Ldggr

Question 1

Wheel brake temperatures are displayed:

Answer 1

On the gear synoptic.

Question 2

During takeoff, RTO braking will not occur unless groundspeed is above:

Answer 2

85 knots.

Question 3

During landing, auto brake application begins:

Answer 3

A. When both thrust levers are retarded to idle.

C. With wheel spinup.

Question 4

Select a TRUE statement about alternate gear extension.

Answer 4

The landing gear free falls to the down and locked position.

Question 5

The B787 has both Nosewheel and Main gear steering.

Answer 5

B. False

Question 6

How do you know that the parking brake is set?

Answer 6

The EICAS memo message PARKING BRAKE SET is displayed.

Question 7

Which autobrake mode provides the highest declaration rate for landing?

Answer 7

MAX AUTOBRAKE

Question 8

The landing gear is held in the up and locked position by:

Answer 8

Hydraulically actuated mechanical locks.

Question 9

Which of the following is true regarding gear down and locked sequence:

Answer 9

Hydraulic pressure unlocks the uplocks, gear falls by gravity, hydraulic pressure closes the gear doors.

Question 10

The landing gear speed limits for all configurations and modes are?

Answer 10

270 / .82

Question 11

Following landing gear retraction, with switches in the ON postion, the Nose Gear Landing and Taxi lights:

Answer 11

extinguish as soon as retraction begins.

Question 12

Hydraulic power for gear retraction and extension is supplied by the:

Answer 12

Center hydraulic system.

Question 13

If an RTO is initiated below 85 knots groundspeed, the RTO autobrake function:

Answer 13

Does not operate.

Question 14

Which of he following woll disarm the Autobrake system and cause the EICAS “AUTOBRAKES” advisory message to display?

Answer 14

A. Selection of the Autobrake switch to Disarm
B. Autobrake system is inoperative for any reason.
C. RTO is initiated above 85kts but autobraking has not been applied.

Question 15

The autobrake system disarms if:

Answer 15

A. Pedal braking is applied
B. Either thrust lever is advanced.
C. Speedbrake lever moved to DOWN detent.

Question 16

What does the alternate landing gear extension system use to extend the gear?

Answer 16

A dedicated DC hydraulic pump and trapped center hydraulic system fluid.

Question 17

What is provided by the RTO function of the autobrake system?

Answer 17

The RTO function automatically applies maximum brake pressure when the thrust levers are retarded to idle above 85 knots groundspeed.

Question 18

If center hydraulic system fluid quantity is low, is it likely that the gear actuation system has all available pressure sources?

Answer 18

No, if center hydraulic system fluid quantity is low, the center system fluid is isolated to provide an alternate extension source.

Question 19

The alternate gear extension system utilizes trapped fluid from the :

Answer 19

Center hydraulic system

Question 20

Nose gear steering will be inoperative after loss of the:

Answer 20

complete center hydraulic system.

Question 21

Maximum autobrake pressure is provided while operating in the:

Answer 21

Rejected takeoff mode only.

Question 22

When using only battery power for braking, _____ protection is available.

Answer 22

A. touchdown
B. normal anti-skid
C. locked wheel

Question 23

The CONFIG PARKING BRAKE warning level EICAS indicates:

Answer 23

The parking brake is set when either engines thrust is in the takeoff range on the ground.