หน่วยสมรรถนะ

หน่วยสมรรถนะ

Remove and install non-pressurized aircraft structural and non-structural.

สาขาวิชาชีพการบิน


รายละเอียดหน่วยสมรรถนะ


1. รหัสหน่วยสมรรถนะ AVT-IOKE-212A

2. ชื่อหน่วยสมรรถนะ Remove and install non-pressurized aircraft structural and non-structural.

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 requires the application of manual skills and maintenance publications for removing and installing structural and nonstructural components of fixed wing aircraft without pressure and rotation during scheduled and unscheduled maintenance. 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)
10 Aircraft Mechanics

9. ชื่ออาชีพและรหัสอาชีพอื่นที่หน่วยสมรรถนะนี้สามารถใช้ได้ (ถ้ามี)
101 Aircraft Maintenance: Airplane

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)
101315.01

Remove components.


101315.01.01 Structure is supported and prepared in accordance with the applicable maintenance manual to ensure the safety of personnel and the absence of damage to the aircraft or component during removal of components, and component extraction is carried out in accordance with the maintenance manual applicable to observe all relevant requirements of health and safety at work (WHS).

101315.01.01 199090
101315.01

Remove components.


101315.01.02 Required maintenance documentation is completed and processed in accordance with standard enterprise procedures. Where applicable, removed components are tagged and prepared for transport in accordance with specified procedures.

101315.01.02 199091
101315.02

Install components.

101315.02.01 Structural and/or non-structural components to be installed are checked to confirm correct part numbers, serviceability and modification status, and component installation is carried out in accordance with the maintenance manual applicable to observe all relevant requirements of the WHS, including the use of MSDS and PPE items.

101315.02.01 199092
101315.02

Install components.

101315.02.02 Support/safety equipment is removed at an appropriate time to ensure personnel safety and freedom from structural damage , and required maintenance documentation is completed and processed in accordance with standard enterprise procedures.

101315.02.02 199093

12. ความรู้และทักษะก่อนหน้าที่จำเป็น (Pre-requisite Skill & Knowledge)

101313  Remove and install aircraft hydro-mechanical and landing gear system 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 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 include:

•  Applying relevant WHS practices, including the use of MSDS and PPE. 

•  Using relevant maintenance documentation and aircraft manuals to: 

•  Remove and install structural and non-structural components. 

•  Remove and install aircraft interior fittings. 

•  Remove and install doors, door seals, windows and transparent panels. 

•  Checking and adjusting all doors and access panels, including locking mechanisms. 

•  Removing and installing emergency equipment. 

It is essential that buttresses, trestling and lifting requirements and security measures applicable to the structure being held are fully observed, understood and respected. Evidence of transferability of skills and knowledge related to the removal and installation is essential. This can be demonstrated by applying through the groups of components contained in the evaluation conditions.



(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 knowledge of:

•  Structural and non-structural component methods of construction and attachment, faying surface treatment and fuel tank sealing. 

•  Non-pressurised fuselage aircraft doors, related seals and window and transparent panel construction, attachment methods and sealing. 

•  Aircraft interior fittings (trim, linings, seats, floor panels, and so on) construction and attachment methods. 

•  The location and attachment or stowage methods for emergency equipment. 

•  Relevant WHS practices. 

•  How to obtain MSDS. 

•  Use of PPE. 

•  Relevant maintenance manuals. 

•  Relevant regulatory requirements and standard procedures. 



(c) Assessment   recommendation

N/A

Assessmen  methods

N/A

 


15. ขอบเขต (Range Statement)

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.



Removable components of structure include:     

Which is installed by bolts and / or screws. Where removal of components and installation requires removal and installation of rivets the applicable unit is or inspect, repair and maintain aircraft structures, inspection and maintenance of structures and related components small aircraft unpressurized or carry out minor repairs and modifications to the structure of metal small aircraft.

• Removable components include: 

• Removable components of wings, tail booms, pylons, empennage, skids, fairings and nacelles. 

• Removable components or sections of non-pressurised fuselages. 

• Non-pressurised fuselage entry, cargo, access doors and associated seals, including checking and adjustment of all doors and access panels and associated locking mechanisms. 

• Non-pressurised fuselage windows and transparent panels. 

• Where applicable, trim panels, linings, seats, cabin equipment and consoles, floor panels and coverings. 

• Applicable emergency equipment, including passenger escape systems, life jackets, rafts, location transmitters, beacons, crew and passenger seat restraints. 



Sealant removal and application includes:     

• The removal and application of faying (contact or overlapping) surface and fuel tank sealants is included, where applicable.



Procedures and requirements include:     

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



(b) Description

N/A

 


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.

• Competition should be assessed in the workplace or work environment 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 routine situations would be used where appropriate.

• An understanding of component handling, attachment methods, adjustment and sealing as it relates to the work must be demonstrated 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 and maintenance stakeholders and must be rigorously 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) point of each of the following groups of components:

• Removable components of wings, tail booms, pylons, empennage, skids, fairings and nacelles. 

• Removable components or sections of non-pressurised fuselages. 

• Non-pressurised fuselage entry, cargo, access doors and associated seals, including checking and adjustment of all doors and access panels and associated locking mechanisms. 

• Non-pressurised fuselage windows and transparent panels. 

• where applicable, trim panels, linings, seats, cabin equipment and consoles, floor panels and coverings. 

• Applicable emergency equipment, including passenger escape systems, life jackets, rafts, location transmitters, beacons, crew and passenger seat restraints. 

• 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). 

 



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