Quiz
SYSTEMS LAY 2,3
Perguntas do quiz (18)
1About the engine fire extinguishing method, select the FALSE statement.
- AEach Bottle has two squibs that enable the discharge of the extinguishing agent
- BThe DISCH light come ON when the Extinguisher bottle is faulty.
- CAs soon as the ENG FIR pb-sw is pressed, a countdown of 10 s starts in the ECAM
- DIf 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.
2Talking about the APU FIRE DETECTION LOGIC, if one fire loop fails after the other within 5 s:
- Aan APU FIRE alert will be triggered.
- Ban APU FIRE DET FAULT will be triggered
- Can APU FIRE LOOP A/B FAULT will be triggered
- DNone of the above
3All the smoke detectors are located on the ceiling of the airplane.
- AVerdadeiro
- BFalso
4Select the correct option. If one Hydraulic System Monitoring Unit (HSMU) fails:
- AThe associated hydraulic system remains inoperative
- BThe fire shutoff valve indications and reservoir level indictions are not lost
- CThe system pressure and pump pressure remain monitored.
- DAll of the above are correct
5Choose the incorrect option. The Door and Ramp Actuation System (DRAS) operates:
- AThe air deflectors
- BThe ramp toes
- CThe kneeling system.
- DThe stabilizer struts
6The Ram Air Turbine (RAT) is always hydraulically powered by the YELLOW hydraulic system.
- AVerdadeiro
- BFalso
7About the GPWS function, select the FALSE sentence:
- AThe mode 1 alerts are inhibited when the aircraft goes below 10 ft
- BIf flaps or landing gear input data are not valid or if systems are failed, the associated flap or gear mode 4 alerts are inhibited
- CThe NORM TAWS integrity is degraded if the TERR function is not active
- DMode 5 is active during approach, when in CLEAN configuration, and the aircraft is between 1000 ft and 30 ft AGL.
8Select the false sentence. The WXR radar does not detect:
- AClear air turbulence
- BSandstorms
- CWet hail.
- DDry snow
9The TCAS determines:
- AA) The relative bearing of the intruders
- BThe distance between the aircraft and the intruders, and the rate of separation or closure
- CThe relative altitude of the intruders, if the intruders have Mode-C or a Mode-S transponder
- DAll of the above.
10Select the false sentence. The TACT TAWS predictive mode automatically engages when:
- AThe TACT TAWS is selected via the TAWS sw
- BThe aircraft is whether in ground or airborne.
- CThe TACT TAWS Database is available
- DPisition accuracy is within the limits (EPUH < 60 m, EPUv < 150 ft)
11About the Windshear display, select the correct sentence:
- AOnly the red circles appear when the NTD range is 10 NM in one of the ROSE modes
- BIt doesn’t appear when in ground mapping display mode.
- CWhen the NTD range is above 10 NM, the red circles appear associated with yellow radial lines
- DWhen 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
12The TCAS inhibits all the RAs below 2000 ft AGL in descent:
- AVerdadeiro
- BFalso
13Select the correct sentence. In case of an engine failure, V2 computation ensures:
- AV2 is reached before 55ft
- BSufficient margin over maximum control speeds
- CA minimum flight path angle during the first segment of 2.7%
- DA minimum flight path angle during the second segment of 3% (2% in ROS).
14Which one of this conditions is not true if you want to be able to engage the AP:
- AThe active flight control law must be the normal or the alternate (Prot Degraded) law
- BAt least two ADRs must be available
- CThe AFS Cp must be available
- DAt least one IR is available.
15Select 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:
- AThe bank angle exceeds 80º right or left
- BThe pitch in CONF0 to 3 goes below 30º nose down
- CThe high angle-of-attack protection is active
- DThe pitch is above 35º
16Select the correct sentence about an FLS BEAM COMPUTATION when the MAP IS BEFORE THE RUNWAY THRESHOLD:
- AThe 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)
- BThe course of the FLS beam is the course that is stored with the MAP in the navigation database
- CThe slope of the FLS beam is the FPA stored with th MAP in the navigation database
- DAll of the above.
17The stall warning always has priority over the overspeed warning, except when all the following conditions occur:
- AThe aircraft is in clean configuration, the aircraft speed is above M 0.64 and the aircraft is
above 25000 ft. - BThe aircraft is in landing configuration, the aircraft speed is above 230 kts and the aircraft is below 1000 ft
- CThe aircraft is in clean configuration, the aircraft speed is above 230 kts and the aircraft is below 1000 f
- DNone of the above
- AThe aircraft is in clean configuration, the aircraft speed is above M 0.64 and the aircraft is
18Select the false sentence about when the ATOC function is only available:
- AAt TOGA power
- BWhen the aircraft speed is below 130 kt
- Cin any flight control law
- DOn ground, when the aircraft ground speed is above 45 kt
Informações
- Descrição
- Preguntas de LAY 2 y 3
- Autor
- Juan Garcia
- Idioma
- Español
- Visualizações
- 51
- Etiquetas
- Avaliação
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