Assessment Requirements for MEA212 Inspect, test and troubleshoot basic aircraft instrument systems and components

Release: 3

Assessment Requirements for MEA212 Inspect, test and troubleshoot basic aircraft instrument systems and components

Modification History

Release 3. Equivalant to MEA212 Inspect, test and troubleshoot basic aircraft instrument systems and components with amended prerequisite codes.

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:

recognition of system and component defects/external damage, correct installation, connection of plugs, terminations, attaching hardware (including cabling/harnesses) and security in:

flight instruments

pitot/static systems

direct reading compasses

remote reading gyro compass systems (may be omitted if not relevant to the enterprise)

piston engine indication systems

gas turbine engine indication systems (may be omitted if not relevant to the enterprise)

electrical systems indication

basic fuel quantity indication systems

pneumatic/vacuum indication systems

applying logic processes, taking and interpreting system measurements, using test equipment and appropriate wiring diagrams and manuals to isolate instrument system malfunctions in the above systems

performing system functional tests and checks to isolate system faults and assess post-maintenance serviceability

applying WHS requirements relevant to instrument system maintenance.

It is essential that system testing procedures, cleanliness requirements and safety precautions applicable to the instrument system being maintained are fully observed, understood and complied with. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice across a range of inspection, testing and troubleshooting applications (including the timely involvement of supervisors or other trades) is critical.

Evidence of transferability of skills and knowledge related to inspection, testing and troubleshooting is essential. This is to be demonstrated through application across a range of basic aircraft instrument systems and components listed in the Assessment Conditions.

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:

the basic layout (block diagram level), function and operation of:

flight systems, including:

altitude (direct reading altimeters)

attitude including DGs and AHs (both air and electrically driven), turn and slip and turn coordinator

airspeed

OAT

remote reading gyro compass systems

piston engine indication systems, including:

direct reading temperature

direct reading pressure (e.g. oil pressure)

speed, including mechanical and electric tachometers

manifold pressure/boost, including aneroid, sylphon bellows and dual compartment types

gas turbine engine indication systems, including:

temperature and pressure

speed, including mechanical and electric tachometers

torque

fuel flow

vibration

auxiliary direct reading systems, including:

electrical

hydraulic pressure

pneumatic pressure and vacuum

basic fuel quantity indication

basic instrument system maintenance and testing requirements, and troubleshooting procedures

WHS requirements relevant to instrument system maintenance

the operating principles of the above systems and associated with:

atmospheric conditions; properties and effects on aircraft instruments and systems

pressure and temperature sensing elements and their use in aircraft instruments

gyroscopes and their use in aircraft instrument systems

electrical fundamentals

direct reading compass installations and calibration

calibration of remote reading gyro compass systems

relevant maintenance manuals

relevant regulatory requirements and standard procedures.

Assessment Conditions

Competency should be assessed in the workplace or simulated workplace using tools and equipment specified in the maintenance manuals. It is also expected that general and special purpose tools, and test and ground support equipment would be used where appropriate.

The application of testing procedures should clearly indicate knowledge of system operation, the relationship of individual components and the links with other systems (if applicable) within the limits of the aircraft/system fault finding guide before undertaking any action. The work plan should take account of applicable safety and quality requirements in accordance with the industry and regulatory standards.

The following conditions of assessment represent the requirements of the Regulators (ADF and CASA) and maintenance stakeholders and must be rigorously observed.

A person cannot be assessed as competent until it can be demonstrated to the satisfaction of the workplace assessor that the relevant elements and performance criteria of the unit of competency are being achieved under routine supervision on a system and at least one (1) major system component/line replaceable unit (LRU) from each of:

pitot/static systems and components, ASIs, VSIs, OAT, and counter-pointer altimeters

DGs and AHs (air and electrically driven)

turn and bank and slip/turn coordinators

direct reading compasses

remote reading gyro compass system components (may be omitted if not relevant to the organisation)

piston engine indication system components (direct reading measuring instruments and temperature indication)

gas turbine engine indication system components (may be omitted if not relevant to the organisation)

electrical systems indication (voltage, current, power and frequency)

basic fuel quantity indication systems and components

pneumatic/vacuum indication components.

This shall be established via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry Evidence Guide (for details refer to the Companion Volume Assessment Guidelines).

Assessors must satisfy the requirements of the National Vocational Education and Training Regulator (Australian Skills Quality Authority, or its successors).

Where the unit is to be used for CASA licensing purposes the Assessor must also meet the criteria specified in the CASR Part 147 Manual of Standards.

Individuals being assessed who have already attained MEA275 Maintain basic light aircraft instrument systems and components will have satisfied the requirements of this unit with regard to common range of conditions variables. The Log of Industrial Experience and Achievement records relating to MEA275 Maintain basic light aircraft instrument systems and components may be accepted as also meeting the evidence requirements for this unit in the applicable common areas.

Links

Companion Volume implementation guides are found in VETNet - https://vetnet.education.gov.au/Pages/TrainingDocs.aspx?q=ce216c9c-04d5-4b3b-9bcf-4e81d0950371