Unit of competency Outline

Date retreived
22/07/2026 9:48 AM AWST

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Maintain aircraft non-primary structural removable components or parts and internal fittings

Maintain aircraft non-primary structural removable components or parts and internal fittings

Unit of competency
National Code
MEA330
State Code
AUF33
TGA Status
Replaced
DTWD Status
Replaced
Current Release Number
2.00
Current Release Date
31/08/2018
View on TGA
State Implementation and Classification
Approved Date
22/07/2015
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
22/07/2015
Nominal Hours
60
Description
This unit of competency requires application of hand skills and use of maintenance documentation to dismantle, inspect, maintain and assemble aircraft non-primary structural removable components and interior fittings/emergency equipment during scheduled or unscheduled maintenance under the guidance of a qualified person. Work under the guidance of a qualified person may be performed individually or as part of a team.Applications include fixed and rotary wing aircraft components either attached to the aircraft or in a workshop.The unit is part of a Mechanical Certificate II training pathway.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).
Notes
Elements and Performance Criteria
1. Prepare to dismantle, inspect, maintain and assemble non-primary structural removable components or parts and internal fittings
  • 1.1 Components are removed and/or disassembled in accordance with enterprise procedures, relevant maintenance documentation and qualified person guidance 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)
  • 1.2 Maintenance and/or repair requirements as defined by the qualified person, enterprise procedures and the relevant maintenance documentation are understood
  • 1.3 Tagging and repair instructions are accurately specified in accordance with enterprise procedures and qualified person directions for parts requiring specialist repair
  • 1.4 Appropriate materials, tools, equipment and assembly or fabrication jigs, where applicable, are selected and prepared for the particular maintenance and repair requirements in accordance with enterprise procedures and relevant maintenance documentation
2. Dismantle, inspect, maintain and assemble non-primary structural removable components or parts and internal fittings
  • 2.1 Routine maintenance, repair or modification processes are carried out as approved by relevant manufacturers’ bulletins or procedures, in accordance with required enterprise procedures and specifications while observing all relevant WHS requirements, including the use of MSDS and items of PPE
  • 2.2 Component parts are assembled within specified tolerances in accordance with enterprise procedures and the appropriate maintenance documents
  • 2.3 Where applicable and as required by the qualified person, assistance is provided in the conduct of final load or functional tests
3. Complete maintenance/ modification activities
  • 3.1 Required documentation is completed and processed in accordance with standard enterprise procedures
  • 3.2 Where applicable, maintained/repaired or modified components are tagged, sealed and packaged within specified procedures
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