A320 Bank
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Quiz areas includes:- General questions; Air conditioning and pressurisation; 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.Which lights go off when the gear is retracted
- A.
Nose and Turn Off
- B.
Turn Off and Wing
- C.
Nose and Land
- D.
Logo and Land
- 2.Which colour code is correct for push button switches?
- A.
AMBER - immediate action : BLUE - temporary operation
- B.
GREEN - temporary operation : WHITE - abnormal position
- C.
WHITE - temporary operation : GREEN - normal operation
- D.
RED - immediate action : 2 DOTS "not used" part of switch
- 3."Below the passenger door window is a red CABIN PRESSURE light which ...
- A.
... flashes if there is residual cabin pressure."
- B.
... is illuminated whenever the cabin pressure is greater than 2.5 mb."
- C.
... flashes with residual pressure and slides armed."
- D.
... cannot be seen from outside the aircraft."
- 4."Set on LO, the actual pack flow may be ...
- A.
... HI due to APU bleed supplying."
- B.
... NORM due to APU bleed supplying."
- C.
... HI due to air conditioning temperature demands."
- D.
... NORM or HI due to single ack operation."
- 5."The MAN V/S CTL switch is ...
- A.
...operative at all times, and it controls the outflow valve."
- B.
... operative in the MAN pressurisation mode: - hold up to OPEN the outflow valve."
- C.
... operative in the MAN pressurisation mofe: - hold up to OPEN the safety valve."
- D.
... inoperative if the DITCHING switch is ON."
- 6.What is displayed on the COND S.D. if the primary channel of the Zone Controller has failed?
- A.
"ALTN MODE"
- B.
"PACK REG"
- C.
Double crosses ( XX )
- D.
"TRIM AIR VALVE FAULT"
- 7.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℃.
- 8.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.
- 9.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.
- 10.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.
- 11.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) ]
- 12.
- 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.
- 13.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).
- 14."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."
- 15.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.
- 16.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.
- 17.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.
- 18.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.
- 19.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.
- 20.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.
- 21.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)
- 22.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.
- 23.What is the effect of selecting the GEN1 LINE to OFF?
- A.
Fuel pump operation is transferred to AC ESS BUS.
- B.
GEN 1 is fed directly onto the AC ESS BUS.
- C.
GEN 1 is de-energised.
- D.
GEN 1 is line contactor opens.
- 24.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.
- 25.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.
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