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Questions and Answers
What is the function of the hydraulic fluid in the landing gear system?
What is the function of the hydraulic fluid in the landing gear system?
- To enhance the aerodynamic performance of the aircraft.
- To lubricate the landing gear components.
- To supply pressure to the actuating cylinders. (correct)
- To cool the engine during flight.
Where is the electrically powered reversible pump located?
Where is the electrically powered reversible pump located?
- In the cockpit area near the control quadrant.
- In the cargo hold of the aircraft.
- In the engine compartment beneath the wings.
- In the aft fuselage between fuselage stations 156 and 191. (correct)
How is the pump controlled during operation?
How is the pump controlled during operation?
- By a selector switch on the instrument panel. (correct)
- Through a wireless remote control system.
- Using a manual lever located on the landing gear.
- Automatically based on fuel levels.
What determines the direction in which the hydraulic fluid is directed?
What determines the direction in which the hydraulic fluid is directed?
What is an integral part of the pump in the landing gear system?
What is an integral part of the pump in the landing gear system?
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Study Notes
Landing Gear Hydraulic System
- An electrically powered pump located in the aft fuselage supplies hydraulic fluid to the landing gear actuating cylinders
- The pump is located between fuselage stations 156 and 191
- The pump has an integrated reservoir
- The pump is controlled by a selector switch on the instrument panel
- There are dedicated pressure lines for each individual actuating cylinder
- The pump directs fluid through these lines based on the position of the selector switch
- The same lines serve as either pressure or return passages depending on the pump rotation, which determines gear extension or retraction
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