Maintaining rotor blade and tail pylon folding systems on rotorcraft (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 are competent inbeing able to carry out maintenance activities on rotor blade and tail pylon folding systems, in accordance with the approved rotorcraftmaintenance manual, approved change documentation (service bulletin) and airworthiness requirements. It covers the whole of thesystem for ensuring automatic or manual folding and spreading of the rotor blades and/or tail pylon, and includes the mechanical,hydraulic, electrical and indicating equipment and systems permanently fitted to the rotorcraft. The maintenance activities will includethe removal, fitting and testing of a range of rotor blade and tail pylon folding system components. They will remove the requiredcomponents and fit approved replacements, as appropriate. They will then need to test and adjust the completed system to meet therotorcraft maintenance manual, change documentation (service bulletin) and airworthiness requirements.
Exam Tips
- Always cross-reference the maintenance task with the specific aircraft chapter and section; cite these references in your portfolio evidence to show compliance.
- Include clear, annotated photographic or video evidence showing test equipment in use and final system adjustments, as this strengthens the demonstration of competence.
- Be prepared to explain the theory of operation, especially safety interlocks that prevent blade folding in flight, as assessors often probe this to confirm deep understanding.
Common Mistakes
- Failing to fully depressurise hydraulic systems before disconnecting components, risking fluid injection injury and contamination of the work area.
- Omitting a complete functional test after reassembly, particularly neglecting to verify emergency or backup folding modes.
- Incorrectly torquing fasteners or using uncalibrated tools, leading to potential joint failure under load or vibration.
- Misinterpreting the applicability of service bulletins, resulting in installation of incompatible parts or missed modifications.
Key Marking Points
- Award credit for demonstrating correct interpretation and application of the rotorcraft maintenance manual procedures during component removal and installation.
- Evidence must show precise testing and adjustment of the folding system to meet the specific tolerances and functional check requirements outlined in the approved data.
- Candidate must adhere to all airworthiness directives, including proper documentation of work, tool control, and verification of system integrity through post-maintenance operational checks.
- Look for correct identification, handling, and fitting of replacement components as per the illustrated parts catalogue and applicable change documentation, ensuring configuration control.