Hydrulics Flashcards

1
Q

How many hydraulic systems are there

A

Three

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2
Q

What normal pressure do all three hydraulic systems operate at

A

3000 psi

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3
Q

What MFD page provides a visual representation of the hydraulic system operation and parameters

A

The hydraulic synoptic page

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4
Q

What pressure is an amber tick mark placed at on the pressure indication for all three systems on the hydraulic synoptic page

A

1800 psi

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5
Q

What color is the symbol for shutoff valves that are open, engine driven pumps that are on and hydraulic flow lines that are pressurized.

A

Green

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6
Q

Will a failure of two hydraulic systems result in a complete loss of flight critical functions

A

No - due to system design.

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7
Q

What is hydraulic system 1 comprised of

A
One reservoir 
one engine driven pump (EDP1) 
one electrical DC motor pump (DCMP1) 
one shutoff valve (SOV1) 
one accumulator
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8
Q

When will the DCMP 1 be automatically commanded on with the HYD 1 ELEC pump knob in the AUTO position

A

During Takeoff and Landing Phases

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9
Q

What is hydraulic system 2 comprised of

A

One reservoir
One engine driven pump (EDP2)
One Shutoff valve (SOV2)
One accumulator

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10
Q

Hydraulic System 3 is designed to operate in conjunction with what electrical systems

A

The battery and RAT

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11
Q

What is the only source of electrical power for HYD system 3

A

The electric DCMP 3

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12
Q

What is the source of the electrical power for the electrical DCMP 3

A

EMER BUS 3

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13
Q

If the airplane loses HYD1 and HYD2, will the overheat protection system of HYD 3 still be functional

A

No, it will be inhibited

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14
Q

What is the backup for HYD systems 1 and 2

A

The PTU

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15
Q

What is the primary function of the PTU

A

To transfer power from hydraulic system 1 to 2 or vice versa

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16
Q

When the PTU knob is in the AUTO position, when will the LGHCUs automatically activate the PTU

A

In the event of an engine failure or EDP failure