Landing Gear Flashcards

1
Q

Positioning the LANDING GEAR Lever _____ removes hydraulic pressure from the Landing Gear System.

A

OFF

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2
Q

The Lever Lock Override Trigger in the LANDING GEAR lever bypasses the _____ under certain conditions.

A

the lever lock if the lever lock solenoid fails

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3
Q

A Main Gear Position Light is not illuminated with the LANDING GEAR lever in the DOWN position. The Supplemental Gear Position light is green. The respective gear is

A

down and locked

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4
Q

The _____ supplies hydraulic fluid to raise the landing gear when Hydraulic System A engine-driven pump volume is lost due to an engine failure.

A

Landing Gear Transfer Valve

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5
Q

Opening the Manual Extension Access Door _____ Landing Gear _____.

A

disables / retraction

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6
Q

Pulling a Manual Gear Extension Handle _________ allowing the respective gear to free-fall.

A

releases the mechanical uplocks

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7
Q

With the Flaps greater than ________ pushing the Horn Cutout switch will not silence the Landing Gear Configuration Aural Warning (horn).

A

10

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8
Q

_____ supplies pressure to the Alternate Brake System if Normal Brake System pressure is low or fails.

A

Hydraulic System A automatically

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9
Q

Braking _____ if both Hydraulic Systems A and B are lost.

A

is available through a Brake Accumulator

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10
Q

_____ System(s) provide(s) skid”,” locked wheel”,” touchdown and hydroplane protection.

A

the Normal and Alternate Brake

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11
Q

Maximum braking automatically begins during a rejected takeoff _____.

A

above 90 knots and retarding the forward thrust levers to IDLE

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12
Q

Landing with the Autobrake set to RTO:

A

results in no autobraking

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13
Q

The Autobrake select switch allows selection of ____________ .

A

increasing rates of deceleration

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14
Q

Autobrakes”,” when engaged”,” _____ when thrust reversers and spoilers deploy during landing.

A

reduce pressure to maintain selected deceleration rate

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15
Q

Disarm the Autobrake System”,” after braking begins”,” by _____ .

A

All of the Above

1) applying manual brakes
2) moving the SPEED BRAKE lever to DOWN detent
3) advancing forward thrust lever(s) more than 3 seconds after landing

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16
Q

How do you set the PARKING BRAKE?

A

depress both brake pedals and pull the lever up and aft

17
Q

The PSEU detects a fault while in flight

A

the PSEU does not illuminate

18
Q

Hydraulic System B was operating normally. If Hydraulic System B is then lost (both pumps inoperative)”,” the Hydraulic Brake Pressure Accumulator indicates

A

approximately 3000 psi

19
Q

The Brake Accumulator

A

is pressurized from Hydraulic System B