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Follow the links below to find material targeted to the unit's elements, performance criteria, required skills and knowledge

Elements and Performance Criteria

  1. Inspect basic aircraft instrument systems and components
  2. Test/adjust basic aircraft instrument systems and components
  3. Troubleshoot basic aircraft instrument systems and components
  4. Remove and install basic aircraft instrument system components

Required Skills

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 pitotstatic systems connections heating and protrusions

recognising system and component defectsexternal damage correct installation connection of plugs terminations attaching hardware including cablingharnesses and security in

flight instruments

pitotstatic 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 postmaintenance 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

pitotstatic 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 counterpointer 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 slipturn 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 pitotstatic system leak testing

relevant maintenance documentation and maintenance publications

relevant regulatory requirements and standard procedures

Evidence Required

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 aircraftsystem faultfinding 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 componentLRU from each of Groups to 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


Range Statement

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