Brakes & Landing Gear

Question 1

What is the function of the landing gear transfer valve during gear retraction when #1 engine RPM drops below a limit value that is less than idle

Answer 1

?

Question 2

When does the landing gear transfer unit operate (aircraft airborne)

Answer 2

?

Question 3

How is wheel rotation stopped during gear retraction

Answer 3

Nose wheel by snubbers and main wheels by auto- hydraulic braking

Question 4

How is the landing gear extended manually

Answer 4

Individual manual extension handles release up locks

Question 5

Which conditions are necessary to use the nose wheel steering

Answer 5

“A” system pressurized, gear lever in DOWN position, nosewheel steering switch NORMAL

Question 6

Which hydraulic system supplies pressure for normal brakes

Answer 6

System “B” for all main wheel brakes

Question 7

How does the ANTI-SKID system control normal braking when a single wheel skid is detected

Answer 7

Modulates pressure to the individual wheel brake

Question 8

Autobrakes are available with a system “B” failure as long as the alternate brakes are operational

Answer 8

False

Question 9

What does a momentary AUTO BRAKE DISARM light indicate when RTO mode is selected

Answer 9

Successful automatic self- test

Question 10

A successful test of the Autobrake RTO feature is indicated by

Answer 10

After the RTO position is selected, the AUTO BRAKE DISARM light illuminates briefly and extinguishes

Question 11

What occurs during a rejected takeoff between 60 and 90 knots with RTO selected

Answer 11

Autobrakes will not be applied; AUTO BRAKE DISARM light illuminates

Question 12

Autobrakes may be disarmed after landing by

Answer 12

All answers are correct

Question 13

What occurs if a landing is made with RTO selected

Answer 13

No automatic braking, AUTO BRAKE DISARM light comes on

Question 14

When would braking with only accumulator pressure occur

Answer 14

With loss of “A” and “B” system hydraulic pressure

Question 15

What is the hydraulic pressure source for the alternate brake system

Answer 15

Hydraulic system “A”

Question 16

How is the alternate brake system activated

Answer 16

Automatically when “B” HYD pressure is low

Question 17

While setting the parking brakes, the ANTI-SKID INOP light illuminated. This indicates

Answer 17

A malfunction in the parking brake system

Question 18

Auto Brakes are available

Answer 18

With “B” system pressure

Question 19

Brakes should not be applied until after touchdown

Answer 19

True

Question 20

A Landing Gear Transfer Unit provides a backup hydraulic power source to

Answer 20

Retract the landing gear in the event #1 engine fails on takeoff

Question 21

What is the maximum speed at which a pilot may extend the landing gear

Answer 21

270 kts

Question 22

Is the RTO position of the autobrakes required for takeoff if the autobrakes are operational

Answer 22

Yes

Question 23

A check of the brake wear indicators is valid when the parking brake is

Answer 23

Set with hydraulic pressure

Question 24

When the aircraft is towed, the ____ should be off or a steering lockout pin must be installed

Answer 24

“A” system pressure

Question 25

With failure of both "A" and "B" hydraulic systems, approximately what will the brake pressure indicator read when no more accumulator braking is available

Answer 25

1000 psi

Question 26

What is the maximum nosewheel turning angle in either direction that can be commanded by the rudder pedals

Answer 26

7 degrees

Question 27

In flight , with the landing gear up, a warning horn that can not be silenced with the HORN CUTOUT will sound

Answer 27

Anytime the flaps are at 25 degrees

Question 28

What is the maximum speed at which the pilot may retract the landing gear

Answer 28

235 kts

Question 29

The gear is down and locked with three green lights. What is the speed limit

Answer 29

320 kts

Question 30

When must the autobrake RTO feature be selected

Answer 30

For all takeoffs with autobrakes operative