32 Landing Gear Flashcards

1
Q

What structure is your nose landing gear and main attached to?

A

Nose = longitudinal members, Main = structural ribs of the nacelle.

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2
Q

How are your nose and main locked in the down position.

A

Nose = internal lock of actuator, Mains = Mechanical lock on drag brace.

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2
Q

How are your nose and main locked in the down position.

A

Nose = internal lock of actuator, Mains = Mechanical lock on drag brace.

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3
Q

What indication do you have for in transit

A

2 Red in-transit lights located in the gear handle.

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4
Q

How many hydraulically brake assemblies does the aircraft have?

A

4

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5
Q

What is the procedure to check the shimmy damper fluid level?

A

insert a wire approx 1/16.

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6
Q

What is used to prevent cavitation of the hydraulic power pack?

A

Bleed air, regulated to 18-20 psi.

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7
Q

What is the power pack made up of?

A

28V motor, pump, two-section reservoir, filter, fourway selector valve, relief valves, lock valves, gear-up pressure switch, low fluid sensor.

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8
Q

Plumbing for the normal extend mode and emergency extend mode is divided by what device?

A

shuttle valve.

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9
Q

What pressure will the gear up switch cut power to the motor? and when will it come back on?

A

2775, if it drops between 300-400.

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10
Q

What helps maintain the gear in the up position?

A

Acuumulator precharged to 800 psi.

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11
Q

What is the brake wear limit?

A

.200 or greater.

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12
Q

What method is recommended to bleed the brakes?

A

pressure pot bleeding, only gravity if neccessary.

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13
Q

What happens if the brake deice switch is not moved to the off position 10 minutes after take off?

A

The timing circuit in the brake deice control module, will close the shut off valves.

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