Maintaining reciprocating engine turbo‐supercharging systems on aircraft (Aviation Maintenance) Revision — Excellence, Achievement & Learning Limited Occupational Qualification
This unit identifies the training and development required in order that the apprentice can demonstrate that they arecompetent in being able 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) andairworthiness requirements. It covers both fixed wing and rotary winged aircraft, and includes power recovery turbineassemblies and turbo-supercharging units when external to the engine. The maintenance activities will include theremoval, fitting and testing of a range of engine turbo-supercharging system components. They will remove the requiredcomponents and fit approved replacements, as appropriate. They will then need to test and adjust the completed systemto meet the aircraft maintenance manual, change documentation (service bulletin) and airworthiness requirements.
Exam Tips
- Always cross-reference the aircraft maintenance manual and service bulletins for the specific airframe-engine combination before starting work.
- Develop a systematic checklist for removal, fitting, and testing to ensure no airworthiness requirement is missed.
- Practice distinguishing between turbo-supercharger units and power recovery turbines, and rehearse the unique steps for each.
- During practical assessments, clearly document all test results and adjustments, linking each to the corresponding specification limit.
Common Mistakes
- Confusing the maintenance requirements of turbo-supercharging systems with those of the basic engine, leading to omitted steps.
- Overlooking the need to verify the latest revision of the service bulletin, resulting in outdated procedures being followed.
- Assuming that test criteria are identical for fixed-wing and rotary-wing aircraft without checking airframe-specific instructions.
- Failing to secure external components like power recovery turbines with the correct locking devices, risking in-flight detachment.
Key Marking Points
- Award credit for demonstrating correct selection and use of the aircraft maintenance manual and any applicable service bulletins to guide removal and fitting procedures.
- Verify that all component removals and installations adhere to prescribed safety precautions, such as system isolation and tagging.
- Ensure torque values and locking methods are applied precisely as specified for all fasteners and connections.
- Assess the apprentice's ability to conduct functional tests, including leak checks and performance runs, and to adjust the system to meet airworthiness requirements.
- Confirm that the apprentice correctly identifies and handles power recovery turbine assemblies and external turbo-supercharging units distinct from internal engine components.