and drawings and data required by CM and/or ILS and for compliance with airworthiness regulations
No information
No information
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| D7552 | MEM23095A | Apply aeronautical system design principles and techniques in aeronautical engineering situations | Unit of competency |
| D7550 | MEM23084A | Apply scientific principles and techniques in aeronautical engineering situations | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| AVP3 | MEA60415 | Advanced Diploma of Aeronautical Engineering | Qualification |
| BDV7 | MEA60418 | Advanced Diploma of Aeronautical Engineering | Qualification |
| BIW5 | MEM60122 | Advanced Diploma of Engineering | Qualification |