Juan Garcia
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Preguntas de LAY 2 y 3

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Juan Garcia
Erstellt von Juan Garcia vor etwa 3 Jahre
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SYSTEMS LAY 2,3

Frage 1 von 18

1

About the engine fire extinguishing method, select the FALSE statement.

Wähle eine oder mehr der folgenden:

  • Each Bottle has two squibs that enable the discharge of the extinguishing agent

  • The DISCH light come ON when the Extinguisher bottle is faulty.

  • As soon as the ENG FIR pb-sw is pressed, a countdown of 10 s starts in the ECAM

  • If the fire alert is till activated after 30s , the flight crew can discharge the agen of the bottle of the adjacent engine, via the AGENT 2 pb.

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Frage 2 von 18

1

Talking about the APU FIRE DETECTION LOGIC, if one fire loop fails after the other within 5 s:

Wähle eine oder mehr der folgenden:

  • an APU FIRE alert will be triggered.

  • an APU FIRE DET FAULT will be triggered

  • an APU FIRE LOOP A/B FAULT will be triggered

  • None of the above

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Frage 3 von 18

1

All the smoke detectors are located on the ceiling of the airplane.

Wähle eins der folgenden:

  • WAHR
  • FALSCH

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Frage 4 von 18

1

Select the correct option. If one Hydraulic System Monitoring Unit (HSMU) fails:

Wähle eine oder mehr der folgenden:

  • The associated hydraulic system remains inoperative

  • The fire shutoff valve indications and reservoir level indictions are not lost

  • The system pressure and pump pressure remain monitored.

  • All of the above are correct

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Frage 5 von 18

1

Choose the incorrect option. The Door and Ramp Actuation System (DRAS) operates:

Wähle eine der folgenden:

  • The air deflectors

  • The ramp toes

  • The kneeling system.

  • The stabilizer struts

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Frage 6 von 18

1

The Ram Air Turbine (RAT) is always hydraulically powered by the YELLOW hydraulic system.

Wähle eins der folgenden:

  • WAHR
  • FALSCH

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Frage 7 von 18

1

About the GPWS function, select the FALSE sentence:

Wähle eine der folgenden:

  • The mode 1 alerts are inhibited when the aircraft goes below 10 ft

  • If flaps or landing gear input data are not valid or if systems are failed, the associated flap or gear mode 4 alerts are inhibited

  • The NORM TAWS integrity is degraded if the TERR function is not active

  • Mode 5 is active during approach, when in CLEAN configuration, and the aircraft is between 1000 ft and 30 ft AGL.

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Frage 8 von 18

1

Select the false sentence. The WXR radar does not detect:

Wähle eine der folgenden:

  • Clear air turbulence

  • Sandstorms

  • Wet hail.

  • Dry snow

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Frage 9 von 18

1

The TCAS determines:

Wähle eine der folgenden:

  • A) The relative bearing of the intruders

  • The distance between the aircraft and the intruders, and the rate of separation or closure

  • The relative altitude of the intruders, if the intruders have Mode-C or a Mode-S transponder

  • All of the above.

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Frage 10 von 18

1

Select the false sentence. The TACT TAWS predictive mode automatically engages when:

Wähle eine der folgenden:

  • The TACT TAWS is selected via the TAWS sw

  • The aircraft is whether in ground or airborne.

  • The TACT TAWS Database is available

  • Pisition accuracy is within the limits (EPUH < 60 m, EPUv < 150 ft)

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Frage 11 von 18

1

About the Windshear display, select the correct sentence:

Wähle eine der folgenden:

  • Only the red circles appear when the NTD range is 10 NM in one of the ROSE modes

  • It doesn’t appear when in ground mapping display mode.

  • When the NTD range is above 10 NM, the red circles appear associated with yellow radial lines

  • When two or more wind shear areas are near (less than 45º between their centers), a single pair of yellow lines appears on each side of the group of windshear areas

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Frage 12 von 18

1

The TCAS inhibits all the RAs below 2000 ft AGL in descent:

Wähle eins der folgenden:

  • WAHR
  • FALSCH

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Frage 13 von 18

1

Select the correct sentence. In case of an engine failure, V2 computation ensures:

Wähle eine oder mehr der folgenden:

  • V2 is reached before 55ft

  • Sufficient margin over maximum control speeds

  • A minimum flight path angle during the first segment of 2.7%

  • A minimum flight path angle during the second segment of 3% (2% in ROS).

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Frage 14 von 18

1

Which one of this conditions is not true if you want to be able to engage the AP:

Wähle eine oder mehr der folgenden:

  • The active flight control law must be the normal or the alternate (Prot Degraded) law

  • At least two ADRs must be available

  • The AFS Cp must be available

  • At least one IR is available.

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Frage 15 von 18

1

Select the TRUE statement. When flying with the Autopilot (AP), The pitch, the bank angle, the speed, and the angle-of-attack are out of normal range, when:

Wähle eine oder mehr der folgenden:

  • The bank angle exceeds 80º right or left

  • The pitch in CONF0 to 3 goes below 30º nose down

  • The high angle-of-attack protection is active

  • The pitch is above 35º

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Frage 16 von 18

1

Select the correct sentence about an FLS BEAM COMPUTATION when the MAP IS BEFORE THE RUNWAY THRESHOLD:

Wähle eine oder mehr der folgenden:

  • The anchor point is on a pseudo Final End Point (FEP) (that the FMS computes) and the TCH (threshold height + 50 ft when there is no TCH in the data)

  • The course of the FLS beam is the course that is stored with the MAP in the navigation database

  • The slope of the FLS beam is the FPA stored with th MAP in the navigation database

  • All of the above.

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Frage 17 von 18

1

The stall warning always has priority over the overspeed warning, except when all the following conditions occur:

Wähle eine oder mehr der folgenden:

  • The aircraft is in clean configuration, the aircraft speed is above M 0.64 and the aircraft is

    above 25000 ft.

  • The aircraft is in landing configuration, the aircraft speed is above 230 kts and the aircraft is below 1000 ft

  • The aircraft is in clean configuration, the aircraft speed is above 230 kts and the aircraft is below 1000 f

  • None of the above

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Frage 18 von 18

1

Select the false sentence about when the ATOC function is only available:

Wähle eine oder mehr der folgenden:

  • At TOGA power

  • When the aircraft speed is below 130 kt

  • in any flight control law

  • On ground, when the aircraft ground speed is above 45 kt

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