Hydraulic System Flashcards

1
Q

Each demand pump has a switch titled “OFF, AUTO, ON.” Describe this switch and its positions.

A

OFF: Demand pump off
AUTO: Turns on when related engine pump pressure low or when related fuel control is in CUTOFF.
(For demand pumps 1 and 4, also turns on when TE flaps in transit, or flaps extend past 1 in flight.)
ON: Turns on demand pump

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2
Q

Each engine hydraulic pump has a switch. Describe this switch.

A

Pushed in= ON: Engine pump pressurizes when engine rotates
Pushed out=OFF: Engine pump off
Amber PRESS light: Engine hydraulic pump pressure low

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3
Q

Above each demand pump switch, there is a light. What does it mean if this light is on with the amber PRESS?

A

-Demand pump pressure low
-Demand pump OFF or AUX
-or, demand pump has failed

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4
Q

Each hydraulic system has an amber SYS FAULT light. What does seeing this light mean?

A

-Low pressure
-Low quantity
-High temp

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5
Q

What would a full hydraulic reservoir indicate on the hydraulic synoptic?

A

1.00 is full

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6
Q

What is the nominal pressure of the hydraulic system?

A

3,000 PSI

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7
Q

On the synoptic, you see a magenta RF. What does this mean?

A

Displays only on ground-refill needed.

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8
Q

On the synoptic, you see a magenta LO. What does this mean?

A

Low hydraulic reservoir quantity

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9
Q

How many hydraulic systems?

A

4 independent systems

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10
Q

What are all of the items that are hydraulically powered?

A
  • primary flight controls
  • autopilot servos
  • spoilers
  • stabilizer trim
  • elevator feel
  • landing gear
  • flaps
  • brakes
  • nosewheel steering/body gear steering
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11
Q

Each system is powered by how many pumps? What types? How are they powered

A

-Each system has at 1 demand pump and 1 engine driven pump
-System 1 and 4 demand pumps powered by bleed air
-System 2 and 3 demand pumps electric
-System 4 also has an electric AUX pump for ground handling

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12
Q

How is each hydraulic reservoir pressurized? Why?

A

-Bleed air.
-To prevent pump cavitation, and to ensure positive pressure in high demand conditions.

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13
Q

Which system powers the flight controls? Is there manual reversion?

A

ALL hydraulic systems redundantly power the flight controls.
No manual reversion.

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14
Q

There are 3 autopilot servos, all hydraulically powered. Left, center and right. Which hydraulic system powers each?

A

Left: System 3
Center: System 1
Right: System 2

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15
Q

What systems power the spoilers?

A

2, 3 and 4

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16
Q

How many hydraulic reservoirs?

A

1 per system.

17
Q

Normally, which pump provides pressure to the hydraulic system? What is its backup?

A

-Normal: EDP (Engine driven pump)
-Backup: Demand pump. Automatically operates during periods of high demand, such as flap in transit and gear retraction, or if the EDP fails.

18
Q

When do demand pumps automatically turn on?

A

ALL: -When EDP pressure low
-When related fuel selector is
in CUTOFF

Demand pump 1 and 4 only:
-When trailing edge flaps in
transit
-When flaps extended greater
than flaps 1 in flight

19
Q

When hydraulic system 4 AUX pump is selected, does the demand pump run?

A

No. The demand pump is OFF. Only the electric AUX pump would run.

20
Q

An EDP operates if______

A

The pump switch is ON, the engine is running, the fire switch is not pulled.

21
Q

You see a RSVR PRESS white indication on the hydraulic synoptic page. But the SYS FAULT light is not illuminated overhead.. what does this mean?

A

It means the bleed air pressure to a reservoir is low.

22
Q

What measures hydraulic quantity?

A

HYQUIM (Hydraulic Quantity Interface Module.)

Note: Can give erroneous indications if it faults due to overvoltage

23
Q

Where is the hydraulic reservoir located?

A

In each respective engine pilon

24
Q

Big ticket Items on System 1

A

-Nose and body gear (operation and steering)
-INBOARD Trailing edge flaps

25
Q

Big ticket items on system 4

A

-Wing gear
-OUTBOARD Trailing edge flaps

26
Q

Big ticket Items on system 2 and 3

A

-Upper and lower rudder
-upper and lower yaw damper
-Stab trim