Ch.14 (Landing Gear) Flashcards

Landing Gear

1
Q

What does positioning the landing gear lever to OFF do?

A

Removes hydraulic pressure from the landing gear system

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2
Q

What is the purpose of the lever lock override trigger?

A

To bypass the landing gear lever lock in certain conditions

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3
Q

A gear position light is not illuminated with the landing gear lever in the down position. The supplemental gear position light is green, what is the gear position?

A

down and locked

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4
Q

What is the purpose of the landing gear transfer valve? Which fluid is used to operate the gear?

A

To supply the volume of hydraulic fluid needed to raise the landing gear at the normal rate when HYD SYS A engine driven pump volume is lost. HYD SYS B fluid is used

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5
Q

What effect does the manual extension access door have on the landing gear?

A

Normal landing gear retraction is disable if this door is left open

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6
Q

What does pulling a manual gear extension handle do?

A

Releases the respective landing gears mechanical uplock, allowing the gear to freefall

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7
Q

The landing gear configuration aural warning (horn) cannot be silenced beyond which flap setting?

A

beyond flaps 10

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8
Q

What supplies pressure to the alternate brake system if normal brake system pressure is lowor fails?

A

HYD SYS A automatically supplies pressure when normal braking pressure is low or failed

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9
Q

How is braking available if both HYD systems A and B are lost?

A

Brake accumulator. Provides 6 braking applications or parking brake pressure for 8
hours

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10
Q

Which brake system(s) provide(s) skid, locked wheel protection, touchdown protection and hydroplane protection?

A

Both normal and Alternate braking systems

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11
Q

When does RTO braking automatically begin during a rejected takeoff?

A

When the forward thrust levers are retarded to idle after reaching 90 kts wheelspeed

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12
Q

Landing with the Autobrake set to RTO results in what level of braking?

A

No autobraking will occur

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13
Q

What is the difference between Autobrake 1,2,3 and max?

A

Increases the rate of deceleration (kts/sec)

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14
Q

What effect does the thrust revers and spoiler deployment have on the autobraking rate?

A

No effect on the auto braking deceleration rate. Pressure is reduced to maintain the
selected deceleration rate

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15
Q

How is the autobrake system disarmed after braking begins?

A
  • Autobrake switch to OFF
  • Brake pedal pressed
  • Thrust lever moved out of IDLE position after having been on the ground for 3 +
    seconds
  • A fault in the Autobrake/antiskid systems
  • Speed brake lever movement from UP to DOWN
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16
Q

How do you set the parking brake?

A

Pull to the UP position and mechanically latched in place with hydraulic pressure
available

17
Q

*In flight, how will a PSEA-detected (Proximity Switch Electronic Unit) fault be indicated?

A

It is not annunciated?

18
Q

How is the brake accumulator pressurized?

A

HYD SYS B