DOMANDE A RISPOSTA MULTIPLA

What is the cause of Standing Water condition?. Is caused by heavy rainfall and /or insufficient runway drainage with a depth of more than 6.3 mm. Is caused by heavy rainfall and /or insufficient runway drainage with a depth of less than 3 mm. Is caused by heavy rainfall and /or insufficient runway drainage with a depth of more than 3 mm. Is caused by heavy rainfall and /or insufficient runway drainage with a depth of more than 12 mm.

Reaching cruise FL, to ensure FMS prediction, how different of wind and temperature from forecast should crew reentry in?. Wind: 30kts, temp: 5°C. Not required, FMS will auto update. Wind: 30° or 30kts, temp: 5°C. Wind: 20° or 20kts, temp: 5°C.

Decreasing take off flap from 15° to 0° will probably result in a _____ Vlof: Increased. Reduced. Unchanged. Greatly reduced.

What is best angle climb speed on A320/21?. Mach 0.76. Green dot. Approximately turbulence speed. 250kts.

The effect on a too late rotation will be an: Decrease the ground roll but increase the climb ability. Increase the ground roll and decrease the climb ability. Decrease both the ground roll and climb ability. Increase the ground roll but climb ability will be good.

After calculating the SPD for takeoff, do we need to check against Minimum Speed?. Yes, anytime. No, if no speed correction. Yes, the speed is too low.

Other factors being equal, an increase in take-off weight will: Increase lift off speed and decrease stalling speed. Increase lift off speed and stalling speed remains. Weight has no effect on take-off speed or lift-off speed. Increase lift off speed and stalling speed.

What is the maximum speed for the use of windscreen wipers?. 240 kts. Green Dot. 250 kts. 230 kts.

What will trigger a fire warning?. Fire detection by Loops A and B together (Engine). Loops A and B failure within 7 seconds of each other (Engine). Fire detection by Loops A or B (Engine). Loops A and B failure within 7 seconds of each other (APU).

For CAT III operations with no DH what are the minimum visual references?. At least one centre line and one edge light each side should be visible. There is no requirement for visual contact with the runway. Two centre line lights (assuming 30m spacing). Either three centre line lights (assuming 15m spacing).

If the IAS is a "split" triangle, which of the following statements is correct?. It may be magenta or blue. It indicates a speed constraint. It will be magenta and signify a Managed Descent only. It will be magenta and signify a Managed Climb or Managed Descent.

What is the limiting speed for selecting the gear down?. 220 kt. 250 kt. Green dot. 260 kt.

When can the RAT be restored?. At any time. Below 140 kts. On the ground only. Below 100 kts.

The ECAM CTL PANEL "WHEEL" pushbutton switch has failed. What must you do to display the WHEEL page?. Use the STS button. Use the ALL button. Use the RECAL button. Transfer the SD to the F/O (or CAPT) using the SWTG PANEL.

Regarding FADEC, which of the following statements is true?. It can be energised on ground by putting ENG MODE SEL to START. Each FADEC has three channels. FADEC runs for 10 minutes after the aircraft is electrically powered-up. The FADEC is able to abort a MANUAL START.

What are the restrictions on ATC reports to an aircraft on finals?. Inside the O.M. - radio silence. Inside the O.M. - RVR reports only. Less than 1nm to touchdown - radio silence. Less than 3nm to touchdown - ILS failures only.

Initial actions when airborne after a "WINDSHEAR" warning?. TOGA PWR, ignore FD - pitch to 17.5°. TOGA PWR, sidestick fully back, maintain gear / flap config. TOGA PWR, follow FD pitch demand, if need sidestick fully back. TOGA PWR, follow FD pitch demand, raise landing gear.

"The MAN V/S CTL switch is ... ... operative in the MAN pressurisation mode: - hold up to OPEN the outflow valve". ... inoperative if the DITCHING switch is ON”. ... operative at all times, and it controls the outflow valve". ... operative in the MAN pressurisation mofe: - hold up to OPEN the safety valve".

What is the maximum runway slope?. +1% / -2%. +2% / -1%. +/-1%. +/-2%.

What happens if EMER CANC button on the ECAM control panel is pressed?. EWD Amber Warnings are transferred to the STS S.D. If pressed for more than 3 seconds, cautions will be suppressed. EWD Red Warnings are transferred to the STS S.D. Aural Warnings are inhibited for the remainder of the flight.

"Below the passenger door window is a red CABIN PRESSURE light which …. ... is illuminated whenever the cabin pressure is greater than 2.5 Mb". ... cannot be seen from outside the aircraft". ... flashes if there is residual cabin pressure". ... flashes with residual pressure and slides armed".

Initial actions in event of a rejected Take-Off at more than 72 kts?. Call "STOP", REVERSE THR MAX, Reverse Idle By 80 kts. Call "STOP", REVERSE THR MAX. Call "STOP", REVERSE THR MAX, Maximum Foot Brakes. Call "STOP", REVERSE THR MAX, Speed Brakes Full.

What is the maximum speed for flight with the cockpit side window open?. 230 kts. 195 kts. 200 kts. Green Dot.

"Pressing the ECAM control panel RCL push-button switch ... ... displays the STATUS page on the lower ECAM". ... continuously scrolls through all the System Displays". ... displays the LANDING MEMO on the E.W.D". ... for more than 3 seconds, will recall any CANCELLED CAUTIONS".

EGPWS uses which BARO information?. Captain's. First Officer's. The pilot whose autopilot is engaged. The lower setting of the Captain's and First Officer's settings.

What is the duration of the Passenger Oxygen supply?. Between 15 and 20 minutes, depending on cabin altitude. 20 minutes. 15 minutes after oxygen compartment door activation. 15 minutes after the mask is pulled towards the passenger seat.

How is the optimum touchdown point marked on the runway?. Red barrettes. Large white painted rectangles on the runway surface. Green centreline lights. Yellow edge lights.

What is the minimum speed for use of full reverse thrust?. 50 kt. 60 kt. 75 kt. 70 kt.

What information is given by the speed trend arrow on the PFD?. The direction the speed should be adjusted to achieve the required speed. The speed attained in 10 seconds with constant acceleration. The ECON speed range during descent. The speed attained in 5 seconds with constant acceleration.

What is the sequence of actions, on the FCU, in order to start an emergency descent (structural failure)?. Select lower ALT and PULL, HDG knob - turn left or right and PULL, SPEED knob, PULL, MACH / SPEED target adjust. PULL and select lower ALT, HDG knob - PULL and turn left or right, MACH / SPEED changeover button - PRESS. Select lower ALT and PUSH, HDG knob - PULL and turn left or right, SPEED knob, PULL, MACH / SPEED changeover button - PRESS. Select lower ALT and PULL, HDG knob - PULL and turn left or right, SPEED knob, PULL and descend at Mᴍᴏ/Vᴍᴏ minus 10 kts.

What happens when the APU MASTER switch is selected to on?. The APU Intake Flap opens and the starter motor engages when the flap is fully open. The APU Intake Flap opens. The APU Intake Flap opens and the starter motor engages immediately. The APU Fuel Pump will operate.

Which is true with regard to the PTU?. It is inhibited from electrical power-up until second engine start. It operates if the Green or Yellow system pressure falls below 2600 psi. It is inhibited between engine starts. It is used as a back-up following a leak in the Green or Yellow systems.

Which of the following is a correct starter limitation?. After 3 failed start attempts, allow one hour cooling. Maximum continuous cranking is 3 minutes. The max speed for starter engagement is 20% N2, (recommended 10%). After 4 failed start attempts, allow one hour cooling.

If the radar on the ND sweeps from the centre outwards, what does it mean?. Weather radar is being used to show EGPWS terrain. It is giving a TEST pattern. Weather radar picture is offset due to a fault. NAV Database is being used to show EGPWS terrain.

Which lights go off when the gear is retracted?. Turn Off and Wing. Logo and Land. Nose and Turn Off. Nose and Land.