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Elements and Performance Criteria

  1. Prepare to evaluate structure
  2. Identify principles and techniques required for evaluation of aircraft structure
  3. Evaluate aircraft structure and structural components
  4. Report results

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.

Aircraft structure includes:

Primary structure

Secondary structure

Tertiary structure

Assembly and attachment hardware

Aircraft structural components include:

Fuselage

Wings

Tailplane

Fin

Flight control surfaces

Flaps

Doors

Access panels

Engine nacelles

Pylons

Fairings

Windscreens and windows

Bearings, assembly and attachment hardware

Standards and guidance material include:

ADF AAP7001 .054 Airworthiness Design Requirements Manual

FAR Part 23 Airworthiness Standards for Airplanes in the Normal, Utility, Aerobatic or Commuter Categories

FAR Part 25 Airworthiness Standards for Airplanes in the Transport Category

EASA CS-23 Certification Specifications for Aeroplanes in the Normal, Utility, Aerobatic or Commuter Categories

EASA CS-25 Certification Specifications for Airplanes in the Transport Category

CASA AC21.16(0) Approval of material, parts, processes and appliances

CASA AC21.145(0) Manufacture of parts during the course of maintenance

CASA AC21.601(0) Australian Technical Standards Order Authorisation

CASA CAAP35 -7(0) Design approval of modifications and repairs

CASA AC 21-99 Aircraft Wiring and Bonding

FAA AC 43-13-1B Acceptable Methods, Techniques and Practices – Aircraft Inspection and Repair

MIL-HDBK-1530A (USAF) Aircraft Structural Integrity Program General Guidelines For

Configuration management (CM)

CM is a process for control and documentation of the design and development process and for the management of system, component and software throughout the service life

Integrated logistic support (ILS)

ILS is an integrated approach to the management of logistic disciplines originally developed for the management of military systems from design concept to final disposal at life-of-type. It covers:

reliability engineering, maintainability engineering and maintenance planning

supply and support

support and test equipment

manpower and personnel

training and training support

technical data and publications

computer resources support

facilities

packaging, handling, storage and transportation

design interface

Appropriate technical and professional assistance includes:

Assistance from individuals with CASA maintenance certification licenses or those with supervisory authorisations in the ADF regulatory system

Professional support from engineers employed within:

organisations with CASA continuing airworthiness management or maintenance approvals

approved engineering organisations under the ADF regulatory system

Engineers employed within organisations recognised by overseas airworthiness organisations

WHS, regulatory requirements and enterprise procedures include:

WHS Acts and regulations

Relevant standards

Industry codes of practice

Risk assessments

Registration requirements

Safe work practices

Civil Aviation Safety Regulations

AAP7001 .053 ADF Technical Airworthiness Management Manual

Overseas airworthiness authorities, where applicable, e.g. Federal Aviation Administration, Transport Canada, European Aviation Safety Agency


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:

identifying WHS, regulatory and risk management procedures, structural design and construction principles, and ageing aircraft structure inspection and maintenance requirements

determining and confirming:

parameters and context of tasks

chain of responsibility

personal functions and responsibilities

team and support functional group interdependencies and communications

appropriate qualifications and delegations

appropriate support, including technical and professional assistance

investigating associated CM and ILS requirements and drafting required data

assessing and applying:

basic aircraft structural analysis and design procedures

design standards

regulatory requirements

graphics skills and techniques

evaluating proposed modification and repair schemes

reporting and documenting results of scoping, principles and techniques identification and evaluation of applications.


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:

aircraft structural design and construction:

design standards and manufacturer’s stress analysis

structural materials

structural hardware

construction and assembly methods

sealants and surface finishing schemes

basic design principles for:

structural modifications

repair schemes and extensions to existing schemes

ageing aircraft structural inspection and maintenance requirements

airworthiness regulator design standards

compliance requirements of the WHS Act and regulations, codes of practice, standards and risk assessment

scope of trade, technical and professional support services required in aircraft structural applications

management data interface with CM and ILS.