Unit of competency Outline
Date retreived
22/07/2026 7:43 AM AWST
22/07/2026 7:43 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.
Inspect, test and troubleshoot rotary wing rotor and control systems and components
Inspect, test and troubleshoot rotary wing rotor and control systems and components
Unit of competency
National Code
MEA316B
MEA316B
State Code
W8415
W8415
TGA Status
Replaced
Replaced
DTWD Status
Replaced
Replaced
State Implementation and Classification
Approved Date
22/06/2011
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
22/06/2011
Nominal Hours
60
Description
Notes
Elements and Performance Criteria
No information
Application of this unit may relate to:
Scheduled or unscheduled maintenance
Individual or team related activities
Procedures and requirements refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise.
1. Main rotor blades, tail rotor blades
2. Rotor heads, swash plates, tail rotor pitch control assemblies
3. Mechanical, powered flight control components
4. Main rotor, intermediate or tail rotor gearboxes
5. Drive shafts, couplings
Scheduled or unscheduled maintenance
Individual or team related activities
Procedures and requirements refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise.
1. Main rotor blades, tail rotor blades
2. Rotor heads, swash plates, tail rotor pitch control assemblies
3. Mechanical, powered flight control components
4. Main rotor, intermediate or tail rotor gearboxes
5. Drive shafts, couplings
Overview of assessment
A person who demonstrates competency in this unit must be able to apply hand skills, use maintenance publications and rotor and rotor control system theory knowledge to inspect, test and troubleshoot rotors and their control systems on rotary wing aircraft while applying 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, testing and troubleshooting applications (including the timely involvement of supervisors or other trades) associated with the rotor control systems. It is essential that testing procedures take into account all safety precautions associated with ground testing of rotor and rotor control systems, and that awareness be demonstrated of dual inspection requirements associated with work on control systems.
Evidence of transferability of skills and knowledge related to inspection, testing and troubleshooting is essential. This may be demonstrated through application across a number of aircraft types. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical. The application of ground testing procedures should also clearly indicate knowledge of system operation. System operation knowledge, the relationship of individual components and the links with other systems will be necessary to supplement evidence of ability to troubleshoot the system within the limits of the aircraft/system fault finding guide before undertaking any action. 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 at least one item from each of Groups 1 to 5, as listed 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 Evidence Guide.
Context of and specific resources for assessment
Competency should be assessed in the work environment or simulated work environment, using tools and equipment specified in aircraft maintenance manuals. It is also expected that general purpose tools, test and ground support equipment found in most routine situations would be used where appropriate. The level of troubleshooting is limited in its application to the use of fault diagnosis guides or other similar information.
A person who demonstrates competency in this unit must be able to apply hand skills, use maintenance publications and rotor and rotor control system theory knowledge to inspect, test and troubleshoot rotors and their control systems on rotary wing aircraft while applying 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, testing and troubleshooting applications (including the timely involvement of supervisors or other trades) associated with the rotor control systems. It is essential that testing procedures take into account all safety precautions associated with ground testing of rotor and rotor control systems, and that awareness be demonstrated of dual inspection requirements associated with work on control systems.
Evidence of transferability of skills and knowledge related to inspection, testing and troubleshooting is essential. This may be demonstrated through application across a number of aircraft types. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical. The application of ground testing procedures should also clearly indicate knowledge of system operation. System operation knowledge, the relationship of individual components and the links with other systems will be necessary to supplement evidence of ability to troubleshoot the system within the limits of the aircraft/system fault finding guide before undertaking any action. 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 at least one item from each of Groups 1 to 5, as listed 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 Evidence Guide.
Context of and specific resources for assessment
Competency should be assessed in the work environment or simulated work environment, using tools and equipment specified in aircraft maintenance manuals. It is also expected that general purpose tools, test and ground support equipment found in most routine situations would be used where appropriate. The level of troubleshooting is limited in its application to the use of fault diagnosis guides or other similar information.
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| W1133 | MEA316A | Inspect, test and troubleshoot rotary wing rotor and control systems and components | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| D4432 | MEA316C | Inspect, test and troubleshoot rotary wing rotor and control systems and components | Unit of competency |
| State Code | National Code | Title | Type |
|---|---|---|---|
| W492 | MEA40707 | Certificate IV in Aeroskills (Mechanical) | Qualification |
| W496 | MEA50207 | Diploma of Aeroskills (Mechanical) | Qualification |