About the engine fire extinguishing method, select the FALSE statement.
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.
Talking about the APU FIRE DETECTION LOGIC, if one fire loop fails after the other within 5 s:
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
All the smoke detectors are located on the ceiling of the airplane.
Select the correct option. If one Hydraulic System Monitoring Unit (HSMU) fails:
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
Choose the incorrect option. The Door and Ramp Actuation System (DRAS) operates:
The air deflectors
The ramp toes
The kneeling system.
The stabilizer struts
The Ram Air Turbine (RAT) is always hydraulically powered by the YELLOW hydraulic system.
About the GPWS function, select the FALSE sentence:
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.
Select the false sentence. The WXR radar does not detect:
Clear air turbulence
Sandstorms
Wet hail.
Dry snow
The TCAS determines:
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.
Select the false sentence. The TACT TAWS predictive mode automatically engages when:
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)
About the Windshear display, select the correct sentence:
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
The TCAS inhibits all the RAs below 2000 ft AGL in descent:
Select the correct sentence. In case of an engine failure, V2 computation ensures:
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).
Which one of this conditions is not true if you want to be able to engage the AP:
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.
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:
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
Select the correct sentence about an FLS BEAM COMPUTATION when the MAP IS BEFORE THE RUNWAY THRESHOLD:
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
The stall warning always has priority over the overspeed warning, except when all the following conditions occur:
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
Select the false sentence about when the ATOC function is only available:
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
