Hydraulic systems: power, pressure and protection
How aircraft hydraulic systems make, store, clean and protect pressure, how they are certified and serviced, and how to find faults and decide on dispatch
Part 1 · Basics
Hydraulic systems: power, pressure and protectionYou are herePart 2 · In practice
Troubleshooting hydraulic leaks and pressure faultsPart 3 · Managing it
Coming soon
Part 4 · What's next
Coming soon
Hydraulics · See the Flight Path →
What you will be able to do
- ✓ Explain why transport aeroplanes use hydraulic power and apply force = pressure × area and flow = speed × area to actuators at 3,000 and 5,000 psi.
- ✓ Distinguish hydraulic fluid families, their seal compatibility and contamination by particles, water, chlorine and air, and interpret a fluid sample report.
- ✓ Describe a three-system twin-jet architecture with engine-driven and electric pumps, power transfer unit and ram air turbine, using the official findings on United Airlines Flight 232.
- ✓ Explain reservoirs, accumulators, filters, priority valves and fuses, and correct an accumulator pre-charge for temperature.
- ✓ Apply the §25.1435 and §25.1309 requirements and the safe practices for depressurising, servicing and handling phosphate-ester fluid.
- ✓ Isolate leaks, cavitation, overheating and low-pressure warnings, and decide when minimum equipment list relief does and does not apply.
Course content
Session 1 · Why hydraulics: pressure doing work
1.1
- Why aircraft use hydraulics · free preview
- Pressure, area and force
- The basic circuit
- Worked example: sizing an actuator at 3,000 and 5,000 psi
Session 2 · Hydraulic fluids and contamination
1.2
- Fluid families and why they never mix
- Contamination: particles, water, chlorine and air
- Sampling and condition monitoring
- Worked example: reading a fluid sample report
Session 3 · Architecture and power sources
1.3
- Three systems, shared users
- Pumps: engine-driven, electric and air-driven
- Back-ups: power transfer unit, ram air turbine and higher-pressure designs
- From the investigation file: United Airlines Flight 232
Session 4 · Storing, cleaning and protecting
1.4
- Reservoirs and pressurisation
- Accumulators and pre-charge
- Filters, priority valves and fuses
- Worked example: correcting accumulator pre-charge for temperature
Session 5 · Certification, servicing and safety
1.5
- How hydraulic systems are certified
- Servicing and depressurising safely
- Phosphate-ester fluid: skin, eye and injection hazards
- Worked example: servicing a reservoir to the right quantity
Session 6 · Faults, troubleshooting and dispatch
1.6
- Leaks and the leak-rate check
- Cavitation, aeration and overheating
- Minimum equipment list relief
- Worked example: isolating a low-pressure warning
- SIA Engineering Company Expands Maintenance Footprint to Manila
- Azul Brazilian Airlines Expands Heavy Maintenance Program for Embraer and Airbus Fleet
- FL Technics Indonesia Secures EASA Part-145 Certification for Bali Facility
Facing a challenge in aircraft systems? Submit a bottleneck →
Experienced in aircraft systems? Join the bench →
Who this course is for
- Engineers new to transport aeroplane hydraulics who need the architecture and its numbers
- Technicians servicing reservoirs, filters and accumulators with phosphate-ester fluid
- Maintenance control staff deciding when hydraulic MEL relief does and does not apply
You need: Basic aircraft systems knowledge and simple physics (force, pressure and area).
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