หน่วยสมรรถนะ

หน่วยสมรรถนะ

Inspect gas turbine engine systems and components.

สาขาวิชาชีพการบิน


รายละเอียดหน่วยสมรรถนะ


1. รหัสหน่วยสมรรถนะ AVT-YASY-228A

2. ชื่อหน่วยสมรรถนะ Inspect gas turbine engine systems and components.

3. ทบทวนครั้งที่ /

4. สร้างใหม่ ปรับปรุง

5. สำหรับชื่ออาชีพและรหัสอาชีพ (Occupational Classification)

7232 Aircraft engine mechanics and fitters  



6. คำอธิบายหน่วยสมรรถนะ (Description of Unit of Competency)
       This unit of competency employs hand skills, maintenance publications, and knowledge of gas turbine engine and system theory in the inspection of gas turbine engines and engine system components of fixed and rotary wing aircraft. This work may be carried out individually or as part of a team.

7. สำหรับระดับคุณวุฒิ
1 2 3 4 5 6 7 8

8. กลุ่มอาชีพ (Sector)
10 Aircraft Mechanics

9. ชื่ออาชีพและรหัสอาชีพอื่นที่หน่วยสมรรถนะนี้สามารถใช้ได้ (ถ้ามี)
102 Aircraft Mechanics: Helicopter

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)
101410.01

Inspect gas turbine engine systems and components.

101410.01.01 Isolation tags already attached to the system or relevant systems are checked and aircraft configured for safe system inspection and operation according to applicable maintenance manual. 

101410.01.01 199356
101410.01

Inspect gas turbine engine systems and components.

101410.01.02Gas Turbine engine systems are visually or physically checked for external signs of defects according to the applicable maintenance manual while noticing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE).

101410.01.02 199357
101410.02

Inspect gas turbine engine components.

101410.02.01 Isolation tags already attached to the system or relevant systems are checked and aircraft configured for safe system inspection and operation according to applicable maintenance manual.

101410.02.01 199358
101410.02

Inspect gas turbine engine components.

101410.02.02 Gas turbine engine components are visually or physically checked for external signs of defects according to the applicable maintenance manual while noticing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE).

101410.02.02 199359

12. ความรู้และทักษะก่อนหน้าที่จำเป็น (Pre-requisite Skill & Knowledge)

101317 Remove and install engine system and components


13. ทักษะและความรู้ที่ต้องการ (Required Skills and Knowledge)

(ก) ความต้องการด้านทักษะ

See Appendix A

(ข) ความต้องการด้านความรู้

See Appendix A


14. หลักฐานที่ต้องการ (Evidence Guide)

(a) Performance Evidence

     Evidence required to express competency in this unit must be related to and fulfil all of the requirements of the elements and performance criteria under the indicated conditions of assessment, and must include:

• Applying relevant WHS procedures, including lifting and handling of heavy components.

• Using MSDS and PPE.

• Using relevant maintenance documentation and aircraft manuals to:

•  Recognise through visual/physical inspection external and internal signs of defects/damage to gas turbine engine, components and system componentsassist with testing of gas turbine engine and engine system operation.

    The fundamental skills inherent in this unit should be transferable across a range of inspection, testing and troubleshooting tasks (including the timely involvement of supervisors or other trades) associated with gas turbine engines, components and systems. It is crucial that inspection procedures consider all safety precautions applicable to the system/component being maintained.

    It is essential to be able to interpret inspection procedures and specifications (allowable limits) and apply them in practice. This shall be demonstrated through application across a range of systems as specified in the Assessment Conditions.

(b) Knowledge Evidence

      Evidence required to express competency in this unit must be related to and fulfil all of the requirements of the elements and performance criteria and include knowledge of :

• Gas turbine engine layout and operation:

• Intakes.

• Compressors.

• Combustion chambers.

• Turbines.

• Exhaust.

• Thrust reversers.

• Accessory drives.

• Bearings and seals.

• Maintenance requirements.

• System and component operation, including electrical and instrument system interfaces:

• Fuel control and fuels.

• Lubrication and lubricants.

•  Air distribution.

• Starting.

• Ignition.

• Power augmentation.

• Instrumentation:

• Performance indication.

• Condition indication.

• Warning.

• Presentation and interpretation of electronic displays.

• Fire warning and extinguishing.

• control system.

• Engine spin/run procedures, including the operation of auxiliary power units (APUs).

• Engine condition monitoring.

• Relevant WHS practices, including the requirements for the lifting and handling of heavy components.

• How to obtain MSDS.

• Selection and use of PPE.

• Maintenance requirements.

• Relevant maintenance manuals.

• Relevant regulatory requirements and standard procedures.

(c) Assessment recommendation

                 N/A


15. ขอบเขต (Range Statement)

a) Recommendation

     Different working environments and conditions that may affect performance are admissible in this field. Crucial 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.

(b) Description

Gas turbine engine and components include:

• Engine change unit, main components and accessories/drives.

• Control system and major system components.

• Ignition and starter systems and major system components.

•  Engine fuel system and major system components.

•  Oil system and major system components.

•  N/AAir system and major system components.

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 based on combination of paper exams, interviewing, and practical demonstrations depending on the assessors’ judgement.

• Competency should be assessed in the work environment or simulated work environment using tools and equipment stated in maintenance manuals. It is also expected that applicable general-purpose tools, test and ground support equipment found in most routine situations and used to assist in the inspection process would be used where appropriate.

• The work plan should consider applicable safety and quality requirements according to 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 and performance criteria of the unit of competency are being achieved under routine supervision on each of the following systems and at least one (1) component of each system.

•  Engine change unit, main components and accessories/drives.

•  Control system and major system components.

• Ignition and starter systems and major system components.

•  Engine fuel system and major system components.

• Oil system and major system components.

• Air system and major system components.

    This shall be proven via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry Evidence Guide.



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