Hydraulics Flashcards

1
Q

What holds the landing gear in the retracted position?

A

Nitrogen charged accumulator maintains hydraulic pressure

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2
Q

How is nosewheel steering accomplished?

A

Direct linkage and differential braking

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3
Q

Describe the hydraulic system?

A

Electrically driven, hydraulically actuated

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4
Q

Hydraulic system components

A

•Power package
•Service tray assembly
•Accumulator
•Time delay relay
•Nitrogen pressure cylinder

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5
Q

How long would the gear be held up after a power package failure?

A

Up to 200 minutes

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6
Q

Where is the hydraulic power package and what does it do?

A

LH wing root behind the spar
Supplies pressurized fluid to the gear selector and service selector valves and accumulator

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7
Q

What is the hydraulic reservoir capacity?

A

.79 gal

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8
Q

What ensures the hydraulic reservoir remains pressurized in flight?

A

Nitrogen tank

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9
Q

What is normal hydraulic system pressure?

A

Up to 2875 psi

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10
Q

How is the system pressurized?

A

DC motor uses pressure switch to turn the motor on at less than 2450 psi and off between 2725 and 2875 psi

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11
Q

What will cause the hydraulic CAWS message to illuminate?

A

Less than 1800 psi

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12
Q

What is the function of the accumulator?

A

Maintain system pressure
Keep gear up if power package fails

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13
Q

What is the function of the nitrogen pressure cylinder?

A

Prevents pump cavitation

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14
Q

The nitrogen pressure cylinder is pressurized to what?

A

56 psi

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15
Q

Tires are inflated to what?

A

60 psi

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16
Q

What prevents gear retraction on the ground?

A

A de-energized solenoid plunger locks the landing gear handle in the down position

17
Q

What is the minimum hydraulic fluid quantity needed for operation?

A

.66 gal

18
Q

When might you get the hydraulic CAWS message on the ground after landing?

A

System cycled 6 times in an hour

19
Q

What are two reasons you might receive a hydraulic CAWS message in flight?

A

Less than 1800 psi
System on for 10 minutes during flight

20
Q

What keep the nose gear in the down position?

A

Drag link acts as an overcenter lock

21
Q

What assists in lowering the nose gear during an emergency?

A

Spring strut…also holds drag link in over center position

22
Q

What holds the main gear down?

A

Pawl lock mechanism holds the actuator in the fully extended position

23
Q

What do red landing gear lights indicate?

A

In transit or unsafe condition

24
Q

When would the gear horn sound and the gear lights illuminate?

A

Flaps >15 no gear down
A/S < 130 and throttle to idle

25
Q

How many strokes are necessary to lock the gear down manually?

A

60

26
Q

Do the main gear have down locks? Up locks?

A

Down locks only

27
Q

Maximum nose steering using rudder pedals?

A

12 degrees either side

28
Q

When can the nose steering extend beyond 12 degrees using rudder pedals?

A

If using brakes simultaneously

29
Q

Maximum towing nose wheel steering

A

+/- 60 degrees

30
Q

Left squat switch…

A

Left stick pusher computer
• Cabin Pressurization Control System
•Central Advisory and Warning System
•Engine Instrument System
•Hydraulic system control

31
Q

Right squat switch…

A

•Right stick pusher computer
•Landing gear indication
•Altitude and Heading Reference System (AHRS)
•Transponder(s)

32
Q

WOW failure in the air prevents what?

A

Gear retraction

33
Q

If both pilots are pressing the brakes, which one controls?

A

The one pressing the hardest