LANDING GEAR | 暗記メーカー

暗記メーカー

LANDING GEAR

49問 • 1年前

問題一覧

1

After T/O the left main gear shock absorber remains in compressed position:

The gear cannot be retracted, gear lever is blocked

2

After a landing gear gravity extension, is it possible to restore normal landing gear operation if green hydraulic pressure is available:

Yes

3

After landing you retract the ground spoilers by bringing thrust levers from reverse to idle. The auto brake is now disarmed:

No

4

After lift off, is brakes HOT warning on ECAM still available:

Yes, gear down or up

5

Alternate braking using the yellow system. Autobrake is:

Lost

6

Are there any mechanical visual gear down lock indicators:

No

7

Auto Braking is initiated by:

Ground spoilers extension

8

Brake pressure from the hydraulic accumulator is still available:

In alternate braking (without anti-skid)

9

During an approach you get a master warning and ECAM: "Gear Not Down!" The reason is:

L/G not down locked and Flaps at 3 or Full and both radio altimeters failed.

10

Following ADIRS 1 and ADIRS 3 failure, is the anti-skid still available?

Yes

11

Handwheel and pedals are operated simultaneously:

Signals are mathematically added

12

How many turns are necessary to extend the landing gear by gravity using the hand crank:

Three turns clockwise

13

Hydraulic pressure to the landing gear is supplied up to:

260 kts

14

In flight, with the parking brake set to ON, a message on ECAM shows PARK BRK:

In amber

15

Is it possible (system wise) to lower the gear by gravity above 260 kts?

Yes

16

L/G position is indicated by:

One panel on center instrument panel and ECAM Wheel page

17

Landing Gear indicator panel UNLK light illuminates red if:

Gear isn’t locked in the selected position

18

Landing gear can be extended by:

Green hydraulic system or mechanical gravity extension

19

MAX braking has been selected: take off being aborted, engines in reverse, you have forgotten to arm the ground spoilers, is autobrake activated:

Yes

20

Maximum speed for landing gear retraction is:

220 kts

21

Nose wheel steering by rudder pedals is limited to:

up to 6° depending on A/C speed

22

Nose wheel steering is available:

A/C speed below 80 kts one ENG running, towing lever normal position, A/C on ground

23

Nose wheel steering is powered by:

Yellow hydraulic system

24

On ECAM WHEEL page, a green arc appears on one wheel indicator meaning the brake temperature is above:

100°C

25

On the WHEEL page of ECAM, AUTO BRK is flashing green for 10 seconds when:

Auto brake is disengaged

26

On the RAMP with APU running, parking brake set ON a message on ECAM shows PARK BRK:

In green

27

Setting the parking brake ON deactivates the auto brake:

False

28

Setting the parking brake deactivates all braking modes, except the anti-skid:

False

29

System page "WHEEL": L/G position indicators (triangles), LH shows green triangles (gear down)? RH has no triangles shown. The L/G is down and locked:

Yes

30

The A/SKID and N/W STRG switch is set to off:

Anti-skid and nose wheel steering are deactivated

31

The HOT light on the BRK FAN pushbutton illuminates when brake temperature reaches:

300°C

32

The MAX speed at which the landing gear may be extended is:

250 kts

33

The MAX speed with landing gear extended (VLE) is:

280 kts / M..67

34

The alternate brake system uses:

(The yellow hydraulic system) and (The hydraulic accumulator) are correct

35

The anti-skid system gets its references speed from:

ADIRU 1, 2 or 3

36

The brake and accumulator pressure gauge shows pressure:

From both yellow brake system and brake accumulator

37

The brakes are actuated by two independent systems, pressurized by the:

Yellow and Green hydraulic system

38

The braking systems are:

Green or yellow with anti-skid, yellow without anti-skid, parking brake

39

The handwheel in the cockpit provide a wheel steering angle of:

75°

40

The landing gear indicator panel receives the information from microswitches and proximity detectors connected to:

LGCIU 1

41

The nose wheel steering is powered by:

Hydraulic system

42

The principle of the anti-skid is:

Comparing wheel speed with A/C reference speed

43

The red arrow, near the landing gear lever illuminates when:

Landing gear is not locked down in landing configuration.

44

What is the MAX tire speed:

195 kts

45

When both hand wheel are operated simultaneously, the signals:

Are mathematically summed

46

When is pressure in the nose wheel steering system shut off:

With towing lever in towing position or both engines are shut down or aircraft in flight

47

When the autobrake operates, it can be disarmed by:

Any

48

Which ADIRS's close the safety valve of the green hydraulic supply when speed > 260 kts?

ADIRS 1 and 3

49

With green hydraulic system available, you find the A/SKID and N/W STG switch in OFF position:

Braking is alternate, nose wheel steering is lost

B777 - Part 8

B777 - Part 8

Angelo Ortiz · 50問 · 3年前

B777 - Part 8

B777 - Part 8

50問 • 3年前

B777 - Part 3

B777 - Part 3

Angelo Ortiz · 50問 · 3年前

B777 - Part 3

B777 - Part 3

50問 • 3年前

B777 - Part 6

B777 - Part 6

Angelo Ortiz · 50問 · 3年前

B777 - Part 6

B777 - Part 6

50問 • 3年前

B777 - Part 4

B777 - Part 4

Angelo Ortiz · 50問 · 3年前

B777 - Part 4

B777 - Part 4

50問 • 3年前

B777 - Part 1

B777 - Part 1

Angelo Ortiz · 50問 · 3年前

B777 - Part 1

B777 - Part 1

50問 • 3年前

B777 - Part 7

B777 - Part 7

Angelo Ortiz · 50問 · 3年前

B777 - Part 7

B777 - Part 7

50問 • 3年前

B777 - Part 9

B777 - Part 9

Angelo Ortiz · 28問 · 3年前

B777 - Part 9

B777 - Part 9

28問 • 3年前

B777 - Part 2

B777 - Part 2

Angelo Ortiz · 50問 · 3年前

B777 - Part 2

B777 - Part 2

50問 • 3年前

B777 - Part 5

B777 - Part 5

Angelo Ortiz · 50問 · 3年前

B777 - Part 5

B777 - Part 5

50問 • 3年前

AIA - VUL

AIA - VUL

Angelo Ortiz · 100問 · 2年前

AIA - VUL

AIA - VUL

100問 • 2年前

Underwriting

Underwriting

Angelo Ortiz · 66問 · 2年前

Underwriting

Underwriting

66問 • 2年前

Airplanes and Aerodynamics

Airplanes and Aerodynamics

Angelo Ortiz · 49問 · 2年前

Airplanes and Aerodynamics

Airplanes and Aerodynamics

49問 • 2年前

Airplane Instruments, Engines and Systems

Airplane Instruments, Engines and Systems

Angelo Ortiz · 77問 · 2年前

Airplane Instruments, Engines and Systems

Airplane Instruments, Engines and Systems

77問 • 2年前

Airport, ATC and Airspace

Airport, ATC and Airspace

Angelo Ortiz · 88問 · 2年前

Airport, ATC and Airspace

Airport, ATC and Airspace

88問 • 2年前

Federal Aviation Regulations - Part 1

Federal Aviation Regulations - Part 1

Angelo Ortiz · 100問 · 2年前

Federal Aviation Regulations - Part 1

Federal Aviation Regulations - Part 1

100問 • 2年前

Federal Aviation Regulations - Part 2

Federal Aviation Regulations - Part 2

Angelo Ortiz · 89問 · 2年前

Federal Aviation Regulations - Part 2

Federal Aviation Regulations - Part 2

89問 • 2年前

Airplane Weight and Balance

Airplane Weight and Balance

Angelo Ortiz · 10問 · 2年前

Airplane Weight and Balance

Airplane Weight and Balance

10問 • 2年前

Medical Factors and Decision Making

Medical Factors and Decision Making

Angelo Ortiz · 25問 · 2年前

Medical Factors and Decision Making

Medical Factors and Decision Making

25問 • 2年前

Weather and Services

Weather and Services

Angelo Ortiz · 87問 · 2年前

Weather and Services

Weather and Services

87問 • 2年前

Navigation

Navigation

Angelo Ortiz · 30問 · 2年前

Navigation

Navigation

30問 • 2年前

問題一覧

1

After T/O the left main gear shock absorber remains in compressed position:

The gear cannot be retracted, gear lever is blocked

2

After a landing gear gravity extension, is it possible to restore normal landing gear operation if green hydraulic pressure is available:

Yes

3

After landing you retract the ground spoilers by bringing thrust levers from reverse to idle. The auto brake is now disarmed:

No

4

After lift off, is brakes HOT warning on ECAM still available:

Yes, gear down or up

5

Alternate braking using the yellow system. Autobrake is:

Lost

6

Are there any mechanical visual gear down lock indicators:

No

7

Auto Braking is initiated by:

Ground spoilers extension

8

Brake pressure from the hydraulic accumulator is still available:

In alternate braking (without anti-skid)

9

During an approach you get a master warning and ECAM: "Gear Not Down!" The reason is:

L/G not down locked and Flaps at 3 or Full and both radio altimeters failed.

10

Following ADIRS 1 and ADIRS 3 failure, is the anti-skid still available?

Yes

11

Handwheel and pedals are operated simultaneously:

Signals are mathematically added

12

How many turns are necessary to extend the landing gear by gravity using the hand crank:

Three turns clockwise

13

Hydraulic pressure to the landing gear is supplied up to:

260 kts

14

In flight, with the parking brake set to ON, a message on ECAM shows PARK BRK:

In amber

15

Is it possible (system wise) to lower the gear by gravity above 260 kts?

Yes

16

L/G position is indicated by:

One panel on center instrument panel and ECAM Wheel page

17

Landing Gear indicator panel UNLK light illuminates red if:

Gear isn’t locked in the selected position

18

Landing gear can be extended by:

Green hydraulic system or mechanical gravity extension

19

MAX braking has been selected: take off being aborted, engines in reverse, you have forgotten to arm the ground spoilers, is autobrake activated:

Yes

20

Maximum speed for landing gear retraction is:

220 kts

21

Nose wheel steering by rudder pedals is limited to:

up to 6° depending on A/C speed

22

Nose wheel steering is available:

A/C speed below 80 kts one ENG running, towing lever normal position, A/C on ground

23

Nose wheel steering is powered by:

Yellow hydraulic system

24

On ECAM WHEEL page, a green arc appears on one wheel indicator meaning the brake temperature is above:

100°C

25

On the WHEEL page of ECAM, AUTO BRK is flashing green for 10 seconds when:

Auto brake is disengaged

26

On the RAMP with APU running, parking brake set ON a message on ECAM shows PARK BRK:

In green

27

Setting the parking brake ON deactivates the auto brake:

False

28

Setting the parking brake deactivates all braking modes, except the anti-skid:

False

29

System page "WHEEL": L/G position indicators (triangles), LH shows green triangles (gear down)? RH has no triangles shown. The L/G is down and locked:

Yes

30

The A/SKID and N/W STRG switch is set to off:

Anti-skid and nose wheel steering are deactivated

31

The HOT light on the BRK FAN pushbutton illuminates when brake temperature reaches:

300°C

32

The MAX speed at which the landing gear may be extended is:

250 kts

33

The MAX speed with landing gear extended (VLE) is:

280 kts / M..67

34

The alternate brake system uses:

(The yellow hydraulic system) and (The hydraulic accumulator) are correct

35

The anti-skid system gets its references speed from:

ADIRU 1, 2 or 3

36

The brake and accumulator pressure gauge shows pressure:

From both yellow brake system and brake accumulator

37

The brakes are actuated by two independent systems, pressurized by the:

Yellow and Green hydraulic system

38

The braking systems are:

Green or yellow with anti-skid, yellow without anti-skid, parking brake

39

The handwheel in the cockpit provide a wheel steering angle of:

75°

40

The landing gear indicator panel receives the information from microswitches and proximity detectors connected to:

LGCIU 1

41

The nose wheel steering is powered by:

Hydraulic system

42

The principle of the anti-skid is:

Comparing wheel speed with A/C reference speed

43

The red arrow, near the landing gear lever illuminates when:

Landing gear is not locked down in landing configuration.

44

What is the MAX tire speed:

195 kts

45

When both hand wheel are operated simultaneously, the signals:

Are mathematically summed

46

When is pressure in the nose wheel steering system shut off:

With towing lever in towing position or both engines are shut down or aircraft in flight

47

When the autobrake operates, it can be disarmed by:

Any

48

Which ADIRS's close the safety valve of the green hydraulic supply when speed > 260 kts?

ADIRS 1 and 3

49

With green hydraulic system available, you find the A/SKID and N/W STG switch in OFF position:

Braking is alternate, nose wheel steering is lost