Assessor Resource

MEA316C
Inspect, test and troubleshoot rotary wing rotor and control systems and components

Assessment tool

Version 1.0
Issue Date: May 2024


This unit requires application of hand skills, the use of maintenance publications and knowledge of rotors and rotor control system theory to inspect, test and troubleshoot rotors and rotor control systems.

Applications include rotary wing aircraft.

This unit of competency is part of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathway. It covers the competencies required to inspect, test and troubleshoot the rotor and control systems and components of rotary wing aircraft. This unit is used in workplaces that operate under the airworthiness regulatory systems of the ADF and CASA.

Where a CASA licensing outcome is sought this unit forms part of the CASA requirement for the granting of the chosen Aircraft Maintenance Engineer Licence under CASR Part 66, in accordance with the licensing provisions in Section 3, Assessment Guidelines.

You may want to include more information here about the target group and the purpose of the assessments (eg formative, summative, recognition)

Prerequisites

MEA308C

Remove and install rotary wing rotor and flight control system components

Co-Requisites

Not applicable

Employability Skills

This unit contains employability skills.



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.

The Evidence Guide provides advice on assessment and must be read in conjunction with the performance criteria, required skills and knowledge, range statement and the Assessment Guidelines for the Training Package.

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.

Method of assessment

Functional testing of rotors and rotor control systems with engine/s running may be carried out with the applicant directing a pilot qualified on type.

Guidance information for assessment

Individuals being assessed who have already attained MEA352A Maintain basic rotary wing aircraft systems, will have satisfied the requirements of this unit with regard to common Range Statement variables. Log of Industrial Experience and Achievement records relating to MEA352A Maintain basic rotary wing aircraft systems, may be accepted as also meeting the evidence requirements for this unit in the applicable common areas.

Submission Requirements

List each assessment task's title, type (eg project, observation/demonstration, essay, assingnment, 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.

Required skills

Look for evidence that confirms skills in:

applying relevant OHS procedures

using relevant maintenance documentation and aircraft manuals to:

recognise through visual/physical inspection external signs of defects in the rotor, rotor head, tail rotor and flight control mechanical system components

ground test the rotor and control system and recognise correct function

rig and adjust rotor controls and systems

using fault diagnosis guides and equivalent data, to accurately and efficiently troubleshoot the causes of unserviceabilities in rotor control systems, clearly record details and identify the required rectification actions

Required knowledge

Look for evidence that confirms knowledge of:

fault diagnosis techniques

standard trade practices relating to tool and test/rigging equipment usage

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

clutches and freewheeling units

system and component operation, including electrical and instrument system interfaces:

cyclic pitch control

collective pitch control

tail rotor control

mechanical and powered control systems

engine control interface

torque reaction and anti-torque devices

engine indication

vibration monitoring

helicopter maintenance procedures and troubleshooting

relevant maintenance manuals

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

relevant OHS practices

The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance. Bold italicised wording, if used in the performance criteria, is detailed below. Essential operating conditions that may be present with training and assessment (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) may also be included.

Note

Range statements listed below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide

Rotor and rotor control system

Rotor and rotor control system may include:

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 and couplings

Troubleshooting

Troubleshooting involves the use of fault-finding charts or similar, to line replacement level

Application of this unit may relate to:

scheduled or unscheduled maintenance activities

individual or team-related activities

Procedures and requirements

Refer to 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 
Defects are identified and recorded in accordance with standard enterprise procedures 
Aircraft and system 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 
Relevant aircraft publications and modification status, including system defect reports, are interpreted to identify an unserviceability 
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 
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 

Forms

Assessment Cover Sheet

MEA316C - Inspect, test and troubleshoot rotary wing rotor and control systems and components
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

MEA316C - Inspect, test and troubleshoot rotary wing rotor and control systems and components

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: