List the assessment methods to be used and the context and resources required for assessment. Copy and paste the relevant sections from the evidence guide below and then re-write these in plain English.
Elements describe the essential outcomes. | Performance criteria describe the performance needed to demonstrate achievement of the element. |
1. | Inspect light aircraft AC instrument systems, power supplies 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 | AC instrument system and AC power supply components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual while observing all relevant work health and safety (WHS) requirements |
| | 1.4 | Defects are correctly identified and reported |
2. | Test/adjust light aircraft AC instrument systems, power supplies 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 and AC power supply 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 light aircraft AC instrument systems, power supplies 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, using test sets, downloaded maintenance data and fault-finding charts or similar, to line replacement level |
| | 3.3 | Specialist advice is obtained, where required, to assist with the troubleshooting process |
| | 3.4 | Instrument system or power supply 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 light aircraft AC instrument system, and power supply 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 or power supply component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements |
| | 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 or power supply components to be installed are checked to confirm correct part numbers, modification status, serviceability and shelf life |
| | 4.6 | Physical installation of instrument or power supply 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 |
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 include:
using approved maintenance documentation and aircraft publications relating to AC instrument systems and related AC power supplies
locating and identifying AC powered instrument system components including:
AH, DG, AHRS, servo and encoding altimeters
engine system temperature, speed, oil pressure, torque and manifold pressure
auxiliary systems, including vacuum, fuel storage quantities and fuel flow
remote reading gyro compasses
locating and identifying AC instrument power supply system components, including:
inverters
transformer/rectifier units
voltage and frequency indication
correctly handling and observing maintenance precautions for gyroscopes and gimbals
recognising system and component defects/external damage, correct installation, connection of plugs, terminations, attaching hardware (including cabling/harnesses) and security in AC powered instruments and related power supply, including:
flight instruments
remote reading gyro compasses
piston engine and gas turbine engine indication systems (indicators and transmitters/sensors)
fuel quantity and flow indication systems (indicators, probes and transmitters)
transmitter/indicator measuring instrument systems (pressure, temperature and vacuum)
AC power supply, including inverters and transformer/rectifier units
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 WHS requirements relevant to instrument and electrical system maintenance.
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 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 AC powered aircraft instrument systems, AC power supplies and components listed in the Assessment Conditions.
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:
component attachment methods
connection of hardware and plugs
handling precautions for electrostatic sensitive devices
relevant WHS practices
AC theory:
calculations and measurement in AC circuits
inductors and inductive reactance
transformer operation
capacitors and capacitive reactance
LCR circuits and resonance
passive filters
power relationship in reactive circuits
the basic layout (block diagram level), function and operation of AC powered:
flight instruments
remote reading gyro compasses
piston engine and gas turbine engine indication systems (indicators and transmitters/sensors)
fuel quantity and flow indication systems (indicators, probes and transmitters)
transmitter/indicator measuring instrument systems (pressure, temperature and vacuum)
AC power supply including AC generators, inverters and transformer/rectifier units
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 instrument systems
gyroscopes and their use in aircraft instrument systems
electrical fundamentals
relevant maintenance documentation and maintenance publications
maintenance requirements and troubleshooting procedures.
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 applicable general-purpose tools and test equipment found in most routine situations 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 the following groups:
DG, AH, AHRS and components, servo and encoding altimeters, remote reading gyro compasses and components
piston engine and gas turbine engine indication system components
fuel quantity indication and flow indication systems and components
transmitter/indicator measuring instrument systems (pressure, temperature, vacuum) and components
inverters and transformer/rectifier units.
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.