Landing Gear

The autobrake system uses _______ to provide maximum deceleration for rejected takeoff. a) Hydraulic System A pressure b) Hydraulic System B pressure c) Hydraulic System A or B pressure

b) Hydraulic System B pressure

After the autobraking has started, any of the following pilot actions disarm the system immediately and illuminate the AUTO BRAKE DISARM light: a) moving speed brake lever to full forward or applying manual brakes b) advancing the forward thrust lever(s), except during the first 3 seconds after touchdown c) all answers are correct

c) all answers are correct

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 b) STBY; hydraulic pressure, gravity, and air loads c) B; gravity, and air loads

a) A; hydraulic pressure, gravity, and air loads

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) 60 b) 90 c) 120

b) 90

Antiskid protection is provided: a) on both brake systems (normal and alternate) b) with normal brakes only c) with alternate brakes only

a) on both brake systems (normal and alternate)

An illuminated red landing gear indicator indicates the related landing gear is in disagreement with the LANDING GEAR lever position (in transit 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) b) landing gear is up c) the landing gear manual extension must be used

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

Hydraulic power for retraction, extension, and nose wheel steering is normally supplied by: a) standby system b) hydraulic system A c) hydraulic system B

b) hydraulic system A

Placing the Nose Wheel Steering Switch to ALT allows _______ to provide power for nose wheel steering. a) the standby hydraulic system b) hydraulic system A c) hydraulic system B

c) hydraulic system B

Skid, locked wheel, touchdown, and hydroplane protection is available: a) only with the normal braking system b) with the normal and alternate braking system c) only with the alternate braking system

b) with the normal and alternate braking system

The brake wear indicators should extend beyond the brake flange with the parking brake: a) set b) released

a) set

Arming the RTO feature is _________ for all takeoffs, if operable. a) required b) not required

a) required

Moving the LANDING GEAR lever to the OFF position: a) is not recommended below 235 knots b) removes hydraulic pressure from the landing gear system c) engages the over center locks

b) removes hydraulic pressure from the landing gear system

An extinguished green landing gear indicator light indicates: a) landing gear is down and locked b) landing gear is not down and locked c) the landing gear manual extension must be used

b) landing gear is not down and locked

When the LANDING GEAR lever is moved to UP: a) the landing gear retracts b) the landing gear extends c) hydraulic pressure is removed from the landing gear

a) the landing gear retracts

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) No. 1 engine RPM drops below a limit value b) No. 2 engine RPM drops below a limit value c) the A electric hydraulic pump is inoperative

a) No. 1 engine RPM drops below a limit value

Manual gear releases on the flight deck are used to_________ that allow the gear to_________ to the down and locked position. a) engage uplocks; hydraulically extend b) release uplocks; free-fall c) release uplocks; hydraulically extend

b) release uplocks; free-fall

The nose wheel steering wheel _____ rudder pedal steering. a) works in the opposite direction of the b) is secondary to the c) overrides

c) overrides

Nose wheel steering is available: a) when the nose gear is in the down position and compressed by the weight of the airplane b) when the nose gear is in the down position c) at all times

a) when the nose gear is in the down position and compressed by the weight of the airplane

_______ allows the aircraft to push back or be towed without depressurizing system A. a) A bypass switch on the forward panel b) A lockout pin c) Pulling nose wheel circuit breaker

b) A lockout pin

If hydraulic system B is low or fails, _______ automatically supplies pressure to the alternate brake system. a) hydraulic system A b) electric friction c) standby system pressure

a) hydraulic system A

The parking brake can be set with: a) hydraulic system A b) hydraulic system B c) A or B hydraulic system, or the accumulator if A and B are not pressurized

c) A or B hydraulic system, or the accumulator if A and B are not pressurized

An amber illuminated AUTO BRAKE DISARM light indicates: a) the auto brakes are set to MAX b) the AUTO BRAKE select switch is set to OFF c) a malfunction exists in automatic braking system

c) a malfunction exists in automatic braking system

Placing the AUTO BRAKE Select Switch to 1, 2, 3, or MAX, selects desired ________ for landing. a) brake pressure b) deceleration rate c) air run

b) deceleration rate

An amber illuminated ANTISKID INOP light indicates: a) the anti-skid system need to be reset b) the auto brakes need to be armed c) a system fault is detected

c) a system fault is detected

On dry runways, the maximum autobrake deceleration rate in the landing mode is _______ that produced by full pedal braking. a) more than b) equal to c) less than

c) less than