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Follow the links below to find material targeted to the unit's elements, performance criteria, required skills and knowledge

Elements and Performance Criteria

  1. Interpret specifications and organise materials
  2. Prepare material and tooling
  3. Form material
  4. Hand correct fabricated components
  5. Inspect components

Required Skills

Look for evidence that confirms knowledge of

aircraft construction principles

causes of structural fatigue and preventative measures

structural corrosion and preventative measures

aircraft structural drawings and repair scheme drawings

material specifications for aluminium alloys and steel alloys used in aircraft structure

structural material identification by markings and numbering systems

material identification by chemical electrical and mechanical methods

material storage requirements

hardware types and specifications

identification of hardware

sealants used in aircraft structure

chemical surface treatments

electroplating

paints and finishes

flat pattern development

design and manufacture of templates

design and manufacture of press tools

methods for folding complex and nested sections

machinery used for stretching shrinking bending cutting drilling rolling wheeling and folding

use of forming blocks templates and press tools to form components

OHS precautions associated with fabrication of aircraft structural components

MSDS

PPE

Look for evidence that confirms skills in

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

the use of approved maintenance documentation and aircraft publications relating to aircraft structure

identifying various aircraft metals and their basic metallurgy properties by interpretation of markings numbering systems or visual chemical or mechanical means

handling and storing aircraft metals to industry standards

identifying aircraft structural assembly fasteners by interpretation of markings numbering systems size shape and colour

fabrication of aircraft structural components and parts by

correctly interpreting drawings including third angle projection isometric sectional formats and hand sketches

developing component flat pattern using basic drawing tools geometric drawing processes parallel radial and triangulation methods calculating and applying bend allowancedeductionsetback an understanding of flat pattern development terminology is required

using appropriate hand tools machines stretching shrinking bending cutting drilling rolling wheeling and folding forming blocks templates and presses to formproduce dished domed curved components bentangled L Z U hat sections and lightening holes flanges and joggles

assembling component parts using appropriate hand and machine tools and standard aircraft fasteners to industry standards

applying appropriate metal heat treatment processes

applying appropriate metal surface treatments

Evidence Required

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 drawings specifications maintenance publications and applicable machinery to fabricate advanced structural components from a range of aircraft metals 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 aircraft applications It is essential that procedures take into account all safety precautions and quality requirements Skill and knowledge application must include flat pattern development and other standard practices associated with forming of material

Evidence of knowledge and skills associated with the broad range of structural fabrication techniques and their application to different materials used in aircraft manufacture will be required to supplement evidence of ability to fabricate components

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 a representative range of structural fabrication tasks 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 by aircraft maintenance manuals It is 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


Range Statement

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.

Components

Components are to be fabricated:

using materials comprising various types of sheet metal used in aircraft manufacture, including aluminium alloys and structural steel alloys across a range of temper

Machinery processes

Machinery processes are to include:

bending, cutting, rolling, shrinking and stretching

Procedures and requirements

Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise