This unit requires application of hand skills and the use of system/component knowledge and applicable test equipment to inspect, test and troubleshoot basic aircraft instrument systems and to remove and install components.

Applications include light fixed wing aircraft with fixed undercarriage and basic rotary wing aircraft with skids or floats and no powered flight controls powered by either a normally aspirated piston engine or small gas turbine.

MEA246C

Fabricate and/or repair aircraft electrical components or parts

1. Inspect basic aircraft instrument systems and components

1.1. Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements

1.2. Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual

1.3. Instrument system components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual

1.4. Defects are correctly identified and reported

2. Test/adjust basic aircraft instrument systems and components

2.1. Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation

2.2. Instrument system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction

2.3. System calibration or adjustments are performed in accordance with maintenance manual, as appropriate

3. Troubleshoot basic aircraft instrument systems and components

3.1. Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination

3.2. Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting

3.3. Specialist advice is obtained, where required, to assist with the troubleshooting process

3.4. Instrument system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures

3.5. Rectification requirements are determined

4. Remove and install basic aircraft instrument system components

4.1. System is rendered safe and prepared in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety

4.2. Instrument component removal is carried out in accordance with the applicable maintenance manual

4.3. Required maintenance documentation is completed and processed in accordance with standard enterprise procedures

4.4. Removed components are tagged and packaged in accordance with specified procedures

4.5. Instrument components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life

4.6. Physical installation of instrument components is performed in accordance with the applicable maintenance manual and regulatory requirements, ensuring appropriate adjustment/alignment is carried out

4.7. System is reinstated to correct operational condition in preparation for testing, as necessary

4.8. Required maintenance documentation is completed and processed in accordance with standard enterprise procedures

Required skills

Look for evidence that confirms skills in:

using approved maintenance documentation and aircraft publications relating to basic instrument systems

locating and identifying flight instrument system components comprising:

engine system temperature, speed (including mechanical and electrical tachometers)

auxiliary direct reading systems including vacuum, fuel storage quantities

flight systems including attitude, altitude, air speed and OAT

locating and identifying direct reading compasses

correct handling and observance of maintenance precautions relating to gyroscopes, gimbals and pitot/static systems (connections, heating and protrusions)

recognising 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

piston engine and gas turbine engine indication systems

electrical systems indication

basic fuel quantity indication systems

vacuum indication systems

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

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

applying OHS requirements relevant to instrument system maintenance

Required knowledge

Look for evidence that confirms knowledge of:

component attachment methods

connection of hardware and plugs

handling precautions for electrostatic sensitive devices

relevant OHS practices

the basic layout (block diagram level), function and operation of the following systems as listed in the Range Statement:

pitot/static systems

piston engine and gas turbine engine direct reading indication systems

basic fuel quantity measurement systems

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

instrument construction and operation:

instrument groupings, panel layout and construction

pitot static instruments (ASI, VSI and counter-pointer altimeters), their operation, calibration safe handling and related terminology

pitot pressure

static pressure

altimeter Q code settings:

QNH

QNE

QFE

IAS

TAS

vacuum system indication component construction and operation

air and electrically powered artificial horizon construction and operation

directional gyro construction and operation

construction and operation of direct reading engine instruments

turn and bank and slip/turn coordinator construction and operation

direct reading compass construction and compass calibration

piston and gas turbine engine direct reading measuring instruments and temperature indication instruments construction and operation

voltage and current measuring instrument construction and operation

volumetric fluid quantity system components, construction and operation

instrument system maintenance requirements and troubleshooting procedures, including pitot/static system leak testing

relevant maintenance documentation and maintenance publications

relevant regulatory requirements and standard procedures

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 inspect, test and troubleshoot basic instrument systems and remove and install components while observing all relevant safety precautions.

Critical aspects for assessment and evidence required to demonstrate competency in this unit

The underlying skills inherent in this unit should be transferable across a range of inspection, testing and troubleshooting applications (including the timely involvement of supervisors or other trades) and component removal and installation associated with aircraft basic instrument systems and components. It is essential that system testing procedures, cleanliness requirements and safety precautions applicable to the system being maintained are fully observed, understood and complied with. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice 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 Range Statement. 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.

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 system and at least one major system component/LRU from each of Groups 1 to 8 listed in the Range Statement. 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

The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance. Bold italicised wording, if used in the performance criteria, is detailed below. 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.

Note

Range statements listed below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide

Applicable instrument systems and system components

Instrument systems and system components include:

1. Pitot/static systems and components, ASI, VSI and counter-pointer altimeters

2. DGs and AHs (air and electrically driven)

3. Turn and bank and slip/turn coordinators

4. Direct reading compasses

5. Piston engine and gas turbine engine indication system components (direct reading measuring instruments and temperature indication)

6. Electrical systems indication (voltage and current)

7. Basic fuel quantity indication systems and components

8. Vacuum indication components

Troubleshooting

Troubleshooting involves the use of fault-finding charts or similar, to line replacement level

Application of this unit may relate to:

scheduled or unscheduled maintenance

individual or team-related activities

Procedures and requirements

Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise

This unit contains employability skills.