A320 Prep Question Bank PDF

Question Option 1 Option 2 Option 3...

Question Option 1 Option 2 Option 3 Option 4 Which of the following AC busses can be powered by the emergency generator? AC BUS 2 AC BUS 1 BAT BUS AC ESS and AC ESS SHED busses Select the correct statement about an engine relight in flight: APU bleed can be used to assist with an engine startDuring throughout an automatic the entirestart flight in envelope flight, the FADEC In flight may the not FADEC need to always engagecommands the starter motor a starter-assisted if the Automatic engineair start is start wind is unavailable milling at a in sufficient flight N2 If the rudder pedals are at full deflection at normal taxi speed, what will the NWS angle be? 20° 16° 6° 10° During an automatic start sequence on the ground when does the ignition start and stop? Ignition starts as soon as the engine MASTER is set Ignition to ON, and starts stops at 22% when N2, N2and is more stopsthan when50% N2 Ignition is more starts thanat56% an N2 of 16%, and stops whenIgnition N2 is more starts than when 50% the MODE selector is set to IGN/START, and stops when N2 is greater than 43% What is output power of each of the AC generators? IDG 100KVA, APU 100KVA, emergency generator 5KVA, IDG 90 Static KVA,Inverter APU 90 1KVA KVA, emergency generator IDG 115KVA, 5 KVA, APU Static115KVA, Inverter emergency 1 KVA generator IDG15KVA, 90KVA,Static APU Inverter 90KVA, 1KVA emergency generator 23KVA, Static Inverter 5KVA How many flight control computers are there? 7: 2 x ELACs, 3 x SECs, 2 x FACs 7: 3 x ELACs, 2 x SECs, 2 x FACs 5: 2 x ELACs, 3 x SECs 8: 3 x ELACs, 3 x SECs, 2 x FACs What is the normal order of priority for supplying power to AC BUS 1? EXT PWR, APU, GEN1 then GEN2 GEN1, EXT PWR, APU, then GEN2 APU, EXT PWR, GEN1 then GEN2 (GEN1, GEN2), EXT PWR then APU Which LGCIU normally controls the retraction cycle? LGCIU 1 is the master, and LGCIU 2 is the slave If LGCIU LGCIU1 1fails, controls LGCIU the2left takes hand over main all and functions nose LGCIU automatically gears, 1 isLGCIU the master 2 controls whenthe either right APhand is offmain or AP1 One gear isLGCIU engaged, controls otherwise one complete LGCIU 2gear is the cycle, master then switches over automatically to the other LGCIU at the completion of the retraction cycle. It also switches over in the case of failure Regarding speed symbols on the PFD, which statement is true? The yellow speed trend arrow indicates the speed theManaged aircraft will speed reach is represented in 15 sec by a magenta Selected speed speed bug is represented by a magenta speed Machbug No. is not displayed below 0.6 Can you reconnect an IDG in flight? No, it is not possible Yes, push and hold the IDG pb until the GEN Yes, fault provided light is the no longer engineilluminated is running or windmilling Yes, but only after contacting maintenance control What is the cockpit handset typically used for? For PAs and SATCOM To transmit to ATC via VHF PA announcements to the cabin only To transmit to ATC via HF What does a blue ON light mean in the EXT PWR pushbutton? The external power line contactor is closed. EXT PWR The willexternal automatically power contactor connect toisthe open AC1 andExternal or AC2 busses power isfollowing pluggedthe in and normal parameters bus tie priorities are Thenormal EXT PWR contactor is closed. EXT PWR takes priority over all other sources of AC power The MAINT BUS switch is used to supply only ground services. Where is it located? Behind the co-pilot's seat There is no such switch on the A320 On the ceiling in the forward galley just outside In thethe flight overhead deck panel When the PACK FLOW selector is positioned to HI, airflow is: 100% of normal 80% of normal 120% of normal 50% more than normal What happens to the wing and engine anti-ice valves when the hot air supply is unavailable? Wing anti-ice valves open, engine anti-ice valves open Wing anti-ice valves close, engine anti-ice valves Wing anti-ice close valves close, engine anti-ice valves Wing open anti-ice valves open, engine anti-ice valves close For routine access into the cockpit by the cabin crew, the buzzer sounds: For a few sec With a triple high-low chime For a few min Continuously Which of the following statements regarding the FWC, ELAC and FAC is true (select the most complete answer)? The FWC computes and displays the characteristic speed The FWC on the generates PFD, thethe ELAC OVERSPEED performs the warnings, A.FLOOR The FWC theprotection, generates ELAC performs and the OVERSPEED the theFAC LOWis SPEED onlywarnings, active protection, The when theFWC ELAC theand AP generates the performs is engaged FAC the only theOVERSPEED HIGH performs SPEED yawwarnings, related protection, functions theand ELAC the (rudder FAC performs computes trim/limits/damping) the HIGH and SPEED displaysprotection, characteristic andspeeds the FAC ononly the performs PFD yaw related functions (rudder trim/limits/damping) If the Engine Interface Unit (EIU) fails, what information does the FADEC loose access to? Master switch, and engine mode selector position Engine sensors Air data from the ADIRS Thrust lever angle What areas of the aircraft are anti-iced with hot air? Engine air intakes, all leading edge slats on each wing Engine air intakes, the three outboard leading Engine edgeair slats intakes, of each andwing, the three the THS outboard and rudder leading Engine leading edgeair slats edge intakes, of each thewing four outboard leading edge slats of each wing, and the flight deck windows What happens if the DITCHING push button is selected ON? (select the most complete answer) A close signal will be sent to the outflow valve, avionics A close ventilation signal inlet will be andsent avionics to theventilation outflow valve, outlet A close emergency signal will ram beair sent valve, to the andoutflow pack flow valve, control avionics A close valves signal ventilation will be inlet sent and to outlet, the emergency emergency ramram airair valve, valve, andand pack pack flow flow control control valves valves When does the generator load turn amber on the ELEC SD page? The engine generator load is above 108% for more than The 10 engine sec generator load is above 108% The engine generator load is above 105% The engine generator load is above 100% Above what cabin altitude will the cabin oxygen masks be deploy automatically? 9,550 ft 14,000 ft 16,000 ft 12,000 ft Select the correct starter limitation for the CFM engine: A 20 minute cooling period is required following 3 failed A 10 start second cycles pause is required between each A 15 start minute cyclecooling period is required following A4 60 failed minute startcooling cycles period is required following 3 consecutive start attempts Which of the following statements is true regarding the APU Fire Extinguishing system (select the most complete answer)? There are two fire agent bottles for the APU one is discharged Immediately automatically after an APU if afire firewarning is detected on the on 3 sec ground, theafter ground, the a fire APU and warning, the automatically other thecan APU be shuts automatically discharged down, and 3by shuts sec the theafter extinguisher flight down.ancrew The APUat flight FIRE bottle anycrew time warning discharges should on follow the