Unit of competency Outline

Date retreived
22/07/2026 1:28 AM AWST

Whilst all efforts are made to provide accurate and timely information from the relevant source/documentation, please be aware that the information supplied may not be the most current version. The accuracy of the detail has not been confirmed by the Department and therefore should not be relied upon without first confirming the contents.

Assemble aircraft piston engine quick engine change unit

Assemble aircraft piston engine quick engine change unit

Unit of competency
National Code
MEA396A
State Code
WG864
TGA Status
Replaced
DTWD Status
Replaced
Current Release Number
1.00
Current Release Date
23/08/2013
State Implementation and Classification
Approved Date
14/11/2013
Field of Education
031503 - Aircraft Maintenance Engineering
Original Release Date
14/11/2013
Nominal Hours
25
Description
This unit of competency is part of the Mechanical Certificate IV (Component Workshop Maintenance Stream) training pathway. It covers the competencies required to assemble aircraft piston engine quick engine change (QEC) units following engine repair and/or overhaul. 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 assemble piston engine QEC unit
  • 1.1 QEC build requirements are correctly interpreted and matched by part and serial numbers
  • 1.2 Correct QEC components are gathered for assembly and their serviceability state and modification status is confirmed in accordance with the relevant maintenance documentation and quality procedures
  • 1.3 Required hardware and plumbing is obtained and confirmed as approved items
2 Assemble piston engine QEC unit
  • 2.1 Piston engine is prepared for QEC assembly in accordance with maintenance manual and/or enterprise procedures
  • 2.2 QEC components are assembled to the engine and adjusted in accordance with the maintenance manual and/or enterprise procedures
  • 2.3 QEC unit is assembled and components and linkages are adjusted in accordance with maintenance data requirements
  • 2.4 Where required, QEC unit is prepared for testing
The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance. 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.
Piston engine QEC unit components
The build requirements for individual QEC units may include components from the following list:
engine
engine mount frame
external lubrication system components
baffles
heat shields
fuel system plumbing
pneumatic plumbing
control linkages
induction system
exhaust system components
turbocharger and waste gate
tachometer generator and wiring
vacuum pump
air pump
hydraulic pump
fire warning system
Application
Application of this unit may relate to:
scheduled or unscheduled maintenance
individual or team-related activities
complex testing and adjusting of components, and where this is undertaken, may be carried out under supervision at the appropriate level
Procedures and requirements
Procedures and requirements refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise
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 component theory knowledge and use maintenance publications to assemble piston engine QEC units while applying all relevant safety precautions.
Critical aspects for assessment and evidence required to demonstrate competency in this unit
Evidence of transferability of skills and knowledge related to repair and overhaul is essential. This may be demonstrated through application across a number of different piston engine QECs. Ability to assess component serviceability and interpret parts requirements will be necessary to supplement the required evidence. Capability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical. The application of adjustment procedures should also clearly indicate knowledge of system operation. The work plan should take account of applicable safety and quality requirements in accordance with the industry and regulatory standards.
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 the engine types maintained by the enterprise. 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 in maintenance documentation. 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
Replaced By
State Code National Code Title Type
AUF85 MEA396 Assemble aircraft piston engine quick engine change unit Unit of competency
State Code National Code Title Type
D744 MEA40711 Certificate IV in Aeroskills (Mechanical) Qualification