Unit of competency Outline
Date retreived
22/07/2026 6:08 AM AWST
22/07/2026 6:08 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.
Remove and install rotary wing rotor and flight control system components
Remove and install rotary wing rotor and flight control system components
Unit of competency
National Code
MEA308B
MEA308B
State Code
W8407
W8407
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.
In the case of powered flying controls, fluid power actuators and control units, the competency is covered by unit MEA302B.
1. Main rotor blades, tail rotor blades
2. Rotor heads
3. Swash plates, tail rotor pitch control assemblies
4. Mechanical flight control components (ie cables, pulleys, guides, fairleads, tension regulators, control rods, bellcranks, torque tubes, control sticks or columns, tail rotor pedals), powered flight control components
5. Main rotor, intermediate or tail rotor gearboxes
6. 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.
In the case of powered flying controls, fluid power actuators and control units, the competency is covered by unit MEA302B.
1. Main rotor blades, tail rotor blades
2. Rotor heads
3. Swash plates, tail rotor pitch control assemblies
4. Mechanical flight control components (ie cables, pulleys, guides, fairleads, tension regulators, control rods, bellcranks, torque tubes, control sticks or columns, tail rotor pedals), powered flight control components
5. Main rotor, intermediate or tail rotor gearboxes
6. Drive shafts, couplings.
Overview of assessment
A person who demonstrates competency in this unit must be able to apply hand skills and use maintenance publications to remove and install rotary wing aircraft rotors and flight control system components 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 into other units that require similar techniques. It is essential that safety precautions applicable to the rotary wing rotor and flight control system components being maintained, including allowance for the effect on weight and balance (ie cg) when heavy components are removed, are fully observed, understood and complied with.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through removal and installation of a representative range of the rotary wing rotor and flight control system components. An understanding of component attachment methods, the need for adjustment or rigging and system operation as it relates to the work must be demonstrated 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 6 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.
A person who demonstrates competency in this unit must be able to apply hand skills and use maintenance publications to remove and install rotary wing aircraft rotors and flight control system components 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 into other units that require similar techniques. It is essential that safety precautions applicable to the rotary wing rotor and flight control system components being maintained, including allowance for the effect on weight and balance (ie cg) when heavy components are removed, are fully observed, understood and complied with.
Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through removal and installation of a representative range of the rotary wing rotor and flight control system components. An understanding of component attachment methods, the need for adjustment or rigging and system operation as it relates to the work must be demonstrated 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 6 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.
Replaces
| State Code | National Code | Title | Type |
|---|---|---|---|
| W1125 | MEA308A | Remove and install rotary wing rotor and flight control system components | Unit of competency |
Replaced By
| State Code | National Code | Title | Type |
|---|---|---|---|
| D4423 | MEA308C | Remove and install rotary wing rotor and flight control system 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 |