Assessor Resource

MEA401
Inspect aircraft structures

Assessment tool

Version 1.0
Issue Date: May 2024


This unit of competency requires application of hand skills and use of maintenance documentation and manuals to inspect aircraft structure and identify damage and deterioration during scheduled or unscheduled maintenance. Work may be performed individually or as part of a team.

Applications include the structure of fixed and rotary wing aircraft.

The unit is part of the Aeroskills Structures Maintenance Certificate IV and of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathways.

The unit is used in workplaces that operate under the airworthiness regulatory systems of the Australian Defence Force (ADF) and the Civil Aviation Safety Authority (CASA).

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



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 aircraft structure

1.1

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

1.2

Appropriate preparation and access to the aircraft structure is undertaken to allow for proper inspection in accordance with maintenance documentation 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

Aircraft structure is visually or physically checked for signs of deformation, defects or damage in accordance with maintenance documentation and approved procedures while observing all relevant WHS requirements, including the use of MSDS and items of PPE

1.4

Damage or defects are assessed against damage or wear limits specified by structural repair manual or other approved data to determine if repair or replacement is required

1.5

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:

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

using approved maintenance documentation and aircraft publications relating to aircraft structure

identifying various aircraft metals and their basic properties

identifying potential causes of structural failure

demonstrating appropriate cleaning procedures to enable structure inspection

demonstrating correct inspection procedures, in particular pressurised aircraft, in accordance with aircraft and procedures manuals

performing aircraft mensuration and alignment checks

identifying damage to aircraft metallic (ferrous and non-ferrous) structures and/or components by way of:

impact

fatigue

corrosion

identifying the various forms of structural corrosion, stating the causes and structural effects of corrosion on aircraft

identifying composite materials used in aircraft construction, associated safety precautions and hazards

inspecting damage and assessing composite components/structures for:

impact damage

fatigue.

The underlying skills inherent in this unit should be transferable across a range of structural inspections associated with aircraft maintenance. It is essential that the procedures take into account all aircraft and personal safety precautions relating to aircraft structure.

Evidence is required of the ability to interpret and apply aircraft structural inspection requirements. This may be demonstrated through application across a range of structural components and materials. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical. The application of the procedures should also clearly indicate knowledge of structural flight loads.

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:

aircraft construction principles

structural component attachment methods

describing the construction methods used in:

fuselage sections

wing sections

engine nacelles and mounts

windows and window frames

doors, locks and access panels in pressurised and unpressurised aircraft

defining of structural terms, i.e. safe life, damage tolerant, failsafe, stress, strain, shear and cycles

inspection requirements for metal and composite structure, including:

ageing aircraft inspection requirements

safe life structure

damage tolerant structure

fail safe structure

procedures and methodology for performing aircraft mensuration and alignment checks

describing NDT methods and application of the various techniques

describing construction methods of, and assessing common defects in, aircraft plastic transparencies

describing basic constructional features of, and assessing common defects in, glass windscreens

defining the terms associated with composite materials

WHS procedures

relevant PPE

how to obtain MSDS.

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

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 the unit of competency are being achieved under routine supervision on at least one (1) task from each of the following groups:

preparation for non-destructive testing (NDT) (access to relevant structural zones and components)

inspection of:

non-ferrous and ferrous alloys and composite (FRP) materials used in aircraft construction

structural fastening and attachment hardware and/or devices

seals and sealants

glass and moulded plastics

application of NDT techniques

doors, hinges and locking mechanisms for damage/misalignment

inspections applicable to each of safe life, damage tolerant and fail safe structure relevant to enterprise

ageing aircraft inspection programs.

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).


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.

Elements describe the essential outcomes.

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

1.

Inspect aircraft structure

1.1

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

1.2

Appropriate preparation and access to the aircraft structure is undertaken to allow for proper inspection in accordance with maintenance documentation 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

Aircraft structure is visually or physically checked for signs of deformation, defects or damage in accordance with maintenance documentation and approved procedures while observing all relevant WHS requirements, including the use of MSDS and items of PPE

1.4

Damage or defects are assessed against damage or wear limits specified by structural repair manual or other approved data to determine if repair or replacement is required

1.5

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.

Preparation and access to structure includes:

Preparation for non-destructive testing (NDT) (access to relevant structural zones and components)

Aircraft structure inspection includes:

Non-ferrous and ferrous alloys and composite (FRP) materials used in aircraft construction

Structural fastening and attachment hardware and/or devices

Seals and sealants

Glass and moulded plastics

Application of NDT techniques

Doors, hinges and locking mechanisms for damage/misalignment

Inspections applicable to each of safe life, damage tolerant and fail safe structure relevant to enterprise

Ageing aircraft inspection programs

Inspection techniques include:

Visual inspection, physical checks, mensuration and alignment

Procedures and requirements include:

Industry standards specified by manufacturers, regulatory authorities or the enterprise

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:

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

using approved maintenance documentation and aircraft publications relating to aircraft structure

identifying various aircraft metals and their basic properties

identifying potential causes of structural failure

demonstrating appropriate cleaning procedures to enable structure inspection

demonstrating correct inspection procedures, in particular pressurised aircraft, in accordance with aircraft and procedures manuals

performing aircraft mensuration and alignment checks

identifying damage to aircraft metallic (ferrous and non-ferrous) structures and/or components by way of:

impact

fatigue

corrosion

identifying the various forms of structural corrosion, stating the causes and structural effects of corrosion on aircraft

identifying composite materials used in aircraft construction, associated safety precautions and hazards

inspecting damage and assessing composite components/structures for:

impact damage

fatigue.

The underlying skills inherent in this unit should be transferable across a range of structural inspections associated with aircraft maintenance. It is essential that the procedures take into account all aircraft and personal safety precautions relating to aircraft structure.

Evidence is required of the ability to interpret and apply aircraft structural inspection requirements. This may be demonstrated through application across a range of structural components and materials. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical. The application of the procedures should also clearly indicate knowledge of structural flight loads.

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:

aircraft construction principles

structural component attachment methods

describing the construction methods used in:

fuselage sections

wing sections

engine nacelles and mounts

windows and window frames

doors, locks and access panels in pressurised and unpressurised aircraft

defining of structural terms, i.e. safe life, damage tolerant, failsafe, stress, strain, shear and cycles

inspection requirements for metal and composite structure, including:

ageing aircraft inspection requirements

safe life structure

damage tolerant structure

fail safe structure

procedures and methodology for performing aircraft mensuration and alignment checks

describing NDT methods and application of the various techniques

describing construction methods of, and assessing common defects in, aircraft plastic transparencies

describing basic constructional features of, and assessing common defects in, glass windscreens

defining the terms associated with composite materials

WHS procedures

relevant PPE

how to obtain MSDS.

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

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 the unit of competency are being achieved under routine supervision on at least one (1) task from each of the following groups:

preparation for non-destructive testing (NDT) (access to relevant structural zones and components)

inspection of:

non-ferrous and ferrous alloys and composite (FRP) materials used in aircraft construction

structural fastening and attachment hardware and/or devices

seals and sealants

glass and moulded plastics

application of NDT techniques

doors, hinges and locking mechanisms for damage/misalignment

inspections applicable to each of safe life, damage tolerant and fail safe structure relevant to enterprise

ageing aircraft inspection programs.

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).

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
Relevant maintenance documentation and modification status, including defect reports, where relevant, are used to identify specific inspection requirements 
Appropriate preparation and access to the aircraft structure is undertaken to allow for proper inspection in accordance with maintenance documentation 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) 
Aircraft structure is visually or physically checked for signs of deformation, defects or damage in accordance with maintenance documentation and approved procedures while observing all relevant WHS requirements, including the use of MSDS and items of PPE 
Damage or defects are assessed against damage or wear limits specified by structural repair manual or other approved data to determine if repair or replacement is required 
Maintenance documentation is completed and processed in accordance with standard enterprise procedures 

Forms

Assessment Cover Sheet

MEA401 - Inspect aircraft structures
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

MEA401 - Inspect aircraft structures

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: