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Elements and Performance Criteria

  1. Inspect aircraft structure
  2. Prepare to undertake repair
  3. Repair and maintain aircraft structure

Range Statement

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.

Inspection of aircraft structure 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 non-destructive testing (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

Damage or defects include:

Impact damage

Fatigue cracking

Corrosion

Delamination of composites and bonded structures

Structural repairs include:

Remove corrosion by chemical and mechanical methods

Restore protective coatings

Apply sealants and jointing compounds

Freehand precision hole generation

Remove and install structural hardware and fastening devices

Remove and replace bushes, bearings and bearing surfaces

Metal scab patch, flush, splice, lap and formed section repair

Composite external patch, scarf, stepped and bolted repairs

Specialist advice is obtained from:

Supervisors

Specialist structures personnel

Relevant maintenance documentation includes:

Servicing schedules

Maintenance manuals

Applicable Defence regulations and instructions

Procedures and requirements include:

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


Performance Evidence

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 MSDS and selection and use of applicable items of PPE

demonstrating appropriate cleaning procedures to enable structure inspection

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

identifying damage to aircraft metallic (ferrous and non-ferrous) structures and/or components by way of impact, fatigue or the various types of corrosion

inspecting damage and assessing composite components/structures

identifying various aircraft metals and their basic properties

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

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

using appropriate hand tools and machines, including riveting equipment, drilling equipment, aligning tools and material fasteners (grip pins)

applying correct removal, installation and repair techniques for:

a range of rivets (blind and solid) using hand, squeeze and pneumatic situations

a range of close tolerance fasteners (standard and oversize – hillocks and taper locks), including hole preparation

threaded devices, including internal and external thread cutting, Helicoil inserts and damaged stud replacement

hardware assembled by close tolerance fits using heat, cooling and force methods, including bearings, bushes and inserts

performing a range of metal structure and composite material repair techniques, including:

metal scab patch, flush, splice, lap and formed section repair

composite external patch, scarf and stepped repairs

bolted repairs to composite skin

metal to metal and metal to composite bonding

applying structural corrosion removal/treatment techniques

restoring aircraft structure sealing and surface finishes.

It is essential that the procedures take into account all aircraft and personal safety precautions relating to aircraft structure.

Evidence of transferability of skills and knowledge related to inspection, testing and repair of aircraft structure is essential. This shall be demonstrated through application across a number of different aircraft components as listed in the Assessment Conditions.

Ability to interpret inspection and repair procedures and specifications and apply them in practice is critical. The application of the procedures should also clearly indicate knowledge of structural flight loads and aerodynamic requirements.


Knowledge Evidence

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:

applicable WHS procedures, including the use of MSDS and PPE

construction methods and materials used in:

fuselage sections

wing sections

engine nacelles and mounts

windows and window frames

doors, locks and access panels in pressurised and non-pressurised aircraft

definition 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

potential causes of structural failure

NDT methods and application of the various techniques

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

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

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

the terms associated with composite materials

requirements for handling and storing aircraft metals and composite materials, including sealing agents, to industry standards

means of identifying aircraft structural assembly fasteners (metal and composite) by interpretation of markings, numbering systems, size, shape and colour

assessment of structural damage:

types and classes of mechanical damage

types of corrosion and determining the extent of damage

relevant documentation and manuals

damage limits and repair schemes for metallic and non-metallic structure

procedures for the fabrication and fitment of metal repairs:

scab patch

flush patch

splice

lap

formed section

corrosion removal and passivation

procedures for performing composite repairs:

external patch

scarf patch

stepped repairs

bolted repairs

repair of integral fuel tanks and sealing of faying surfaces, including specific WHS and PPE requirements

surface finishes and methods of restoration, including specific WHS and PPE requirements

how to obtain MSDS

relevant maintenance and structural repair manuals

relevant regulatory requirements and standard procedures.