Hydraulic Systems Quiz

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Questions and Answers

Which component prevents damage from high system pressure in the hydraulic system?

  • The engine-driven pump
  • The one-way check valve
  • The pressure relief valve (correct)
  • The hydraulic fuse

Where is the hydraulic system service bay located?

  • In the upper aft fuselage behind the right wing trailing edge
  • In the upper aft fuselage behind the left wing trailing edge
  • In the lower aft fuselage behind the left wing trailing edge
  • In the lower aft fuselage behind the right wing trailing edge (correct)

What does the hydraulic pump pressurize in the system?

  • The nose wheel steering and hydraulic fuse
  • The normal system and emergency accumulator (correct)
  • The flaps and speed brake
  • The landing gear and main gear doors

At what pressure does the hydraulic pressure display change from white to amber?

<p>1800 psi (C)</p> Signup and view all the answers

What does an amber HYD FL LO caution indicate on the EICAS display?

<p>The fluid level is low (C)</p> Signup and view all the answers

How is the hydraulic fluid level checked in the hydraulic system service bay?

<p>By comparing the position of the green indicating rod to marked indicator windows (B)</p> Signup and view all the answers

What should be done if the fluid level is not FULL AC or FULL AD?

<p>Depressurize the emergency accumulator (A)</p> Signup and view all the answers

What should happen to the fluid level in the reservoir as the accumulator discharges?

<p>It should increase (A)</p> Signup and view all the answers

When should the hydraulic system be serviced?

<p>When the accumulator is fully discharged (C)</p> Signup and view all the answers

What is the capacity of the engine-driven pump in the hydraulic system?

<p>Approximately 5 quarts (B)</p> Signup and view all the answers

Where is the circuit breaker for the hydraulic system located?

<p>On the battery bus circuit breaker panel in the front cockpit (A)</p> Signup and view all the answers

What happens when the circuit breaker for the hydraulic system is open?

<p>The pressure indication and HYD FL LO sensor is not available (C)</p> Signup and view all the answers

How is the emergency hydraulic pressure activated?

<p>By pulling the emergency gear extension handle in the front cockpit (A)</p> Signup and view all the answers

What is the indication of the emergency accumulator's status?

<p>An amber EHYD PX LO caution on the EICAS (B)</p> Signup and view all the answers

What prevents the emergency system from bleeding back into the main system?

<p>A check valve (D)</p> Signup and view all the answers

What is the maximum fluid loss allowed in the event of an emergency hydraulic system leak?

<p>20-30 cubic inches (0.5 quart) (A)</p> Signup and view all the answers

When will the HYD FL LO caution illuminate?

<p>When there is insufficient fluid in the main reservoir (C)</p> Signup and view all the answers

What happens if the leak rate in the emergency system is below.25 GPM?

<p>The system depletes the main reservoir until the HYD FL LO caution illuminates (D)</p> Signup and view all the answers

What is the purpose of the landing gear system?

<p>To retract and extend the landing gear (A)</p> Signup and view all the answers

What are the major components of the landing gear system?

<p>Two main landing gear, outboard gear doors, inboard gear doors, and a steerable nose gear (B)</p> Signup and view all the answers

What happens to the flaps if power to the flap control circuit is lost?

<p>The flaps will retract to the UP position (D)</p> Signup and view all the answers

Where is the emergency selector valve located?

<p>In the hydraulic power system emergency manifold (B)</p> Signup and view all the answers

What happens to the flaps after emergency extension until the aircraft is serviced by maintenance?

<p>The flaps can be retracted (C)</p> Signup and view all the answers

What does the position pointer on the flap indicator indicate?

<p>Flap motion (B)</p> Signup and view all the answers

What is the maximum deflection of the speed brake?

<p>70° (D)</p> Signup and view all the answers

When will the speed brake automatically retract?

<p>When the FLAPS selector is moved out of the UP position (A)</p> Signup and view all the answers

Which component prevents damage from high system pressure in the hydraulic system?

<p>The pressure relief valve (D)</p> Signup and view all the answers

What is the capacity of the engine-driven pump in the hydraulic system?

<p>5 quarts (B)</p> Signup and view all the answers

Where is the hydraulic system service bay located?

<p>In the lower aft fuselage behind the right wing trailing edge (A)</p> Signup and view all the answers

What is the indication of the emergency accumulator's status?

<p>The position of the green indicating rod (A)</p> Signup and view all the answers

What should be done if the fluid level is not FULL AC or FULL AD?

<p>Service the system (A)</p> Signup and view all the answers

When will the HYD FL LO caution illuminate?

<p>When the accumulator is fully discharged (D)</p> Signup and view all the answers

Which type of steering is used for the nose wheel of the aircraft?

<p>Free castoring steering (A)</p> Signup and view all the answers

What is the purpose of the friction collar on the nose landing gear strut cylinder?

<p>To provide additional shimmy damping (C)</p> Signup and view all the answers

Where is the power for the nose wheel steering system provided from?

<p>Generator bus (B)</p> Signup and view all the answers

What should be done if the nose wheel steering system fails to respond to pilot input?

<p>Disengage the system (B)</p> Signup and view all the answers

What should be done if there is a known failure of the nose wheel steering system during takeoff?

<p>Disengage the system (D)</p> Signup and view all the answers

What is the source of electrical power for the flap system?

<p>Battery bus (B)</p> Signup and view all the answers

Which component prevents movement of the landing gear selector handle when the right weight-on-wheels switch is energized?

<p>The downlock solenoid (B)</p> Signup and view all the answers

What is the purpose of the downlock override button?

<p>To raise the landing gear handle when the right weight-on-wheels switch is energized (A)</p> Signup and view all the answers

What is the maximum fluid loss allowed in the event of an emergency hydraulic system leak?

<p>20-30 cubic inches (0.5 quart) (A)</p> Signup and view all the answers

What is the indication of the emergency accumulator's status?

<p>Amber EHYD PX LO caution on the EICAS (D)</p> Signup and view all the answers

Where is the circuit breaker for the hydraulic system located?

<p>On the battery bus circuit breaker panel in the front cockpit (D)</p> Signup and view all the answers

What is the indication of the gear handle and red indicator lights?

<p>The nose gear is in transit or main gear doors are not closed (B)</p> Signup and view all the answers

Which component is responsible for opening the inboard main gear doors in the landing gear system?

<p>The hydraulic actuator (C)</p> Signup and view all the answers

What locks the nose gear in the down position during landing gear extension?

<p>The over-center position of the folding strut (C)</p> Signup and view all the answers

What cockpit indications confirm that the landing gear is fully down and locked?

<p>All of the above (D)</p> Signup and view all the answers

What activates the aural landing gear position warning?

<p>All of the above (D)</p> Signup and view all the answers

When can the warning horn be silenced using the WARNING SILENCE button?

<p>When the gear handle is raised with flaps LDG (B)</p> Signup and view all the answers

How is directional control during taxi accomplished?

<p>All of the above (D)</p> Signup and view all the answers

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