Unit of Competency Mapping – Information for Teachers/Assessors – Information for Learners

MEA352 Mapping and Delivery Guide
Maintain basic rotary wing aircraft systems

Version 1.0
Issue Date: May 2024


Qualification -
Unit of Competency MEA352 - Maintain basic rotary wing aircraft systems
Description
Employability Skills
Learning Outcomes and Application This unit of competency requires application of hand skills and the use of system/component knowledge and applicable maintenance publications and test equipment to inspect, test and troubleshoot, and replace components of rotor, rotor control systems and airframe systems of basic rotary wing aircraft during the performance of scheduled or unscheduled maintenance. Maintenance may be performed individually or as part of a team.Applications include rotary wing aircraft that have mechanical control systems, either skids or floats and a normally aspirated engine.This unit of competency is part of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathway. Where a Civil Aviation Safety Authority (CASA) licensing outcome is sought this unit forms part of the CASA requirement for the granting of the chosen maintenance certification licence under Civil Aviation Safety Regulation (CASR) Part 66, in accordance with the licensing provisions in the Companion Volume Implementation Guide.
Duration and Setting X weeks, nominally xx hours, delivered in a classroom/online/blended learning setting.

Competency should be assessed in the work environment or simulated work environment using tools and equipment specified in maintenance documentation. It is also expected that applicable general-purpose tools and test equipment found in most routine situations would be used where appropriate.

The application of testing procedures should clearly indicate knowledge of system operation, the relationship of individual components and the links with other systems (if applicable) 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.

The following conditions of assessment represent the requirements of the Regulators (ADF and CASA) and maintenance stakeholders and must be rigorously observed.

A person cannot be assessed as competent until it can be demonstrated to the satisfaction of the workplace assessor that the relevant elements and performance criteria of this unit of competency are being achieved under routine supervision on groups listed in the Range of Conditions, as follows:

at least one (1) component from each of:

main rotor blades and tail rotor blades

rotor heads, swash plates and tail rotor pitch control assemblies

mechanical flight control components (collective and cyclic pitch levers, rudder pedals, cables, pulleys, guides, fairleads, bellcranks, rods, torque tubes, chains and sprockets)

main rotor, intermediate or tail rotor gearboxes

drive shafts and couplings

fuel systems

cabin heating systems

a representative range of components from:

rigid or flexible fuel tanks, selector/shutoff valves and rigid or flexible plumbing

cabin heater ducting and control valves.

This shall be established via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry Evidence Guide (for details refer to the Companion Volume Assessment Guidelines).

Assessors must satisfy the requirements of the National Vocational Education and Training Regulator (Australian Skills Quality Authority, or its successors).

Where the unit is to be used for CASA licensing purposes the Assessor must also meet the criteria specified

Prerequisites/co-requisites
Competency Field Aviation maintenance
Development and validation strategy and guide for assessors and learners Student Learning Resources Handouts
Activities 		Slides
PPT 		Assessment 1 Assessment 2 Assessment 3 Assessment 4
Elements of Competency Performance Criteria              
Element: Inspect rotor and rotor control systems and components
  • Isolation and warning signs are fitted/installed to the system or related systems and the aircraft configured for safe system inspection and operation in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices
  • Rotor and rotor control system is visually or physically checked/inspected for external signs of defects in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices while observing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE)
  • Defects are identified and recorded in accordance with standard enterprise procedures
       
Element: Inspect basic rotary wing airframe systems
  • Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements
  • Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual
  • Airframe system components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE
  • Defects are correctly identified and reported
       
Element: Ground test rotor and rotor control systems
  • Aircraft and system are prepared in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices for the operation of engine and rotor system
  • Rotor and rotor control system are functionally tested in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices for evidence of malfunction
  • System calibration or adjustments are performed in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices
       
Element: Test/adjust basic rotary wing airframe systems and components
  • Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation
  • Airframe system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction
       
Element: System adjustment is performed in accordance with maintenance manual
       
Element: Troubleshoot rotor and rotor control systems
  • Available information from aircraft maintenance documentation, inspection and test results is used to assist in fault determination
  • Relevant aircraft publication fault diagnosis guide and logical processes are used to ensure efficient and accurate troubleshooting to line replacement level
  • Specialist advice is obtained to assist with the troubleshooting process
  • Rotor and rotor control system faults are located and the causes of the faults are clearly identified and recorded in aircraft maintenance documentation in accordance with standard enterprise procedures
  • Fault rectification requirements are determined
       
Element: Troubleshoot basic rotary wing airframe systems
  • Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination
  • Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting
  • Specialist advice is obtained, where required, to assist with the troubleshooting process
  • Airframe system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures
  • Rectification requirements are determined
       
Element: Remove and install rotary wing rotor and rotor system components
  • System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety
  • Rotor and rotor system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE
  • Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures
  • Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices
  • Rotor or rotor system component to be installed is checked to confirm correct part or model numbers, modification status and serviceability
  • Mass balance of rotor blades/head is checked in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices
  • Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices
  • Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage
       
Element: Remove and install rotor control system components
  • System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety
  • Rotary wing flight control system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE
  • Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures
  • Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices
  • Rotary wing flight control system components to be installed are checked to confirm correct part or model numbers, modification status and serviceability
  • Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices
  • Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage
       
Element: Remove and install basic rotary wing airframe system components
  • System is rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety
  • Airframe system component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE
  • Required maintenance documentation is accurately completed and correctly processed
  • Removed components are tagged, sealed and packaged in accordance with specified procedures
  • Components to be installed are checked to confirm correct part numbers, serviceability and modification status
  • Mass balance of control surfaces to be installed is checked in accordance with the applicable maintenance manual, if required
  • Installation is carried out in accordance with the applicable maintenance manual
  • Required maintenance documentation is completed and processed in accordance with standard enterprise procedures
       


Evidence Required

List the assessment methods to be used and the context and resources required for assessment. Copy and paste the relevant sections from the evidence guide below and then re-write these in plain English.

Elements describe the essential outcomes.

Performance criteria describe the performance needed to demonstrate achievement of the element.

1.

Inspect rotor and rotor control systems and components

1.1

Isolation and warning signs are fitted/installed to the system or related systems and the aircraft configured for safe system inspection and operation in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices

1.2

Rotor and rotor control system is visually or physically checked/inspected for external signs of defects in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices while observing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE)

1.3

Defects are identified and recorded in accordance with standard enterprise procedures

2.

Inspect basic rotary wing airframe systems

2.1

Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements

2.2

Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual

2.3

Airframe system components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE

2.4

Defects are correctly identified and reported

3.

Ground test rotor and rotor control systems

3.1

Aircraft and system are prepared in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices for the operation of engine and rotor system

3.2

Rotor and rotor control system are functionally tested in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices for evidence of malfunction

3.3

System calibration or adjustments are performed in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

4.

Test/adjust basic rotary wing airframe systems and components

4.1

Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation

4.2

Airframe system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction

43

System adjustment is performed in accordance with maintenance manual

5.

Troubleshoot rotor and rotor control systems

5.1

Available information from aircraft maintenance documentation, inspection and test results is used to assist in fault determination

5.2

Relevant aircraft publication fault diagnosis guide and logical processes are used to ensure efficient and accurate troubleshooting to line replacement level

5.3

Specialist advice is obtained to assist with the troubleshooting process

5.4

Rotor and rotor control system faults are located and the causes of the faults are clearly identified and recorded in aircraft maintenance documentation in accordance with standard enterprise procedures

5.5

Fault rectification requirements are determined

6.

Troubleshoot basic rotary wing airframe systems

6.1

Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination

6.2

Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting

6.3

Specialist advice is obtained, where required, to assist with the troubleshooting process

6.4

Airframe system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures

6.5

Rectification requirements are determined

7.

Remove and install rotary wing rotor and rotor system components

7.1

System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety

7.2

Rotor and rotor system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE

7.3

Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures

7.4

Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

7.5

Rotor or rotor system component to be installed is checked to confirm correct part or model numbers, modification status and serviceability

7.6

Mass balance of rotor blades/head is checked in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

7.7

Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

7.8

Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage

8.

Remove and install rotor control system components

8.1

System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety

8.2

Rotary wing flight control system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE

8.3

Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures

8.4

Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

8.5

Rotary wing flight control system components to be installed are checked to confirm correct part or model numbers, modification status and serviceability

8.6

Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

8.7

Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage

8.8

Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures

9.

Remove and install basic rotary wing airframe system components

9.1

System is rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety

9.2

Airframe system component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE

9.3

Required maintenance documentation is accurately completed and correctly processed

9.4

Removed components are tagged, sealed and packaged in accordance with specified procedures

9.5

Components to be installed are checked to confirm correct part numbers, serviceability and modification status

9.6

Mass balance of control surfaces to be installed is checked in accordance with the applicable maintenance manual, if required

9.7

Installation is carried out in accordance with the applicable maintenance manual

9.8

Required maintenance documentation is completed and processed in accordance with standard enterprise procedures

Evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria under the specified conditions of assessment, and must include:

using hand skills, tools and test equipment in the testing, adjustment and troubleshooting of:

rotary wing mechanical control systems

helicopter airframe systems and components, including rotors and rotor system

recognising system and component defects/external damage, correct installation and security for the range of airframe systems listed in the Range of Conditions

removing, installing and rigging of rotor systems and rotor/flight controls

removing and installing the range of airframe components listed in the Range of Conditions

checking rotor mass balance

performing system functional tests and checks to isolate system faults and assess post-maintenance serviceability

effectively using maintenance documentation and relevant fault diagnosis guides in the troubleshooting process and for component removal and installation

applying standard procedures

observing all relevant WHS procedures, including the use of PPE and MSDS.

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, rotors, rotor control systems, airframe systems and components of basic rotary wing aircraft. It is essential that relevant procedures, cleanliness requirements and safety precautions are fully observed, understood and complied with. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical.

This shall be demonstrated through application across a range of rotors, rotor control systems, airframe systems and components as listed in the Assessment Conditions.

Evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria and include knowledge of:

WHS precautions relevant to airframe system maintenance, including the lifting and handling of heavy components and how to obtain PPE and MSDS

standard trade practices relating to tool and test/rigging equipment usage and installation/securing of system components

theory of flight:

airflow

conditions of flight

lift and forces

drag

rotary flight principles:

terminology relating to:

aerofoils

main rotor blades

rotor discs

rotors (main and tail)

aerodynamic characteristics:

aerofoil design

forces

rotor thrust and power requirements

vortex ring

autorotation

helicopter stability

helicopter dynamic components:

main rotors:

blades

heads

linkages

tail rotors

swash plates

transmissions and drive shafts

helicopter structure and airframe systems:

structure and layout

engine and transmission

flight control system layout and operation

cabin heater system layout and operation

fuel system layout and operation

helicopter maintenance procedures and troubleshooting

relevant maintenance manuals

relevant regulatory requirements and standard procedures, including requirements for engine and rotor system operation.

Submission Requirements

List each assessment task's title, type (eg project, observation/demonstration, essay, assignment, checklist) and due date here

Assessment task 1: [title]      Due date:

(add new lines for each of the assessment tasks)

Assessment Tasks

Copy and paste from the following data to produce each assessment task. Write these in plain English and spell out how, when and where the task is to be carried out, under what conditions, and what resources are needed. Include guidelines about how well the candidate has to perform a task for it to be judged satisfactory.

Elements describe the essential outcomes.

Performance criteria describe the performance needed to demonstrate achievement of the element.

1.

Inspect rotor and rotor control systems and components

1.1

Isolation and warning signs are fitted/installed to the system or related systems and the aircraft configured for safe system inspection and operation in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices

1.2

Rotor and rotor control system is visually or physically checked/inspected for external signs of defects in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices while observing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE)

1.3

Defects are identified and recorded in accordance with standard enterprise procedures

2.

Inspect basic rotary wing airframe systems

2.1

Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements

2.2

Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual

2.3

Airframe system components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE

2.4

Defects are correctly identified and reported

3.

Ground test rotor and rotor control systems

3.1

Aircraft and system are prepared in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices for the operation of engine and rotor system

3.2

Rotor and rotor control system are functionally tested in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices for evidence of malfunction

3.3

System calibration or adjustments are performed in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

4.

Test/adjust basic rotary wing airframe systems and components

4.1

Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation

4.2

Airframe system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction

43

System adjustment is performed in accordance with maintenance manual

5.

Troubleshoot rotor and rotor control systems

5.1

Available information from aircraft maintenance documentation, inspection and test results is used to assist in fault determination

5.2

Relevant aircraft publication fault diagnosis guide and logical processes are used to ensure efficient and accurate troubleshooting to line replacement level

5.3

Specialist advice is obtained to assist with the troubleshooting process

5.4

Rotor and rotor control system faults are located and the causes of the faults are clearly identified and recorded in aircraft maintenance documentation in accordance with standard enterprise procedures

5.5

Fault rectification requirements are determined

6.

Troubleshoot basic rotary wing airframe systems

6.1

Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination

6.2

Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting

6.3

Specialist advice is obtained, where required, to assist with the troubleshooting process

6.4

Airframe system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures

6.5

Rectification requirements are determined

7.

Remove and install rotary wing rotor and rotor system components

7.1

System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety

7.2

Rotor and rotor system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE

7.3

Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures

7.4

Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

7.5

Rotor or rotor system component to be installed is checked to confirm correct part or model numbers, modification status and serviceability

7.6

Mass balance of rotor blades/head is checked in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

7.7

Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

7.8

Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage

8.

Remove and install rotor control system components

8.1

System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety

8.2

Rotary wing flight control system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE

8.3

Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures

8.4

Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

8.5

Rotary wing flight control system components to be installed are checked to confirm correct part or model numbers, modification status and serviceability

8.6

Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices

8.7

Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage

8.8

Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures

9.

Remove and install basic rotary wing airframe system components

9.1

System is rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety

9.2

Airframe system component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE

9.3

Required maintenance documentation is accurately completed and correctly processed

9.4

Removed components are tagged, sealed and packaged in accordance with specified procedures

9.5

Components to be installed are checked to confirm correct part numbers, serviceability and modification status

9.6

Mass balance of control surfaces to be installed is checked in accordance with the applicable maintenance manual, if required

9.7

Installation is carried out in accordance with the applicable maintenance manual

9.8

Required maintenance documentation is completed and processed in accordance with standard enterprise procedures

This field allows for different work environments and conditions that may affect performance. Essential operating conditions that may be present (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) are included.

Rotor and rotor control system components include:

Main rotor blades and tail rotor blades

Rotor heads, swash plates and tail rotor pitch control assemblies

Mechanical flight control components (collective and cyclic pitch levers, rudder pedals, cables, pulleys, guides, fairleads, bellcranks, rods, torque tubes, chains and sprockets)

Main rotor, intermediate or tail rotor gearboxes

Drive shafts and couplings

Engine and rotor system operation:

Must be performed by a qualified pilot

Airframe systems include:

Fuel systems

Cabin heating systems

Airframe system components include:

Rigid or flexible fuel tanks, selector/shutoff valves and rigid or flexible plumbing

Cabin heater ducting and control valves

Procedures and requirements include:

Industry standard procedures specified by manufacturers, regulatory authorities or the enterprise

Copy and paste from the following performance criteria to create an observation checklist for each task. When you have finished writing your assessment tool every one of these must have been addressed, preferably several times in a variety of contexts. To ensure this occurs download the assessment matrix for the unit; enter each assessment task as a column header and place check marks against each performance criteria that task addresses.

Observation Checklist

Tasks to be observed according to workplace/college/TAFE policy and procedures, relevant legislation and Codes of Practice Yes No Comments/feedback
Isolation and warning signs are fitted/installed to the system or related systems and the aircraft configured for safe system inspection and operation in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices 
Rotor and rotor control system is visually or physically checked/inspected for external signs of defects in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices while observing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE) 
Defects are identified and recorded in accordance with standard enterprise procedures 
Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements 
Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual 
Airframe system components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE 
Defects are correctly identified and reported 
Aircraft and system are prepared in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices for the operation of engine and rotor system 
Rotor and rotor control system are functionally tested in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices for evidence of malfunction 
System calibration or adjustments are performed in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices 
Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation 
Airframe system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction 
 
Available information from aircraft maintenance documentation, inspection and test results is used to assist in fault determination 
Relevant aircraft publication fault diagnosis guide and logical processes are used to ensure efficient and accurate troubleshooting to line replacement level 
Specialist advice is obtained to assist with the troubleshooting process 
Rotor and rotor control system faults are located and the causes of the faults are clearly identified and recorded in aircraft maintenance documentation in accordance with standard enterprise procedures 
Fault rectification requirements are determined 
Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination 
Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting 
Specialist advice is obtained, where required, to assist with the troubleshooting process 
Airframe system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures 
Rectification requirements are determined 
System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety 
Rotor and rotor system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE 
Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures 
Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices 
Rotor or rotor system component to be installed is checked to confirm correct part or model numbers, modification status and serviceability 
Mass balance of rotor blades/head is checked in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices 
Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices 
Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage 
System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety 
Rotary wing flight control system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE 
Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures 
Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices 
Rotary wing flight control system components to be installed are checked to confirm correct part or model numbers, modification status and serviceability 
Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices 
Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage 
System is rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety 
Airframe system component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE 
Required maintenance documentation is accurately completed and correctly processed 
Removed components are tagged, sealed and packaged in accordance with specified procedures 
Components to be installed are checked to confirm correct part numbers, serviceability and modification status 
Mass balance of control surfaces to be installed is checked in accordance with the applicable maintenance manual, if required 
Installation is carried out in accordance with the applicable maintenance manual 
Required maintenance documentation is completed and processed in accordance with standard enterprise procedures 

Forms

Assessment Cover Sheet

MEA352 - Maintain basic rotary wing aircraft systems
Assessment task 1: [title]

Student name:

Student ID:

I declare that the assessment tasks submitted for this unit are my own work.

Student signature:

Result: Competent Not yet competent

Feedback to student

 

 

 

 

 

 

 

 

Assessor name:

Signature:

Date:

Assessment Record Sheet

MEA352 - Maintain basic rotary wing aircraft systems

Student name:

Student ID:

Assessment task 1: [title] Result: Competent Not yet competent

(add lines for each task)

Feedback to student:

 

 

 

 

 

 

 

 

Overall assessment result: Competent Not yet competent

Assessor name:

Signature:

Date:

Student signature:

Date: