Maintaining hydraulic systems on aircraft (Aviation Maintenance) (ATA 29) 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 aircraft hydraulic systems, in accordance with the approved aircraft maintenancemanual, approved change documentation (service bulletin) and airworthiness requirements. It covers both fixed wing and rotarywinged aircraft, and covers the units and components which supply the hydraulic fluid under pressure (includes tanks, pumps,accumulators, valves, pipes) to a common point (manifold) for redistribution to other defined systems. The maintenance activities willinclude the removal, fitting and testing of a range of hydraulic components. They will be expected to use the approved procedure forcorrectly isolating and de-pressurising the system, breaking into the system circuit and catching/containing any spilled fluids. They willremove the required components and fit approved replacements, as appropriate. They will then need to test and adjust the completedsystem to meet the aircraft maintenance manual, change documentation (service bulletin) and airworthiness requirements.
Exam Tips
- Always refer to the aircraft maintenance manual for torque values.
- Use correct personal protective equipment (PPE).
- Double-check all connections before pressurising.
Common Mistakes
- Failing to properly depressurise the system before work.
- Cross-threading fittings during reassembly.
- Not using correct fluid type for top-up.
Key Marking Points
- Depressurise and isolate hydraulic system safely before maintenance.
- Remove and replace hydraulic components correctly.
- Test system for leaks and correct operation after maintenance.
- Complete documentation in accordance with airworthiness requirements.