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SYSTEMS LAY 2,3

Description

Preguntas de LAY 2 y 3
Juan Garcia
Quiz by Juan Garcia, updated more than 1 year ago
Juan Garcia
Created by Juan Garcia over 2 years ago
42
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Resource summary

Question 1

Question
About the engine fire extinguishing method, select the FALSE statement.
Answer
  • 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.

Question 2

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

Question 3

Question
All the smoke detectors are located on the ceiling of the airplane.
Answer
  • True
  • False

Question 4

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

Question 5

Question
Choose the incorrect option. The Door and Ramp Actuation System (DRAS) operates:
Answer
  • The air deflectors
  • The ramp toes
  • The kneeling system.
  • The stabilizer struts

Question 6

Question
The Ram Air Turbine (RAT) is always hydraulically powered by the YELLOW hydraulic system.
Answer
  • True
  • False

Question 7

Question
About the GPWS function, select the FALSE sentence:
Answer
  • 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.

Question 8

Question
Select the false sentence. The WXR radar does not detect:
Answer
  • Clear air turbulence
  • Sandstorms
  • Wet hail.
  • Dry snow

Question 9

Question
The TCAS determines:
Answer
  • 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.

Question 10

Question
Select the false sentence. The TACT TAWS predictive mode automatically engages when:
Answer
  • 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)

Question 11

Question
About the Windshear display, select the correct sentence:
Answer
  • 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

Question 12

Question
The TCAS inhibits all the RAs below 2000 ft AGL in descent:
Answer
  • True
  • False

Question 13

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

Question 14

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

Question 15

Question
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:
Answer
  • 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

Question 16

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

Question 17

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

Question 18

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