Landing Gear System Flashcards

1
Q

The maximum tire ground speed is _____.

A

195 kts

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2
Q

Arming the RTO feature is _________ for all takeoffs, if operable

A

required

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3
Q

The brake wear indicators should extend beyond the brake flange with the parking brake _____________.

A

set

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4
Q

Hydraulic power for retraction, extension, and nose wheel steering is normally supplied by _______________.

A

hydraulic system A

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5
Q

The normal brake system is powered by _________ and the alternate brakes system is powered by _______.

A

hydraulic system B; hydraulic system A

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6
Q

Antiskid protection is provided _________________.

A

on both brake system (normal and alternate)

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7
Q

During retraction, the ____________ stop rotation of the main gear wheels.

A

brakes automatically

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8
Q

During retraction, the nose wheels retract forward into the wheel well and nose wheel rotation is stopped by _________.

A

snubbers

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9
Q

After retraction, the main gear are held in place by ______and the nose gear is held in place by ______________.

A

mechanical uplocks; an overcenter lock

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10
Q

Moving the LANDING GEAR lever to the OFF position ____________________.

A

removes hydraulic pressure from the landing gear system

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11
Q

An illuminated red landing gear indicator light indicates the related landing gear is in disagreement with LANDING GEAR lever position (in transits or unsafe), or ____________________.

A

landing gear is not down and locked (with either or both forward thrust levers retarded to idle and below 800 feet AGL)

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12
Q

An extinguished green landing gear indicator light indicates _______________.

A

landing gear is not down and locked

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13
Q

When the LANDING GEAR lever is moved to UP, _______________.

A

the landing gear retracts

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14
Q

When the LANDING GEAR lever is moved to DN, hydraulic system ___ pressure is used to release the uplocks. The landing gear extends by _______________.

A

A; hydraulic pressure, gravity, and air loads

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15
Q

The landing gear is down and locked _________ green landing gear indicator light(s) (center panel and/or overhead panel) for each gear is/are illuminated.

A

as long as one

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16
Q

The landing gear transfer unit allows hydraulic system B to supply the volume of hydraulic fluid required to raise the landing gear at the normal rate when airborne, LANDING GEAR lever is positioned UP, either main landing gear is not up and locked and ________________.

A

Nº1 enginbe RPM drops below a limit value

17
Q

Opening the Manual Extension Access Door _________ landing gear retraction.

A

disables

18
Q

Manual landing gear extension is possible with the landing gear lever ____________.

A

in any position

19
Q

Manual gear releases on the flight deck are used to_________ that allow the gear to_________ to the down and locked position.

A

release uplocks free-fall

20
Q

The nose wheel steering wheel _________________ rudder pedal steering.

A

overrides

21
Q

Nose wheel steering is available _____________________.

A

when the nose gear is in the down position and compressed by the wieght of the airplane

22
Q

Pushing the rudder pedal allows for nose wheel turning up to ______in either direction.

A

7 deg

23
Q

________ allows the aircraft to push back or be towed without depressurizing system A.

A

a lockout pin

24
Q

Placing the Nose Wheel Steering Switch to ALT, allows ____________ to provide power for nose wheel steering.

A

hydraullic system B

25
Q

If normal and alternate brake system pressure is lost, trapped hydraulic pressure in the brake accumulator can still provide ____________ or parking brake application.

A

several braking applications

26
Q

Skid, locked wheel, touchdown, and hydroplane protection is available ____________.

A

with the normal and alternate braking system

27
Q

If hydraulic system B is low or fails, _____________automatically supplies pressure to the alternate brake system

A

hydraullic system A

28
Q

The parking brake can be set with _________.

A

A or B hydraullic system, or the accumulator if A and B are not pressurized

29
Q

Normal hydraulic brake pressure as indicated on the brake accumulator _________.

A

3000 psi

30
Q

Anti-skid protection is provided in the _______________.

A

normal and alternate brake system

31
Q

An amber illuminated AUTO BRAKE DISARM light indicates _______________.

A

a malfunction exists in automatic braking system

32
Q

Placing the AUTO BRAKE Select Switch to 1, 2, 3, or MAX, selects desired ________for landing.

A

deceleration rate

33
Q

With the AUTO BRAKE Select Switch in RTO, maximum brake pressure is automatically applied when the thrust levers are retarded to idle at or above ____ knots.

A

90

34
Q

An amber illuminated ANTISKID INOP light indicates _______________.

A

a system fault is detected

35
Q

The auto brake system uses ______________ to provide maximum deceleration for rejected takeoff.

A

hydraullic system B pressure

36
Q

On dry runways, the maximum autobrake deceleration rate in the landing mode is _______ that produced by full pedal braking.

A

less than

37
Q

After the autobraking has started, any of the following pilot actions disarm the system immediately and illuminate the AUTO BRAKE DISARM light:

A

all answers are correct:

  • moving the speed brake lever to full forward or applying manual brakes
  • advancing the forward thrust levers except during teh first 3 seconds after touchdown for landing or applying manual brakes