Hydraulics Flashcards

1
Q

How many hydraulic systems are there?

A

Three.

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2
Q

What nominal pressure do all three 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

Hydraulic synoptic page.

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4
Q

An amber tick marker is placed at the position relative to what pressure?

A

1800 psi.

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5
Q

What color is the symbol for SOVs that are open, EDPs that are on and 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.

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7
Q

What is hydraulic system 1 comprised of?

A

EDP, DCMP, SOV, reservoir, and accumulator.
(DCMP … DC Motor Pump)

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8
Q

When will the DCMP1 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

EDP, SOV, reservoir, and accumulator.

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10
Q

What is hydraulic system 3 comprised of?

A

DCMP, reservoir, and accumulator.

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11
Q

Hydraulic system 3 is designed to operate in conjunction with what electrical system?

A

Battery and RAT.

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12
Q

What is the only source of hydraulic power for hydraulic system 3?

A

DCMP3.

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13
Q

What is the source of electrical power for DCMP3?

A

EMER BUS 3.

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14
Q

If the airplane loses any 2 of the 3 hydraulic systems due to overheat, will the overheat protection system still be functional on the remaining system?

A

No, it will be inhibited.

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15
Q

What is the backup for hydraulic systems 1 and 2?

A

The PTU.

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16
Q

What is the primary function of the PTU?

A

To transfer power from system 1 to 2 and vise versa.

17
Q

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

A

Engine or EDP failure.