Hydraulics Flashcards

(16 cards)

1
Q

How many hydraulic systems are there?

A

3

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2
Q

What nominal pressure do all three hydraulic systems operate at?

A

3000 psi

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3
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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4
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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5
Q

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

A

no

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6
Q

What is Hydraulic System 1 compromised of?

A

One reservoir, one engine driven pump (EDP 1), one electrical DC motor pump (DCMP 1), one shutoff valve (SOV 1) and one accumulator

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7
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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8
Q

What is Hydraulic System 2 compromised of?

A

One reservoir, one engine driven pump (EDP 2), one shutoff valve (SOV 2) and one accumulator

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9
Q

What is Hydraulic System 3 compromised of?

A

One reservoir, one electrical DC motor pump (DCMP 3) and one accumulator

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10
Q

What is the only source of hydraulic power for Hydraulic System 3?

A

The battery and the Ram Air Turbine (RAT)

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11
Q

What is the only source of hydraulic power for Hydraulic System 3?

A

The electric DCMP 3

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12
Q

What is the source of electrical power for the electric DCMP3 (Hydraulic System 3)?

A

EMER BUS 3

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13
Q

If the airplane loses HYD 1 and HYD 2, 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 Hydraulic 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 System 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