Hydraulics Flashcards

1
Q

What is the difference between hydraulic systems 1 and 2?

A

Services provided by each system, and system 1 has a priority valve

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2
Q

What is the capacity of the hydraulic reservoir?

A

6 liters

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3
Q

What quantity of hydraulic fluid will trigger the hydraulic low quantity EICAS message?

A

Below 1 liter

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4
Q

Where is the hydraulic system 1 accumulator located?

A

Forward right nose hydraulic compartment

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5
Q

Where is the hydraulic system 2 accumulator located?

A

Hydraulic compartment on the right side of the aircraft, behind the wing

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6
Q

How is a clogged hydraulic filter indicated?

A

Pop-up indicator on the hydraulic manifold. There is no cockpit indication.

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7
Q

What is the main difference between the engine driven hydraulic pump and electric hydraulic pump?

A

Volume output is much higher when using engine driven pump

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8
Q

What is the output of the engine driven hydraulic pump?

A

3,000 psi
9.2 gallons per minute

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9
Q

What is the output of the electric hydraulic pump?

A

2,900 psi
0.7 gallons per minute

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10
Q

How is the hydraulic reservoir pressurized?

A

It uses its own system pressure referred to as “bootstrapping”

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11
Q

What is the purpose of the priority valve?

A

To ensure adequate pressure to the flight controls when operating on the electric hydraulic pump

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12
Q

What is the number 1 hydraulic accumulator used for?

A

Raising the main cabin door
Assisting in raising landing gear

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13
Q

What is the number 2 hydraulic accumulator used for?

A

Emergency brake - 6 applications

Parking brake - holds 24 hours

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14
Q

What are two ways to close the hydraulic shutoff valve?

A

Press the ENG PUMP SHUTOFF guarded button

Pull the fire handle

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15
Q

What is the function of the AUTO position of the electric hydraulic pump?

A

Electric pump is in standby, and will turn on in either of the following conditions:

Pressure drops below 1600 psi
N2 drops below 56.4%

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