MEA292 — Remove and install advanced aircraft instrument system components
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What an assessment for MEA292 must cover
31 assessable components: 3 elements (10 performance criteria), 15 performance evidence and 6 knowledge evidence requirements. An audit-defensible tool maps every question and task back to these — that mapping is the coverage matrix Auditori generates alongside the assessment.
Elements & performance criteria
1 Remove advanced aircraft instrument system components
- 1.1Render system safe and prepare for removal according to applicable maintenance manual
- 1.2Fit isolation tags, where necessary, to ensure personnel safety
- 1.3Remove instrument component according to applicable maintenance manual and work health and safety (WHS) requirements
- 1.4Complete required maintenance documentation and process according to standard organisational procedures
- 1.5Tag and package removed components according to specified procedures
2 Install advanced aircraft instrument system components
- 2.1Check instrument components to be installed to confirm correct part numbers, modification status, serviceability, and shelf life
- 2.2Perform physical installation of instrument components according to maintenance manual and regulatory requirements, and carry out required adjustment and alignment
- 2.3Reinstate system to correct operational condition in preparation for testing, as necessary
3 Finalise removal and installation documentation
- 3.1Complete required maintenance documentation
- 3.2Process maintenance documentation according to organisational procedures
Performance evidence
- pitot/static system components, airspeed indicators (ASIs), vertical speed indicators (VSIs), air data system components, machmeters, altimeters, including servo and encoding altimeters, outside air temperature gauge (OAT) angle of attack and stall warning/avoidance systems
- turn and slip, directional gyros (DGs), artificial horizons (AHs), attitude and heading reference system (AHRS) components where applicable to organisation, remote reading gyro compass system components, and direct reading compasses
- turbine engine indication system
- transmitter/indicator measuring instrument systems (pressure, temperature, and position)
- fuel quantity indication and flow systems components
- ground proximity warning system (GPWS), which may be omitted where not applicable to the organisation
- flight data recorder (FDR), which may be omitted where not applicable to the organisation.
- prepare for work in line with safety and quality requirements and according to industry, regulatory and organisational requirements, procedures, and methods
- locate and identify flight instrument system components comprising: engine system temperature, pressure (including thermocouples, sensor units, and transmitters), speed (including mechanical or electrical tachometers), thrust (fan, propeller and jet), torque, fuel flow, and vibration; auxiliary systems, including hydraulic pressure and temperature, transmission pressure and temperature, fuel storage quantities, fuel remaining/used, component position, i.e. flaps, landing gear, speed brakes and door/pylon locking; flight systems, including attitude, altitude, air speed, OAT and GPWS (where applicable to the enterprise)
- locate and identify direct reading compasses, remote compass system components (flux valve, gyro, amplifier and indicator), and AHRS components
- locate and identify FDR system components (where applicable to the organisation)
- apply correct handling procedures and maintenance precautions relating to gyroscopes, gimbals, pitot/static systems (connections, heating and protrusions)
- apply required work health and safety (WHS) practices
- complete and process maintenance documentation
- comply with cleanliness requirements and safety precautions applicable to system being maintained, as well as with work practices associated with electrostatic sensitive devices.
Knowledge evidence
- industry standard procedures specified by manufacturers, regulatory authorities, and the organisation relating to the work described in the performance evidence
- maintenance manual requirements relating to: performing physical installation of instrument components; rendering system safe for removal; removing instrument components; adjusting and aligning instrument components and systems
- industry, regulatory and organisational requirements, procedures and methods relating to the work described in the performance evidence, including: WHS processes and practices, including handling precautions for electrostatic sensitive devices; completing and processing required maintenance documentation; tagging and packaging removed components; attaching components, including attachment methods; connecting hardware and plugs; adjusting and calibrating system operation
- using approved maintenance documentation and aircraft publications relating to basic and advanced instrument systems
- operating principles of basic instrument systems and components, including: atmospherics and barometry; terminology and unit of measurement conversion; aircraft instrumentation requirements; instrument panel layout; pressure sensing elements; pitot static systems and testing requirements; gyroscopic principles; direct reading compasses; temperature sensors; fluid quantity indication systems
- general layout and components of the following systems: flight systems, including: altitude (direct reading, servo and encoding altimeters); attitude, including DG and AH (both air and electrically driven) and turn and slip, and AHRS; airspeed, including ASI, machmeters and air data systems; VSI; angle of attack and stall warning/avoidance; OAT; GPWS; engine indication systems, including: temperature and pressure, including thermocouples, sensors, and transmitters; speed, including mechanical and electric tachometers; thrust, including fan, propeller and jet; torque; fuel flow; vibration; auxiliary transmitter/indicator measuring systems, including: hydraulic pressure and temperature; pneumatic pressure; transmission oil pressure and temperature; fuel remaining/used; fuel quantity indication; component position; remote compass systems; FDR systems.
Unit content sourced from training.gov.au — © Commonwealth of Australia, licensed under CC BY 4.0. Auditori is not affiliated with the Department of Employment and Workplace Relations.
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Questions about assessing MEA292
What does an assessment tool for MEA292 need to cover?
To satisfy the Principles of Assessment and Rules of Evidence, an assessment for MEA292 needs to address all 31 unit components: 3 elements with 10 performance criteria, 15 performance evidence requirements, 6 knowledge evidence requirements, and the foundation skills. A coverage matrix mapping each question and task to these components is what an auditor looks for.
How does Auditori generate an assessment tool for MEA292?
Auditori pulls the current release of MEA292 from training.gov.au and generates a complete package: candidate assessment, assessor guide with model answers and observation criteria, and a coverage matrix mapping every component. A suitably qualified person then reviews and approves the draft in a built-in workflow — consistent with ASQA's guidance on AI use in VET — before export as branded PDF and editable Word.
Is the first assessment tool really free?
Yes. Every new account includes one free credit — enough to generate the complete assessment tool for MEA292 — with no card and no subscription required. After that it's pay-as-you-go per unit.
Can I check my existing MEA292 assessment instead of generating a new one?
Yes — upload your existing assessment or learner guide and Auditori maps it against every element, performance criterion, PE and KE of MEA292, showing exactly what's covered and what's missing. Mapping costs a quarter of a credit.
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