Unit of competency Outline
Date retreived
22/07/2026 4:55 AM AWST
22/07/2026 4:55 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.
Apply basic aircraft power plant design characteristics
Apply basic aircraft power plant design characteristics
Unit of competency
National Code
MEA342
MEA342
State Code
AUE99
AUE99
TGA Status
Replaced
Replaced
DTWD Status
Replaced
Replaced
State Implementation and Classification
Approved Date
22/07/2015
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
22/07/2015
Nominal Hours
120
Description
This unit of competency requires application of basic knowledge of propulsion and power plant selection for aeroplanes and rotary wing aircraft, piston engines and propellers/rotors, turbo prop, gas turbines and gas turbine/rotor.The unit is part of Diploma and Advanced Diploma training pathways. It 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. Research and evaluate the types of aeroplane and rotary wing aircraft power plant and their relative advantages and disadvantages
- 1.1 The types of aeroplane and rotary wing aircraft power plant are identified and compared in terms of relative advantages and disadvantages
- 1.2 Types of propeller are identified and compared in terms of relative advantages and disadvantages
- 1.3 Turbojet and turbofan performance is compared in terms of relative advantages and disadvantages
- 1.4 Maintenance requirements for aircraft power plants are identified
2. Apply basic power plant and propulsion system selection processes
- 2.1 Given required aeroplane use and performance characteristics an appropriate type of power plant is determined
- 2.2 An appropriate type of propulsion system is selected
- 2.3 Given required rotary wing aircraft use and performance characteristics an appropriate type of power plant is determined
No information
No information
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| W8440 | MEA342A | Apply basic aircraft power plant design characteristics | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| OEH04 | MEAMEC0033 | Apply basic aircraft power plant design characteristics | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| AVP3 | MEA60415 | Advanced Diploma of Aeronautical Engineering | Qualification |
| AVO1 | MEA50615 | Diploma of Aeronautical Engineering | Qualification |
| BDW4 | MEA50618 | Diploma of Aeronautical Engineering | Qualification |
| BDV7 | MEA60418 | Advanced Diploma of Aeronautical Engineering | Qualification |
| BDX1 | MEA50518 | Diploma of Aeroskills (Non-Destructive Testing) | Qualification |
| AVN8 | MEA50515 | Diploma of Aeroskills (Non-Destructive Testing) | Qualification |
| BDW9 | MEA60318 | Advanced Diploma of Aviation Non-Destructive Testing | Qualification |
| AVN3 | MEA60315 | Advanced Diploma of Aviation Non-Destructive Testing | Qualification |