Landing Gear Flashcards

1
Q

The maximum NWS angle using pedals

A

6 degrees

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2
Q

The maximum NWS using hand wheel

A

75 degrees

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3
Q

The steering system receives actuating hydraulic pressure when

A

The Antiskid and NWS switch is on.
Towing control lever is in the normal position.
At least one engine is running.
The aircraft is on the ground.

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4
Q

NW STRG DISC appears in amber when the nose wheel steering selector is in the towing position and if

A

One engine is running

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5
Q

The normal brake system uses ——— hydraulic pressure

A

Green

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6
Q

The alternate brake system uses ——- hydraulic pressure

A

Yellow

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7
Q

A changeover between the two BSCU channels takes place at each

A

DOWN landing gear lever selection or in case one channel fails

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8
Q

The anti skid system is deactivated below

A

20 knots

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9
Q

MAX autobrake mode cannot be armed

A

In flight

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10
Q

Automatic braking is activated when

A

The command for ground spoiler extension is detected (for LO or MED).
The command for ground spoiler extension is detected and the wheel speed is above 40 knots (for MAX)

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11
Q

For autobrake to activate at least —- SEC’s must be operative

A

Two

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12
Q

The accumulator can supply at least —- full brake applications

A

Seven

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13
Q

The accumulator maintains the parking pressure for at least

A

12 hours

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14
Q

Medium autobrake mode sends progressive pressure to the brakes — seconds after the ground spoilers deploy in order to decelerate the aircraft at —m/s

A

Two seconds

3 m/s

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15
Q

LO autobrake mode sends progressive pressure to the brakes — seconds after the ground spoilers deploy in order to decelerate the aircraft at —m/s

A

2 seconds

2 m/s

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16
Q

DECELERATIONS light comes on green when

A

The actual deceleration is 80% of the selected rate

17
Q

The nose landing gear retracts

A

Forward

18
Q

The main landing gears retract

A

Inboard

19
Q

The LGCIU’s switch over automatically at the completion of the

A

Retraction cycle

20
Q

When the aircraft is flying faster than ——- a safety valve automatically cuts off hydraulic supply to the landing gear system.

A

260kt

21
Q

The LGCIU’s receive position information from the

A

Landing gear.
Cargo doors.
Landing flap.

22
Q

The Landing Gear Indicator Panel is connected to

A

LGCIU 1. Therefore if LGCIU 1 is U/S there will be no gear indication on this panel. LGCIU 2 will still indicate on lower ECAM.