Learning aim(s)
A: Investigate how the operation of hydraulic power, landing gear and flying control systems contribute to safe flight
Assignment title: Hydraulic Power, Landing Gear and Flying Controls
Vocational Scenario or Context
You are working as an apprentice engineer in a large civil aircraft maintenance organisation. You have been tasked to inspect a hydraulic-power, landing gear and flying control, system on an Airbus A380. On completion of the inspections, you are to compile a technical report that justifies how these systems and their components contribute to safe flight.
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Using the relevant technical manuals, you have been tasked with safely inspecting and reporting on the following systems on the Airbus A380:
- Green Hydraulic System
- Wing Landing gear
- High Lift flight Control System
During your inspection of the systems, you are to take appropriate photographs that you will use to illustrate your report.
On completion of the inspections you are to compile a written report that justifies how these systems and their components contribute to safe flight as detailed below:
Green Hydraulic System
Your report must include the following:
- An explanation of the operation, components, layout and function of the system and its power sources under normal and emergency conditions and considering alternative hydraulic supply sources, component type and layouts.
- An analysis and justification of how the hydraulic system contributes to the safe operation of the landing gear and high lift flight controls during the full ground-air-ground cycle.
Wing Landing Gear
Your report must include the following:
- An explanation of the operation, components, layout and function of the system and its power sources under normal and emergency conditions and considering alternative hydraulic supply sources, component type and layouts.
- An analysis and justification of how the landing gear system contributes to the safe flight including the interaction between pilot throttle settings, airspeed, weight switches and the landing gear extension / retraction.
High Lift System
Your report must include the following:
- An explanation of the operation, components, layout and function of the system and its power sources under normal and emergency conditions and considering alternative hydraulic supply sources, component type and layouts.
- An analysis and justification of how the high lift system system contributes to the safe flight including the interaction between pilot throttle settings, airspeed, weight switches and the operation of the high lift devices.
You will need to ensure that the report is easy to read, well-structured and uses the correct technical terminology and any applicable engineering mathematical notations
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Hire NowChecklist of evidence required
- Technical report using appropriate technical terminology
- Diagrams / graphical representations / photographs as appropriate
- Harvard References as appropriate
| Unit/Criteria reference | To achieve the criteria you must show that you are able to: |
| 53/A.D1 | Justify, using the findings from safe inspection and research, the function and operation of hydraulic-power, landing-gear and flight-control systems and their components, assessing the contribution made by each to safe flight. |
| 53/A.M1 | Analyse, using the practical findings from the safe inspection and research, the operation of hydraulic power, landing gear and flight control systems and their components, identifying their contribution to safe flight. |
| 53/A.P1 | Inspect one hydraulic-power, landing-gear and flight-control system safely. |
| 53/A.P2 | Explain, using the practical findings and research, the operation of hydraulic power, landing-gear and flight-control systems and their components, identifying their contribution to safe flight. |
| Sources of information to support you with this Assignment | Aircraft type specific technical manuals
|
| Other assessment materials attached to this Assignment Brief | e.g. work sheets, risk assessments, case study |
| Notes to Assessor and technician |
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