7 Flight Controls

44問 • 4ヶ月前

Via

通報

問題一覧

The pitch direct law is:

a direct side stick to elevator relationship

When is the THS not available?

after yellow and green failure

The PFD displays in amber the message “USE MAN PITCH TRIM” in

Direct Law

Which surfaces are used for lift dumping?

all spoilers

Which signals cause rudder pedal movement?

rudder trim signals

If ELAC 1 and 2 have failed:

the elevator and pitch trim are controlled by SEC 1 or 2

If FAC 1 and 2 have failed:

the rudder can always be controlled from the pedals

When both sticks are moved in the same or opposite direction:

the surface movement is proportional to the algebraic sum of the deflections of both sticks

The elevator, ailerons, spoilers are:

hydraulically activated and electrically controlled

Rudder control is electrical for yaw damping and trim:

yes

What statement is correct:

ground spoiler function: all spoilers deploy

How many control modes are there on the elevators servo jacks?

3 - active, damping and centering

What are the limits for maneuvre protection:

c. a and b are correct

Which ELAC normally controls the elevators and the stabilizer:

ELAC 2

How many hydraulic motors drive the screw jack of the stabilizer:

How many electric motors can control the hydraulic motor of the stabilizer:

If neither ELAC 1 nor ELAC 2 are available, pitch control is automatically transferred to:

SEC 1 or SEC 2

In normal law, the flight mode changes to the landing mode when passing:

50 ft

At landing when passing 30 ft:

the altitude is progressively reduced to 2º nose down over a period of 8 secs.

How can a deactivated stick be reactivated:

by momentary action on either stick take over push buttons

In roll normal law, the bank angle protection is active when bank angle is:

> 67 degrees

The roll normal law provides combined control of the:

ailerons + spoilers 2 to 5 + rudder

If ELAC 1 and ELAC 2 have failed:

roll control is provided by spoilers only

In flight, if a WTB (wing tip brake) is activated, can you release it:

What happens when SFCC 1 fails:

flaps and slats operate at half speed

If one Flap power control unit fails, what happens:

flaps at half speed

If CONF. 0 is not selected after take-off, the flaps automatically retract at:

210 kts

After an automatic retraction of the flaps with CONF. 1, the flaps will automatically re-extend when speed decreases:

Is it possible to select an intermediate position with the flaps and slats selector:

If you are flying at an angle of attack more than Alpha Prot, what happens when you release the stick:

speed returns to Alpha Prot

When ALT LAW is active, the High Speed and High Angle of Attack protections are:

lost

When ALT LAW is active, the Yaw Damping is:

available (damper authority is limited to ±5 degrees of rudder deflection)

When in CONF 1+F, the flaps retract to 0º automatically at 210 kts:

Automatic Retraction function

How many hydraulic systems activate the rudder:

Lift augmentation is achieved on each wing by:

2 flap surfaces + 5 slat surfaces

Slat retraction from 1 to 0 is inhibited if angle of attack exceeds 8.5º or speed goes down below 148 KTS, this function is called:

Alpha/Speed Lock

In alternate law, the change to direct law occurs when:

landing gear down or at the selection of flaps 2 (LGCIU 1 + 2 fault)

Slats SYS 1 fault on the ECAM warning display means:

the slat channel in one SFCC has failed

With hydraulic blue system remaining and before landing gear extension, the flight control law is:

alternate

In flight control normal law, the stall warning is activated:

angle of attack corresponding to stall warning cannot be reached in normal law

The pitch normal law provides:

manoeuvre + high angle of attack + high speed + pitch attitude protection

When is the THS not available?

after yellow and green hydraulic system failure

Flight control computers are:

2 ELACs - 3 SECs - 2 FACs

When bank angle protection is active, is auto trim is inoperative?

Yes

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CPL Radio Telephony (3)

Met 1

Met 1

Met 2

Met 2

Met 3

Met 3

Met 4

Met 4

Met 5

Met 5

Met 6

Met 6

Met 7

Met 7

Met 8

Met 8

Human Performance 3

Human Performance 3

Met 9

Met 9

Met 10

Met 10

AGK 1

AGK 1

AGK 2

AGK 2

AGK 3

AGK 3

問題一覧

The pitch direct law is:

a direct side stick to elevator relationship

When is the THS not available?

after yellow and green failure

The PFD displays in amber the message “USE MAN PITCH TRIM” in

Direct Law

Which surfaces are used for lift dumping?

all spoilers

Which signals cause rudder pedal movement?

rudder trim signals

If ELAC 1 and 2 have failed:

the elevator and pitch trim are controlled by SEC 1 or 2

If FAC 1 and 2 have failed:

the rudder can always be controlled from the pedals

When both sticks are moved in the same or opposite direction:

the surface movement is proportional to the algebraic sum of the deflections of both sticks

The elevator, ailerons, spoilers are:

hydraulically activated and electrically controlled

Rudder control is electrical for yaw damping and trim:

yes

What statement is correct:

ground spoiler function: all spoilers deploy

How many control modes are there on the elevators servo jacks?

3 - active, damping and centering

What are the limits for maneuvre protection:

c. a and b are correct

Which ELAC normally controls the elevators and the stabilizer:

ELAC 2

How many hydraulic motors drive the screw jack of the stabilizer:

How many electric motors can control the hydraulic motor of the stabilizer:

If neither ELAC 1 nor ELAC 2 are available, pitch control is automatically transferred to:

SEC 1 or SEC 2

In normal law, the flight mode changes to the landing mode when passing:

50 ft

At landing when passing 30 ft:

the altitude is progressively reduced to 2º nose down over a period of 8 secs.

How can a deactivated stick be reactivated:

by momentary action on either stick take over push buttons

In roll normal law, the bank angle protection is active when bank angle is:

> 67 degrees

The roll normal law provides combined control of the:

ailerons + spoilers 2 to 5 + rudder

If ELAC 1 and ELAC 2 have failed:

roll control is provided by spoilers only

In flight, if a WTB (wing tip brake) is activated, can you release it:

What happens when SFCC 1 fails:

flaps and slats operate at half speed

If one Flap power control unit fails, what happens:

flaps at half speed

If CONF. 0 is not selected after take-off, the flaps automatically retract at:

210 kts

After an automatic retraction of the flaps with CONF. 1, the flaps will automatically re-extend when speed decreases:

Is it possible to select an intermediate position with the flaps and slats selector:

If you are flying at an angle of attack more than Alpha Prot, what happens when you release the stick:

speed returns to Alpha Prot

When ALT LAW is active, the High Speed and High Angle of Attack protections are:

lost

When ALT LAW is active, the Yaw Damping is:

available (damper authority is limited to ±5 degrees of rudder deflection)

When in CONF 1+F, the flaps retract to 0º automatically at 210 kts:

Automatic Retraction function

How many hydraulic systems activate the rudder:

Lift augmentation is achieved on each wing by:

2 flap surfaces + 5 slat surfaces

Slat retraction from 1 to 0 is inhibited if angle of attack exceeds 8.5º or speed goes down below 148 KTS, this function is called:

Alpha/Speed Lock

In alternate law, the change to direct law occurs when:

landing gear down or at the selection of flaps 2 (LGCIU 1 + 2 fault)

Slats SYS 1 fault on the ECAM warning display means:

the slat channel in one SFCC has failed

With hydraulic blue system remaining and before landing gear extension, the flight control law is:

alternate

In flight control normal law, the stall warning is activated:

angle of attack corresponding to stall warning cannot be reached in normal law

The pitch normal law provides:

manoeuvre + high angle of attack + high speed + pitch attitude protection

When is the THS not available?

after yellow and green hydraulic system failure

Flight control computers are:

2 ELACs - 3 SECs - 2 FACs

When bank angle protection is active, is auto trim is inoperative?

Yes