SYSTEMS LAY 2,3

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.

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

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

The air deflectors

The ramp toes

The kneeling system.

The stabilizer struts

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.

Clear air turbulence

Sandstorms

Wet hail.

Dry snow

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.

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)

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

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).

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.

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

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.

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

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