Airbus A320 System Practice Test!
(229).jpg "Airbus A320 System Practice Test! - Quiz")
Airbus A320 System Practice Test! Quiz areas include:- General questions; Air conditioning and pressurization; Automatic Flight; Auxiliary Power Unit; Communications; Electrical; Energy Equipment; Fire Protection; Flight Controls; Flight Instruments; Fuel; Hydraulic Power; Ice and Rain Protection; Landing Gear; Navigation; Pneumatics; Power Plant; Limitations; Minimum Equipment List; Emergency Procedures; Low Visibility; EIS and FMS.
- 1.What are the Fan Air Valve and pre-cooler used for?
- A.
Initial cooling of air after entering the pack.
- B.
Cooling H.P. air only.
- C.
Cooling bleed air in accordance with pack demands.
- D.
Cooling bleed air to a maximum of 200℃.
- 2.The Trim Air Valves:
- A.
Are electrically controlled by the zone controller.
- B.
Adjusts temperature by adding cold air.
- C.
Mix fresh air from the packs with recirculated cabin air.
- D.
Regulate pack flow depending on number of passengers.
- 3.With the PACK FLOW selector to NORM, what will the actual flow be?
- A.
LO or NORM or HI.
- B.
Always NORM.
- C.
NORM or HI.
- D.
NORM or LO.
- 4.The Avionics Vent System has two "conditions" - GROUND and FLIGHT. When does the transition from GROUND to FLIGHT occur?
- A.
After second engine start.
- B.
At lift-off.
- C.
At 100 kts. on the take-off roll.
- D.
When the thrust is set for take-off.
- 5.Regarding the A/THR indications on the FMA, which is true?
- A.
ATHR in blue - [ ARMED (actual thrust = TLA) ]
- B.
ATHR in white - [ ARMED (actual thrust = TLA) ]
- C.
ATHR in blue - [ ACTIVE (actual thrust is limited by TLA) ]
- D.
ATHR in white - [ ACTIVE (actual thrust is always less than TLA) ]
- 6.When can both Autopilots be engaged at the same time?
- A.
After the APPROACH PHASE is activated on the MCDU.
- B.
After APPR is armed on the FCU.
- C.
After LOC capture.
- D.
After G/S capture.
- 7.The APU has been switched off, but it has not stopped . Why is this?
- A.
The APU Fuel Pump continuing to run.
- B.
The Air Intake Flap failing to close.
- C.
A cooling period, which occurs on all APU shutdowns.
- D.
A cooling period (following use of APU Bleed).
- 8."The APU may be started ...
- A.
... at or below 35,000 feet only."
- B.
... at or below 25,000 feet only."
- C.
... at or below 300 knots only."
- D.
...throughout the normal flight envelope."
- 9.What happens when the APU MASTER switch is selected to on?
- A.
The APU Intake Flap opens and the starter motor engages immediately
- B.
The APU Intake Flap opens and the starter motor engages when the flap is fully open.
- C.
The APU Fuel Pump will operate.
- D.
The APU Intake Flap opens.
- 10.What does the AVAIL light on the START switch indicate?
- A.
APU starter disengagement.
- B.
APU electrical power can be used.
- C.
N speed greater than 75%
- D.
ECB power-up check is satisfactory.
- 11.When does the APU starter engage?
- A.
When the FLAP is fully open and the start switch is pressed on.
- B.
When the Oil Pressure reaches 7 p.s.i.
- C.
When the MASTER SW is pressed on.
- D.
When the START SW is pressed on.
- 12.On the overhead, when should AUDIO SWITCHING be selected to CAPT 3?
- A.
The Captain is using RMP tuning of the NAVAIDS.
- B.
The Captain's ACP has failed.
- C.
The Captain's loudspeaker has failed.
- D.
Both RMPs have failed.
- 13.For the ACP, which is true?
- A.
The PA TRANSMISSION key operates like other transmission keys.
- B.
The ON VOICE key enables audio to be heard on the loudspeakers.
- C.
The RESET key transfers associated ACP (1 or 2) operation to ACP3
- D.
The RESET key cancels all CALL lights.
- 14.On the ACP, what does an amber light on a Transmission Key indicate?
- A.
Failure of the associated transmitter.
- B.
Failure of the associated transmitter and receiver.
- C.
SELCAL operation only.
- D.
SELCAL operation or a call from maintenance or the cabin.
- 15.What are the correct actions if RMP 1 fails?
- A.
Switch it off : use ACP 2
- B.
Switch it off : use RMP 3 only.
- C.
Switch it off : use RMP 3 or RMP 2.
- D.
Use the AUDIO SWITCHING switch (on the overhead panel)
- 16.Which is true of the AC ESS Bus in the event of an AC BUS 1 FAULT?
- A.
It cannot be powered.
- B.
It can be powered from AC BUS 2, if so selected.
- C.
It will be powered automatically from AC BUS 2.
- D.
It will be powered by the emergency generator.
- 17.What happens if, in flight, with the hydraulic Blue System inoperative (fluid loss), the MAN ON switch (on the EMER ELEC PWR panel) is pressed?
- A.
The Emergency Generator will be driven by the Blue Hydraulic System.
- B.
The Emergency Generator will be driven directly by the RAT.
- C.
The RAT will not deploy.
- D.
The RAT will extend, but the Emergency Generator will not operate.
- 18.The aircraft is on the chocks. All sources (Engine, APU and External Power) are ON. Which of the following is true?
- A.
The External Power is supplying the network.
- B.
If the Engines are shut down, the APU will supply the network.
- C.
If the Engines are shut down, External Power will supply the network.
- D.
If the APU is shut down, the External Power will supply the network.
- 19.Which conditions will cause the Cabin Signs and Lighting to illuminate?
- A.
Above 11,000 feet (approx.) cabin altitude, regardless of the SEAT BELTS and NO SMOKING switch positions.
- B.
Above 11,000 feet (approx.) cabin altitude, provided the EMERGENCY EXIT light switch is at ARM or ON.
- C.
Above 10,000 feet (approx.) cabin altitude, provided the EMERGENCY EXIT light switch is at ARM.
- D.
If the cabin altitude exceeds 14,000 feet.
- 20.What is the duration of the Passenger Oxygen supply?
- A.
Between 15 and 20 minutes, depending on cabin altitude.
- B.
20 minutes.
- C.
15 minutes after the mask is pulled towards the passenger seat.
- D.
15 minutes after oxygen compartment door activation.
- 21.If, on opening a door with the slide armed, the slide does not auto-inflate, what are the correct actions?
- A.
Close the door and use another exit.
- B.
Manually open the Air Valve.
- C.
Recycle the Door Control Handle.
- D.
Recycle the Slide Arming lever.
- 22.What will trigger a fire warning?
- A.
Loops A and B failure within 7 seconds of each other (Engine).
- B.
Loops A and B failure within 7 seconds of each other (APU).
- C.
Fire detection by Loops A and B together (Engine).
- D.
Fire detection by Loops A or B (Engine).
- 23.Following an engine fire, when will AGENT pushbutton lights illuminate?
- A.
SQUIB when FIRE switch is pushed; DISCH when squib has fired.
- B.
SQUIB when squib has failed; DISCH when squib has fired.
- C.
SQUIB as soon as the fire is detected.
- D.
SQUIB when FIRE switch is pushed; DISCH when extinguisher bottle is depressurised.
- 24.What are the pitch and roll limits in Normal Law configuration?
- A.
Pitch + 30° (+ 25° at low speed), - 15°, Roll : 67°
- B.
Pitch + 30° (+ 25° at low speed), - 10°, Roll : 67°
- C.
Pitch + 25° (+ 20° at low speed), - 15°, Roll : 67°
- D.
Pitch ± 30°. Roll 45°
- 25.What does the sidestick control between neutral and full aft in alpha prot?
- A.
Alpha.
- B.
Altitude.
- C.
Airspeed.
- D.
G.
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