หน่วยสมรรถนะ

หน่วยสมรรถนะ

Minor repair for aircraft electrical hardware or parts.

สาขาวิชาชีพการบิน


รายละเอียดหน่วยสมรรถนะ


1. รหัสหน่วยสมรรถนะ AVT-FTN-4-035ZA

2. ชื่อหน่วยสมรรถนะ Minor repair for aircraft electrical hardware or parts.

3. ทบทวนครั้งที่ - / -

4. สร้างใหม่ ปรับปรุง

5. สำหรับชื่ออาชีพและรหัสอาชีพ (Occupational Classification)


101 Aircraft Mechanics: Airplane




102 Aircraft Mechanics: Helicopter



6. คำอธิบายหน่วยสมรรถนะ (Description of Unit of Competency)
          This skill unit requires the use of workforce skills and knowledge of standards and cabling specifications to manufacture aircraft electrical looms, harnesses and cables in hangars and aircraft maintenance workshops during maintenance scheduled or unscheduled. The work can be done individually or as part of a team.

7. สำหรับระดับคุณวุฒิ
1 2 3 4 5 6 7 8

8. กลุ่มอาชีพ (Sector)
7232 Aircraft Mechanics

9. ชื่ออาชีพและรหัสอาชีพอื่นที่หน่วยสมรรถนะนี้สามารถใช้ได้ (ถ้ามี)
N/A

10. ข้อกำหนดหรือกฎระเบียบที่เกี่ยวข้อง (Licensing or Regulation Related) (ถ้ามี)
ICAO Doc 7192 / EASA Part 66

11. สมรรถนะย่อยและเกณฑ์การปฏิบัติงาน (Elements and Performance Criteria)
หน่วยสมรรถนะย่อย (EOC) เกณฑ์ในการปฏิบัติงาน (Performance Criteria) รหัส PC
(ตามเล่มมาตรฐาน)
รหัส PC
(จากระบบ)
101403.01 Interpret specifications and organise materials. 101403.01.01 Specifications are interpreted to determine the dimensionsand procedure for fabrication. 101403.01.01 71054
101403.01 Interpret specifications and organise materials. 101403.01.02 Appropriate materials,tools and equipment areselected and prepared for the particular specificationrequirements. 101403.01.02 71055
101403.02 Minor repair for electrical components or parts. 101403.02.01 Assembly or fabrication jigs, where applicable, arealigned to ensure accurate fabrication of components. 101403.02.01 71056
101403.02 Minor repair for electrical components or parts. 101403.02.02 Components or partsare repaired in accordance withrequired specifications while observing allrelevant work health and safety (WHS) requirementsincluding the use of material safety data sheets (MSDS) and personal protective equipment (PPE). 101403.02.02 71057
101403.03 Test / repaired components or parts. 101403.03.01 Test equipment and/or rigs are used,where applicable,to confirm serviceability of finished components. 101403.03.01 71058
101403.03 Test / repaired components or parts. 101403.03.02 Repaired componentsare tagged, sealed and packaged within specified procedures. 101403.03.02 71059

12. ความรู้และทักษะก่อนหน้าที่จำเป็น (Pre-requisite Skill & Knowledge)


101309 Remove and install miscellaneous aircraft electrical hardware/components




101311 Use electrical test equipment


13. ทักษะและความรู้ที่ต้องการ (Required Skills and Knowledge)

(ก) ความต้องการด้านทักษะ


EASA Part 66: Module 6Materials and Hardware



EASA Part 66: Module 7A Maintenance Practices

(ข) ความต้องการด้านความรู้


EASA Part 66: Module 6Materials and Hardware




EASA Part 66: Module 7A Maintenance Practices


14. หลักฐานที่ต้องการ (Evidence Guide)


(a) Performance Evidence




          • 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 must include:




          • applying relevant WHS practices, including the use of PPE and reference to MSDS




          • using approved repair/fabrication procedures and processes relating to electrical cables, harnesses, antenna leads and aerial components




          • recognising the integrity/security of electrical component crimps, wire wrapping, joints, and plug/connector pins




          • constructing cables, harnesses and looms, including wire marking, to approved industry standards




          • performing component testing to assess post-construction serviceability. The underlying skills inherent in this unit should be transferable into other areas that require similar techniques. It is essential that the general aspects of material specification and selection, measurement and fabrication/manufacture are related to specific aircraft component applications.




(b) Knowledge Evidence




          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 and system operation




          • aircraft wiring specifications and standards




          • standard repair methods for:




          • electrical cables




          • ignition harnesses




          • fire warning system harnesses




          • coaxial cables, such as antenna leads




          • aerial components




          • electrical plugs and connectors




          • soldering methods




          • fabrication methods for the above wiring and cables




          • wire marking methods




          • assembly of electrical cables into wiring looms




          • relevant WHS procedures




          • how to obtain relevant MSDS




          • relevant maintenance manuals




          • relevant regulatory requirements and standard procedures.


15. ขอบเขต (Range Statement)


          This field allows for different work environments and conditions that may affect performance. Essential operating conditions that may be present (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) are included.




          Components or parts include:




          Electrical looms, harnesses and cables associated with:




          power distribution




          ignition




          control circuits




          signal circuits




          Procedures and requirements include:




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


16. หน่วยสมรรถนะร่วม (ถ้ามี)
N/A

17. อุตสาหกรรมร่วม/กลุ่มอาชีพร่วม (ถ้ามี)
N/A

18. รายละเอียดกระบวนการและวิธีการประเมิน (Assessment Description and Procedure)


          • 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.




          • Competency should be assessed in the work environment or simulated work environmentusing tools and equipment specified by aircraft in the maintenance manuals. It is alsoexpected that applicable general-purpose tools and test equipment found in most routinesituations would be used where appropriate.




          • Evidence of knowledge about individual components and their links with systems will benecessary to supplement evidence of ability to interpret requirements and repaircomponents before undertaking any action. The work plan should take account ofapplicable 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 satisfactionof the workplace assessor that the relevant elements and performance criteria of the unit ofcompetency are being achieved under routine supervision on a representative range oftasks, including:




          • power distribution




          • ignition




          • control circuits




          • signal circuits.




          • This shall be established via the records in the Log of Industrial Experience and



          Achievement or, where appropriate, an equivalent Industry Evidence Guide (for detailsrefer to the Companion Volume Assessment Guidelines).



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