7232 Aircraft engine mechanics and fitters  

N/A

(ก) ความต้องการด้านทักษะ

See Appendix A

(ข) ความต้องการด้านความรู้

See Appendix A

(a) Performance Evidence

      Evidence required to demonstrate competency in this unit should be of interest and meet all requirements of the elements and performance criteria under the specified conditions assessment, and should include: 

•    Identifying / location: 

•    DC power generation systems, regulation, and distribution and control components, ie regulators and busbars systems. 

•    Poiston ignition engines and components, ie coils, magnetos, auxiliary power (links impulses and / inductors vibrators). 

•    Ignition.components gas turbine engine and ignition system (if the company) .

•    Batteries (acid and nickel cadmium, lead) and associated equipment assembly, including anti-vibration related aid. 

•    Motors and actuators on basic electrical systems DC. 

•    Electrical components.

•    Specific DC systems, such as flaps and landing gear.

•    Correctly connect DC generators and generators alternator / rectifier. 

•    Applying relevant practices WHS.  

     It is essential that the cleaning requirements and security measures applicable to the system under maintenance are fully observed, understood and respected, and work practices associated with ESD. Evidence of transferability of skills and knowledge related to the removal and installation is essential. This is to demonstrate for application to a variety of major components of the aircraft electrical power system covering mechanical interface, installations that require alignment and / or adjustment (mechanical or electrical).



(b) Knowledge Evidence

     Evidence required to demonstrate competency in this unit should be of interest and meet all requirements of the elements and performance criteria and include basic knowledge of:

•    Component attachment methods. 

•    Connection of hardware and plugs. 

•    Relevant WHS practices. 

•    the use of approved maintenance documentation and aircraft publications relating to DC electrical systems. 

•    properties of permanent magnets. 

•    precautions for the care and storage of permanent magnets. 

•    general construction, operating characteristics and applications for: 

•    aircraft DC generators. 

•    alternator/rectifier DC generators. 

•    DC starter/generators.

•    DC motors, including starter motors. 

•    DC rotary and linear actuators. 

•    Batteries. 

•    how to locate and identify components of: 

•    DC power regulation and distribution systems. 

•    piston engine ignition and starting systems. 

•    gGs turbine engine igniter systems, includingg specific WHS precautions. 

•    Gas turbine engine starting systems. 

•    DC electrical systems, such as flaps and landing gear retraction. 

•    lighting systems. 

•    relevant maintenance manuals. 

•    relevant regulatory requirements and standard procedures. 

(c) Assessment   recommendation

         N/A

Assessmen  methods

 

(a) Recommendation

(b) Description

        N/A

 

The assessment are based on combination of paper exams, interviewing, and practical demonstrations depending on the assessors’ judgement.Competition should be assessed in the workplace or place of work simulated using tools and equipment specified in the maintenance manuals. It is also expected that general purpose tools, test and ground support equipment found in most situations routine maintenance would be used where appropriate. 

•    An understanding of the methods of fixing, connecting hardware, and the need for adjustment or rigging and operation of the system in relation to the work must be demonstrated 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 evaluation conditions represent the regulatory requirements (ADF) and the House and stakeholders maintenance and must be strictly observed. 

•    A person can not be assessed as competent until they can demonstrate to the satisfaction of the assessor workplace relevant elements and performance criteria of competence unit is carried out under routine supervision at least one (1) component each: 

•    DC generators and generators alternator / rectifier and control system components single generator and related distribution.

•    Motors .

•    Actuators. 

•    System components engine ignition and starting piston. 

•    Aircraft batteries. 

•    Specific components of electrical current systems, such as flaps, landing gear. 

•    Lighting aircraft. 

•    Lighter gas turbine engine and starting systems (can be omitted when not applicable to the company). 

•    This is done through the records in the register of industrial experience and achievement or, where appropriate, a guide equivalent Industry Evidence (for details see the companion volume Assessment Guidelines). 

•    Assessors must meet the requirements of the National Education and Vocational Regulator.

•    people who have already reached evaluated Keep MEA274 light aircraft electrical systems and core components have met the requirements of this unit with respect to the common range of varying conditions. The Registry of industry experience and accomplishments related records Keep MEA274 be accepted as meeting the requirements of evidence for this unit in public areas apply the basic light aircraft electrical systems and components.