Hydraulics Flashcards

(30 cards)

1
Q

What does an Engine or Electric Hydraulic Pump PRESS light indicate?

A

Low pump pressure

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2
Q

What is powered by the Ram Air Turbine (RAT)?

A

Flight controls

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3
Q

What condition automatically deploys the Ram Air Turbine (RAT)?

A

Both engines fail

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4
Q

What is the minimum airspeed required to maintain adequate Ram Air Turbine (RAT)
hydraulic pressure?

A

130 knots

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5
Q

What cockpit indication assures adequate pressure to the center system when the
Ram Air Turbine (RAT) is deployed?

A

PRESS light

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6
Q

What does RF indicate on the Status page adjacent to hydraulic quantity?

A

Reservoir requires refilling

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7
Q

What does the SYS PRESS light indicate?

A

Low system pressure

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8
Q

Is it possible to deploy the Ram Air Turbine (RAT) on the ground with no power on
the aircraft?

A

Yes, RAT will deploy on the ground if RAT switch is

pushed regardless of Battery switch position

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9
Q

How does pulling the Engine Fire switch affect the hydraulic system?

A

Shuts off fluid to the engine pump and depressurizes the

pump

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10
Q

(757) What does the RSVR light indicate?

A

Low reservoir hydraulic quantity and/or pressure

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11
Q

(757) What does the OVHT light indicate?

A

Respective pump temperature is high

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12
Q

(757) What are the electrical inhibits associated with the hydraulic system?

A

With one engine‐driven generator operating and both
Center Electric Pump switches ON, the number two
electric pump is inhibited

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13
Q

(757) Which components are powered by the left hydraulic system?

A

Flight controls, alternate brakes, left thrust reverser,
main cargo door, flaps and slats, landing gear, and
nosewheel steering

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14
Q

(757) Which components are powered by the center hydraulic system?

A

Flight Controls

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15
Q

(757) Which components are powered by the right hydraulic system?

A

Flight controls, normal and reserve brakes, and right

thrust reverser

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16
Q

(757) What system uses the left reservoir reserve hydraulic fluid?

A

Power Transfer Unit (PTU)

17
Q

(757) What condition(s) cause the Power Transfer Unit (PTU) to operate
automatically?

A

Left engine failure and/or left engine‐driven hydraulic

pump pressure low

18
Q

(757) Which components are powered by the Power Transfer Unit (PTU)?

A

Landing gear, nosewheel steering, flaps and slats, and

main cargo door

19
Q

(757) What system uses the center reservoir reserve hydraulic fluid?

A

Ram Air Turbine (RAT)

20
Q

(757) What system uses the right reservoir reserve hydraulic fluid?

A

Reserve brakes

21
Q

(767) What does a QTY light indicate?

A

Low reservoir quantity

22
Q

(767) Which components are powered by the left hydraulic system?

A

Flight controls

23
Q

(767) What reservoir maintains reserve hydraulic fluid for use by reserve brakes and
steering?

A

Center hydraulic system

24
Q

(767) Which system(s) use reserve hydraulic fluid?

A

Reserve brakes and steering

25
(767) Which components does the center hydraulic system power?
Flight controls, alternate brakes, reserve brakes, tailskid, landing gear, nosewheel steering, Hydraulic Driven Generator (HDG), and flaps and slats
26
(767) Which components are powered by the right hydraulic system?
``` Flight controls and normal brakes and Pitch Enhancement System (PES) ```
27
(767) When does the left electric demand pump operate in AUTO?
Left engine pump pressure low
28
(767) When does the right electric demand pump operate in AUTO?
Right engine pump pressure low or flap lever in 1, 5, 15 | or 20 to ensure pressure to normal brakes during takeoff
29
(767) When does the Air Demand Pump (ADP) operate automatically?
Low center hydraulic system pressure, heavy load items are selected or when the Hydraulic Driven Generator (HDG) is signaled to operate
30
(767) What is the power source for the Air Demand Pump (ADP)?
Bleed air from the center pneumatic duct