Aircraft Mechanics: Avionics

101403 Minor repair for aircraft electrical components or parts 

(ก) ความต้องการด้านทักษะ

See Appendix A

(ข) ความต้องการด้านความรู้

See Appendix A

(a) Performance Evidence

          software management control requirements.

(b) Knowledge Evidence

(c) Assessment  recommendation

          N/A

Assessment methods

(a) Recommendation

          This field allows different environments and working conditions that can affect the performance. the essential operating conditions that may be present (depending on the work situation, accessibility requirements, the candidate of the topic, and local industry and regional contexts) are included.

          Applicable instrument systems and components include:

          • Pitot/static systems and components, airspeed indicators (ASI), vertical speed indicators (VSI), outside air temperature gauges (OAT) and counter-pointer altimeters

          • Directional gyros (DGs) and artificial horizons (AHs) (air and electrically driven)

          • Turn and bank and slip/turn coordinators

          • Direct reading compasses

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

          • Electrical systems indication (voltage and current)

          • Basic fuel quantity indication systems and components

          • Vacuum indication components

          • Electronic flight and engine instruments (where applicable to the enterprise)

          Procedures and requirements include:

          Industry standard procedures specified by manufacturers, regulatory authorities or the enterprise

(b) Description

          N/A

          The assessment are composed of paper exams , interviews, and practical demonstrations, which the paper exam is the main testing. The selection of interviews and practical demonstrations are depending on the assessors’ judgment. Competition should be assessed in the workplace or work environment simulated using tools and equipment specified in the maintenance documentation. It is also expected that the general purpose tools and test equipment found in most routine situations would be used where appropriate.

          The application of the test procedures should clearly indicate the knowledge of system operation, the relationship of the individual components and linkages with other systems (if applicable) within the limits of the aircraft / guidance system troubleshooting before taking any action. The work plan should take into account the applicable safety requirements and quality in accordance with industry and regulatory standards.

The following conditions of assessment represent the requirements of the Regulators 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/LRU from each of the following groups:

          • HF and VHF communication LRUs, transmission lines and antennas

          • ADF, VOR and GNS navigation system LRUs, transmission lines and antennas

          • ATC transponders, transmission lines and antennas

          • ELT

          • ADS-B.

          • 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.