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Maintaining reciprocating engine turbo-supercharging systems on aircraft

URN: SEMAE3347
Business Sectors (Suites): Aeronautical Engineering Suite 3
Developed by: Enginuity
Approved on: 2021

Overview

This standard identifies the competences you need to carry out maintenance activities on aircraft reciprocating engine turbo-supercharging systems, in accordance with the approved aircraft maintenance manual, approved change documentation (service bulletin) and airworthiness requirements. It covers both fixed wing and rotary winged aircraft, and includes power recovery turbine assemblies and turbo-supercharging units when external to the engine. The maintenance activities will include the removal, fitting and testing of a range of engine turbo-supercharging system components. You will remove the required components and fit approved replacements, as appropriate. You will then need to test and adjust the completed system to meet the aircraft maintenance manual, change documentation (service bulletin) and airworthiness requirements.

Your responsibilities will require you to comply with the specific practices and procedures identified in the aircraft manual, change/service bulletin documentation and airworthiness requirements for the maintenance activities undertaken, and to report any problems with these requirements that you cannot personally resolve, or that are outside your permitted authority, to the relevant people. You must ensure that all tools, equipment and materials used are correctly accounted for on completion of the activities, and that all necessary job/task documentation is completed thoroughly, accurately and legibly. You will be expected to work with a minimum of supervision, taking personal responsibility for your own actions and for the quality and accuracy of the work that you carry out.

Your underpinning knowledge will provide a good understanding of your work, and will provide an informed approach to applying the appropriate maintenance techniques and procedures to aircraft engine turbo-supercharging systems. You will understand the removal, fitting and testing methods and procedures, and their application, along with the turbo- supercharging systems maintenance requirements. You will know how the equipment functions, the common problems that can occur, the purpose of the individual components and associated defects, in adequate depth to provide a sound basis for carrying out the maintenance activities, correcting faults and for ensuring that the equipment is maintained to the required standard.

You will understand the safety precautions required when working on aircraft engine turbo-supercharging systems, especially those for isolating the equipment. You will be required to demonstrate safe working practices throughout, and will understand your responsibility for taking the necessary safeguards to protect yourself and others in the workplace.

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Notes:

  1. This standard is designed to cover the practical experience requirements of the Airline Transport Association (ATA) Chapter 81 Reciprocating Engine Turbines.
  2. To display competence in this standard, it is necessary to both remove and fit aircraft engine turbo-supercharging system components. You must remove components; however, you may fit a replacement component where the original was previously removed by another person. You should also be aware of how to leave a system in a safe condition if maintenance tasks cannot be completed. This covers both the physical systems and the job documentation.

Performance criteria

You must be able to:

  1. work safely at all times, complying with health and safety and other relevant regulations, directives and guidelines
  2. follow the relevant maintenance schedules to carry out the required work
  3. carry out the maintenance activities within the limits of your personal authority
  4. carry out the maintenance activities, and replace components in the specified sequence and in an agreed timescale
  5. report any instances where the maintenance activities cannot be fully met or where there are identified defects outside the planned schedule
  6. complete relevant documentation in accordance with organisational requirements
  7. dispose of waste materials in accordance with safe working practices and approved procedures
  8. leave the aircraft and system in a safe and appropriate condition, free from foreign object debris on completion of the activities

Knowledge and Understanding

You need to know and understand:

  1. the specific safety practices and procedures that you need to observe when working on aircraft engine turbo- supercharging systems (including any specific legislation, regulations/codes of practice for the activities, equipment or materials)
  2. the need to check that cabin/cockpit switches, selectors and circuit breakers are in the correct position before applying any form of external power (such as electrical, hydraulic, air or vacuum)
  3. the importance of maintenance on aircraft engine turbo-supercharging systems, and impact upon Extended Range Twin-Engine Operations Procedures (ETOPS) systems, Electrical Wiring Interconnect Systems (EWIS), legislation and local procedures
  4. the requirements and importance of understanding and applying human factors as defined by the regulatory requirements and the potential impact if these are not adhered to
  5. the hazards associated with carrying out maintenance activities on aircraft engine turbo-supercharging systems, and with the tools and equipment used (such as hot parts of engines, traps from moving parts, misuse of tools) and how to minimise them and reduce any risk

  6. the protective equipment that you need to use for both personal protection (PPE) and protection of the aircraft

  7. what constitutes a hazardous voltage and how to recognise victims of electric shock

  8. how to reduce the risks of a phase to earth shock (such as insulated tools, rubber matting and isolating transformers)

  9. the importance of aircraft husbandry and of ensuring that, throughout the maintenance activity, the aircraft and work area are maintained free from foreign objects, and the implications of FOD to the safety of the aircraft

  10. how to extract and use information from aircraft manuals, log books, flight logs, charts, circuit and physical layouts, specifications, symbols used in aircraft engine turbo-supercharging systems, and other documents needed in the maintenance activities
  11. how to carry out currency/issue checks on the specifications you are working with
  12. terminology used in aircraft engine turbo-supercharging systems, and the use of system diagrams and associated symbols
  13. the principles of operation of the aircraft engine turbo-supercharging system being worked on (such as system layout, and indication and warning)
  14. the techniques used to remove components from aircraft engine turbo-supercharging systems without damage to the components or surrounding structure (such as release of pressures/force, removal of components and the need to protect the circuit integrity by ensuring that exposed components and pipe ends are correctly covered/protected)
  15. the various mechanical fasteners to be removed and replaced, and their methods of removal and replacement (such as threaded fasteners, special securing devices)
  16. the various types of electrical connector that are used, methods of unlocking, orientation indicators and locating and locking-in of the connections
  17. the need to label and store correctly components that require repair or overhaul, and to check that replacement components have the correct part/identification markings and accompanying release documentation
  18. how to fit components into the system (such as ensuring the correct position and orientation; correct tightness of fittings and connections; eliminating stress on pipework, cables and connections; carrying out visual checks of all components)
  19. why electrical bonding is critical, and why it must be both mechanically and electrically secure
  20. the tools and equipment used in the maintenance activities and their calibration/care and control procedures
  21. why tool/equipment control is critical and what to do if a tool or piece of equipment is unaccounted for on completion of the activities
  22. how to make adjustments to components/assemblies to ensure that they function correctly (such as adjusting density controller)
  23. why securing devices need to be tightened to the correct torque, locked and labelled, and the different methods that are used
  24. how to carry out routine checks and servicing of the aircraft engine turbo-supercharging system (including checking the security of critical fasteners, checking condition of gaskets)
  25. the types of test to be carried out on the aircraft engine turbo-supercharging system and the test equipment to be used
  26. the methods and procedures to be used to carry out the various tests on the turbo-supercharging system
  27. how to record the results of the tests and the documentation that must be used
  28. how to analyse the test results, and how to make valid decisions about the acceptability of the aircraft turbo- supercharging system
  29. the procedures to be followed if the equipment or system fails to meet the test specification
  30. the recording documentation to be completed for the activities undertaken and, where appropriate, the importance of marking and identifying specific pieces of work in relation to the documentation
  31. the procedure for the safe disposal of waste materials and scrap components
  32. the extent of your own authority and to whom you should report if you have problems that you cannot resolve

Scope/range

Scope Performance

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  1. Carry out all of the following during the maintenance of the aircraft engine turbo-supercharging system:

    1. ensure that appropriate authorisation to work on the aircraft is obtained, and observe all relevant isolation and safety procedures
    2. obtain and use the correct documentation (such as job instructions, technical instructions, aircraft manuals and maintenance documentation)
    3. obtain the correct tools and equipment for the activity, and check that they are in a safe, tested and usable condition and within current calibration dates
    4. adhere to procedures or systems in place for risk assessment, COSHH, personal protective equipment and other relevant safety regulations and procedures to realise a safe system of work
    5. ensure that the relevant safety devices and mechanical/physical locks are in place (where appropriate)
    6. use approved removal, fitting and testing techniques and procedures at all times
    7. return tools and equipment to the correct storage location on completion of the activities
    8. ensure that work carried out is correctly documented and recorded
    9. ensure that any outstanding tests are correctly documented

  2. Carry out maintenance on two of the following parts of the aircraft engine turbo-supercharging system:

    1. power recovery turbine     
    2. supercharger
    3. exhaust turbocharger       
    4. turbo-supercharger system wiring

  3. Remove and fit four different aircraft engine turbo-supercharger system components (at least one must be from group A):

Group A

1.  turbo blower          
2.  density controller
3.  supercharger unit        
4.  actuators
5.  waste gate                    
6.  cables/harness/wiring

Group B
7. levers and linkages  
8. service panels/fairings
9. plugs/sockets/switches
10. control mechanisms
11. air filters    
12. position indicators/warning devices
13. seals         
14. springs
15. pipes and hoses
16. heat shields
17. other specific components

  1. Carry out fifteen of the following maintenance activities:

    1. removing access panels and covers to expose components to be removed
    2. carrying out fault diagnosis and system checks
    3. preparing the system for maintenance (such as isolating)
    4. disconnecting electrical connections (where applicable)
    5. refitting components in the correct position, orientation and alignment
    6. disconnect/removing hoses and pipes      
    7. removing securing devices and mechanical fasteners  
    8. setting and adjusting replaced components (such as travel, working clearance)
    9. supporting equipment to be removed          
    10. dismantling equipment to an appropriate level 
    11. making mechanical connections
    12. covering (protecting) exposed components, wires, pipework or vents 
    13. making electrical connections
    14. disconnecting/reconnecting bonding leads
    15. torque loading as required
    16. checking components for serviceability           
    17. carrying out system functional checks
    18. replacing damaged/defective components
    19. replacing single use items (such as seals, filters, gaskets)
    20. ensuring that replacement components have the correct part numbers
    21. fitting blanks, labelling (and storing in the correct location) components that require repair or overhaul
    22. applying bolt locking methods (such as split pins, wire locking, lock nuts)
    23. carrying out area inspections prior to task close down

  2. Service/check the aircraft engine turbo-supercharging system, to include carrying out three of the following:

    1. inspecting the turbo-supercharger units (such as for cracks, signs of leakage or damage)
    2. inspecting heat shields for damage/deterioration
    3. checking and adjusting density controller
    4. checking turbo-supercharging indicating systems

  3. Carry out three of the following tests on the aircraft engine turbo-supercharging system:

    1. leak test                               
    2. movement tests (such as range, timing, sequencing)
    3. pressure test              
    4. built in test equipment (BITE) test
    5. 'special-to-type' tests

Using one of the following:
6. aircraft power source/systems
7. ground test rig

  1. Complete the relevant paperwork, to include one from the following and pass it to the appropriate people:

    1. job cards/work sheets
    2. computer records
    3. aircraft technical log
    4. aircraft cabin log
    5. aircraft log book

  2. Carry out maintenance on aircraft engine turbo-supercharging systems in compliance with one of the following:

    1. Civil Aviation Authority (CAA)/European Aviation Safety Agency (EASA)
    2. Extended Range Twin-Engine Operations Procedures (ETOPS) (where appropriate)Ministry of Defence (MoD)
    3. Military Aviation Authority (MAA)
    4. Aerospace Quality Management Standards (AS)
    5. Federal Aviation Authority (FAA)
    6. aircraft maintenance manual/approved change documentation (service bulletin)
    7. manufacturers standards and procedures

Scope Knowledge

Values

Behaviours

​

You will be able to apply the appropriate behaviours required in the workplace to meet the job profile and overall company objectives, such as:

  • strong work ethic
  • positive attitude
  • team player
  • dependability
  • responsibility
  • honesty
  • integrity
  • motivation
  • commitment

Skills

Glossary

Links To Other NOS

External Links

Version Number

3

Indicative Review Date

2024

Validity

Current

Status

Original

Originating Organisation

Enginuity

Original URN

SEMAE3347

Relevant Occupations

Engineer, Engineering, Engineering and Manufacturing Technologies, Engineering Technicians

SOC Code

5234

Keywords

engineering; aeronautical; aircraft reciprocating; engine turbo-supercharging systems; cabin/cockpit switches; selectors; circuit breakers