Assessor Resource

MEA367A
Repair_modify aircraft composite structure using cold bonding

Assessment tool

Version 1.0
Issue Date: May 2024


This unit requires application of hand skills and the use of maintenance publications, applicable materials, tools and methods to repair aircraft composite material structure and components using cold cure repair techniques.

Applications include composite material structure and components from fixed and rotary wing aircraft either on-aircraft or in the workshop.

This unit of competency is part of the Aeroskills Structures Maintenance Certificate IV training pathway, and of the Mechanical Certificate IV (Aircraft Maintenance Stream) training pathways. It covers the competencies required for the repair or modification using cold bonding methods of fixed and rotary wing aircraft structural components that are made from composite materials. The unit is used in workplaces that operate under the airworthiness regulatory systems of the ADF and CASA.

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

Prerequisites

MEA401C Inspect aircraft structures

OR

MEA339C Inspect, repair and maintain aircraft structures

OR

MEA363B Inspect, repair and maintain structures and related components of non-pressurised small aircraft

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 and use maintenance publications, applicable materials, tools and methods to repair aircraft composite material structure and components using cold cure adhesives while applying all relevant safety procedures.

Critical aspects for assessment and evidence required to demonstrate competency in this unit

The underlying skills inherent in this unit should be transferable across the range of different material applications applicable to cold curing. It is essential that specific aspects of the laying up and curing process for aircraft composite materials are checked to ensure quality and safety standards are achieved in this area. Correct checking and wearing of PPE is critical.

Evidence of knowledge about repair techniques and the use of the standard repair manual in a range of different repair situations will be necessary to supplement evidence of ability to plan and undertake component repair. Ability to apply different materials and curing cycles, including composite to composite and composite to metal components, will be necessary to indicate competency in preparing and curing composite materials.

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 using materials from each of Groups 1 and 2 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 workplace or simulated workplace. It is also expected that general purpose tools and test equipment found in most routine situations would be used where appropriate.

Method of assessment

Guidance information for assessment

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.

Look for evidence that confirms knowledge of:

aircraft construction principles and the causes of structural damage, including metal fatigue and corrosion

structural fatigue preventative measures

composite terminology and materials used in both hot and cold bonding

composite component construction and repair methods including structural assembly fastener types, specifications and identification

procedures for the design and approval of repair schemes and modifications

composite material storage requirements

sealants used in aircraft structure and their application and handling

paints and finishes for composite structure

OHS precautions associated with repair of aircraft structure

MSDS

PPE

Look for evidence that confirms skills in:

applying relevant OHS procedures, including the use of MSDS and applicable items of PPE

using approved maintenance documentation and aircraft publications relating to aircraft structure

identifying composite component applications in aircraft structures

identifying various aircraft composite materials/resins and their basic properties by interpretation of markings and visual means

handling and storing of composite materials to industry standards

assessing composite component damage using visual and tap test methods

relative advantages and disadvantages of hot and cold cure

performing composite component repairs using cold cure adhesives:

external patch repair

scarf repair

stepped repair

wet lay up repair

composite fastener hole repair

metal to metal and metal to composite bonding

correctly interpreting and/or producing repair scheme/modification drawings/sketches

using appropriate hand tools and machines to disassemble and assemble aircraft composite components, parts, sections and skin, including extraction/installation equipment, drilling/cutting equipment, and material fastener

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

Applicable materials and methods

Applicable materials and methods include:

1. Cold cure or wet lay-up (using either fibreglass or carbon graphite)

2. Core materials (using one of aluminium, nomex, or foam)

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
Extent of damage is correctly assessed to assist in determining repair procedure 
Structure is supported and prepared in accordance with the applicable maintenance manual to ensure personnel safety and freedom from damage 
Appropriate modification or repair scheme is identified in accordance with structural repair manual and/or approved data 
Specialist advice is obtained in establishing an approved repair scheme where a standard repair scheme cannot be identified or damage criteria are out of limits 
All materials and equipment required are organised 
Lay-up of materials is checked to confirm that components meet required specifications and bagging equipment is correctly installed and operated 
Curing cycle is regularly monitored to ensure required specifications are met 
Components are checked for blemishes or delamination in accordance with quality procedures 
Component assemblies requiring further or special treatment are made ready for the appropriate processes 
Required maintenance documentation is completed and processed in accordance with standard enterprise procedures 
Completed assemblies are tagged, sealed or packaged as required 

Forms

Assessment Cover Sheet

MEA367A - Repair_modify aircraft composite structure using cold bonding
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

MEA367A - Repair_modify aircraft composite structure using cold bonding

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: