Landing Gear Flashcards

(30 cards)

1
Q

Why are there two triangles for each gear on the ECAM WHEEL page

A

Each triangle represents the gear position detected by one of the two LGCIUs

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2
Q

The landing gear hydraulic safety valve is controlled by

A

The gear lever and ADIRUs 1 and/or 3

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3
Q

Which statement is true concerning the green hydraulic system as it relates to normal landing gear extension

A

Hydraulic system remains pressurized with gear extended

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4
Q

The landing gear extension and retraction is controlled electrically by

A

LGCIU 1 or 2

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5
Q

With the gear NOT down, what causes the red landing gear DOWN arrow to illuminate

A

RA < 750 feet with power at approach settings and flaps not 0

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6
Q

The landing gear DOWN arrow illuminates red with associated ECAM L/G GEAR NOT DOWN warning if the landing gear is not down and

A

Flaps 3 or FULL selected with both radio altimeters inoperative

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7
Q

According to the graphic what is the position of the landing gear

A

One LGCIU has failed and the gear is downlinked

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8
Q

What is a characteristic of landing gear gravity extension

A

Noswheel steering is deactivated

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9
Q

Which landing gear system is lost with a green hydraulic failure

A

Nose wheel steering

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10
Q

With a green hydraulic system failure only, which brake system is not available

A

Autobrakes

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11
Q

How do you stop an airplane with a failed parking brake, during engine start

A

Restore braking with the brake pedals

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12
Q

What happens if the A/SKID & N/W STRG switch is turned off

A

Brakes revert to the alternate brake system without nose wheel steering or anti skid

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13
Q

A brake accumulator supplies at least _____ brake applications

A

7

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14
Q

Which hydraulic systems provides pressure for the ALTERNATE brakes

A

Yellow

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15
Q

Which hydraulic system is used for the parking brake

A

Yellow

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16
Q

Which hydraulic system provides brake pressure indications on the BRAKES and ACCU PRESS indicator

17
Q

What pilot action is required on landing with a loss of normal braking and a failure of the anti skid system

A

Monitor the brake pressure using the BRAKES and ACCU PRESS indicator

18
Q

What type of brakes are available with only a green hydraulic failure

A

Alternate brakes with anti skid

19
Q

When alternate braking is available without antacid due to a BSCU failure, pedal pressure must be controlled to prevent wheel lockup and

A

Brake pressure must be limited to a maximum of 1000 PSI on the BRAKES and ACCU PRESS indicator

20
Q

The anti skid system is deactivated with

A

Groundspeed less than 20 knots

21
Q

Which system is not active if a takeoff is rejected below 72 knots

22
Q

The BSCUs control

A

Antiskid operation

23
Q

Which hydraulic systems supplies pressure for nose wheel steering

24
Q

What does the green NW STRG DISC ECAM memo indicate

A

A lever on the towing electrical box is in the towing position and the nose wheel steering system is deactivated

25
If the PEDALS DISC button is pushed and held what happens
Rudder pedal control of the nose wheel steering is disconnected
26
What does an amber NW STRG DISC ECAM memo indicate
The nose gear steering has been deactivated for towing and the first engine is started
27
Automatic braking is initiated by the
Ground spoiler extension command
28
The green DECEL light on the AUTO/BRK panel illuminates when
Actual airplane deceleration equals 80% of selected rate
29
The auto brake system can be disarmed by
Applying sufficient brake pedal pressure to one pedal
30
After landing, where would you look to find the actual brake temperature
On the ECAM WHEEL page