15.1.14 Perform Landing Gear system Operations and Procedures Flashcards

1
Q

Which hydraulic system is used to actuate the landing gear?

A

The center hydraulic system

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2
Q

Selecting DN on the ALTN GEAR EXTEND switch:

A

Releases all door and gear uplocks, free-falling the gear to the down locked position

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3
Q

What is the maximum that the tiller can turn the nose wheel?

A

65 degrees

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4
Q

What is the maximum that the rudder pedals can turn the nose wheel?

A

7 degrees

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5
Q

If normal and alternate brakes are lost including the reserve brake system, what can be used to stop the airplane?

A

The brake accumulator can provide several braking applications or be used. It can also be used to set the parking brake

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6
Q

What hydraulic system powers the alternate brakes?

A

The center system

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7
Q

The “BRAKE SOURCE” light will illuminate when?

A

Both normal and alternate brake system pressures are low

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8
Q

What is the maximum airspeed to retract or extend landing gear of a B767:

A

270 knots or mach .82

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9
Q

A TAILSKID light illuminates and the EICAS advisory message TAILSKID indicates?

A

The tailskid position disagrees with the landing gear lever position

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10
Q

The BRAKE TEMP light illuminates for values above?

A

Above 5

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