Landing Gear Flashcards

1
Q

Pressurizing system 4 before pressurizing the other systems precludes what?

A

Transfer of hydraulic fluid from system 1 or 2 to system 4

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2
Q

The normal brake hydraulic system is powered by which hydraulic system?

A

4

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3
Q

After alternate gear extension, the gear doors are in what position?

A

Open

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4
Q

The autobrake system provides braking until when?

A

A complete stop or the system disarmed

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5
Q

What would cause the autobrake system to disarm immediately?

A

Advancing thrust levers or fault

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6
Q

What is the source of the ground speed information provided to the antiskid controller?

A

The IRUs

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7
Q

In flight, the gear lever lock is released when what two conditions are met?

A

Main gear is tilted and body gear is centered

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8
Q

Body gear steering operates when the nosewheel steering angle exceeds __ degrees.

A

20

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9
Q

The body gear is hydraulically centered and body gear steering is deactivated as the aircraft accelerates through what speed?

A

20 knots

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10
Q

For which hydraulic brake systems are autobrakes available?

A

Normal

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11
Q

If hydraulic system 4 pressure is low, which hydraulic system would supply pressure to the alternate brake hydraulic system?

A

1

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12
Q

Rather than to individual wheels, the alternate brake system provides antiskid protection to the wheels how?

A

Lateral wheel pairs

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13
Q

During takeoff, with RTO selected, when would RTO engage?

A

Aircraft on ground, groundspeed > 85 knots, and all thrust levers closed.

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14
Q

Loss of which hydraulic systems causes the brake source light to illuminate?

A

4, 1, 2

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15
Q

Which brake hydraulic system provides main gear wheel with individual antiskid protection?

A

Normal

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16
Q

At what speed is the RTO autobrake function inoperable if an RTO is initiated?

A

below 85 knots

17
Q

The autobrake system is only available through which of the following?

A

Normal brake system

18
Q

Which autobrake setting provides maximum braking?

19
Q

When are autobrakes disarmed?

A

DISARM or OFF are selected, manual brakes are applied, or any Thrust Lever is advanced

20
Q

For landing, the 5 levels of autobrake settings modulate autobrake pressure based on what?

A

Deceleration rate

21
Q

Body gear steering is reactivated when decelerating past what speed?

22
Q

Rudder pedals will steer the nosewheel up to what angle?

23
Q

The tiller will steer the nosewheel up to what angle?

A

70 degrees

24
Q

Which hydraulic brake systems have antiskid protection?

A

Normal and alternate

25
Is it possible to stop the aircraft with the brake accumulator?
No
26
How are alternate brakes powered?
Hyd system 1 or system 2 if 1 is unpressurized
27
What does the BRAKE SOURCE light indicate?
Loss of Hydraulic system 4, 2, and 1
28
Which hydraulic system pressurizes the parking brake accumulator?
4
29
Can the parking brake be set with only the alternate brake hydraulic system pressurized?
Yes
30
How can parking brakes be set?
Hyd system 2 alternate brakes and normal brakes
31
During gear retraction, how is main gear wheel rotation stopped?
Brakes are applied on the main gear wheels automatically
32
During alternate gear extension, how are the gear uplocks and gear door latches released?
Electically
33
After landing when does autobrake application begin?
Main wheels have spun up and all Thrust Levers are closed
34
Autobrakes are available with what?
Normal brakes
35
How are autobrakes powered?
Hydraulic system 4