320, Landing Gear Flashcards

1
Q

Alternate braking WITH antiskid activates automatically following:

A

Failure of the Green hydraulic system

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2
Q

The nose wheel steering is electrically controlled and hydraulically operated by the __________ hydraulic system.

A

Green (basic aircraft) or Yellow (enhanced aircraft)

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3
Q

The main gear and doors are electrically controlled and hydraulically operated by the _________ hydraulic system.

A

Green

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4
Q

Above ______ knots, provided the ground spoilers are armed, moving the thrust levers to idle signals the flight control system to deploy the ground spoilers.

A

72

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5
Q

The two Landing Gear Control Interface Units (LGCIU 1 & LGCIU 2):

A

Swap roles as controlling and back up of gear extension and retraction each time the landing gear is RAISED.

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6
Q

The maximum indicated airspeed for gear extension is ______ knots and for gear retraction is ______ knots.

A

250, 220

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7
Q

The landing gear is controlled by ____ Landing Gear Control Interface Units, or LGCIUs.

A

Two

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8
Q

The LGCIUs send information to various systems about whether the aircraft is on ground or in flight.

T/F?

A

True

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9
Q

Braking and nose wheel steering are controlled by the _________ Unit.

A

BSCU

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10
Q

Prior to takeoff, autobrakes can be armed using the ______ pushbutton.

A

MAX

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11
Q

Autobrakes MAX is used only for takeoff.

T/F?

A

True

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12
Q

When MAX is armed, maximum auto braking is immediately applied when the ______________ signal is triggered.

A

Ground spoiler deployment order

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13
Q

For normal braking:

Green hydraulic system pressure must be available.

At least one channel of the BSCU must be operational.

The A/SKID & NW STRG switch must be selected to ON.

All of the above

A

All of the above

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14
Q

If both the Green and Yellow hydraulic systems fail, braking is still possible through a________.

A

Dedicated accumulator

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15
Q

Alternate braking is available with accumulator pressure from the ________ hydraulic system.

A

Yellow

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