Hydraulic Flashcards

1
Q

How many hydraulic systems are on the EMB175?

A

3

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2
Q

can hydraulic fluid be transferred between systems?

A

NO

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3
Q

What hydraulic pump can be powered by the RAT?

A

ACMP3A

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4
Q

Hydraulic system 3 supplies power for which systems?

A

Primary flight controls

Elevator
Aileron
Rudder

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5
Q

How many ACMP are installed for the hydraulics?

A

4 (1 for HYD1 & 2 - 2 for HYD 3)

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6
Q

How long after power up should you wait until Hydraulics are powered on? why?

A

3 mins - to allow flight controls to finish their PBIT test.

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7
Q

When will ACMP 1 &2 Operate on the ground?

A

-Flaps> 0 and power set to TO or
-Flaps>0 and Groundspeed greater than 50kts

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8
Q

When would ACMP 1&2 operate in flight?

A

engine or EDP FAIL
OR
flaps greater than 0

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9
Q

can we disable EDP by pushing out on the pb?

A

NO, this only shuts off the valve and isolates it from the system

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10
Q

What are some systems on HYD 2 that are not on HYD 1?

A

Nosewheel steering
Landing gear retract
Inboard brakes

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11
Q

What is the purpose of the PTU?

A

Transfers power from system 1 to be used on system 2 in the event of engine 2 failure or EDP failure.

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12
Q

What conditions must be met for the PTU to activate automatically?

A

Engine 2 fail or EDP fail
Gear not up
flaps not up
EDP1 NOT FAILed

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13
Q

Why is PTU still necessary if we have ACMP2?

A

to assist in gear retraction
ACMP is not strong enough

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14
Q

Why does ACMP 3B have AUTO?

A

Its a backup for ACMP3A

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15
Q

Why do HYD1 and 2 electric pumps have an ON?

A

to override system logic

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16
Q

If both engines fail, what provides Hydraulic pressure for HYD3 while the RAT is deploying?

A

Accumulator pressure

17
Q

The Hydraulic PBIT will run when?

A

when all 3 Hydraulic systems are pressurized

18
Q

What would interrupt a Hydraulic PBIT?

A

Moving flight controls.

19
Q

What is the primary purpose of HYD 3?

A

Backup for the primary flight controls