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Topic question bank: Type Specific Questions, A320

Questions and Answers

AIR

What are the benefits of a pack-off take-off?

A pack-off take-off involves temporarily switching off one or both air conditioning packs during takeoff to reduce engine bleed air demand. This provides several operational benefits:

  • Improved engine performance, as more air is available for thrust instead of being diverted to the pneumatic system.
  • Lower EGT during takeoff, which helps reduce engine wear and contributes to lower maintenance costs.
  • Increased takeoff performance margins, especially useful in hot and high conditions, or on short or contaminated runways.

Typically, the packs are automatically re-engaged after takeoff, during the climb phase.

How is the pneumatic system of the A320 controlled and monitored?

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Name the available sources of pneumatic air on the A320.

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Explain the role of the High Pressure Valve (HPV).

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How is the temperature of the bleed air controlled?

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What is the function of the crossbleed valve?

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Can the crossbleed valve be operated manually from the cockpit?

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Explain how the APU bleed is prioritized over engine bleed.

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Is it possible for both the APU and an engine to supply bleed air simultaneously?

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Can a single bleed source supply both air conditioning packs?

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What happens in case of an engine bleed source failure in flight?

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How is a bleed air leak indicated to the crew?

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What happens in case of a bleed leak?

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How are the hydraulic reservoirs pressurized on the A320?

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AUTOFLT

You read 2 FD 2 on your FMA. What does that mean?

The FMA message 2 FD 2 means that Flight Director 2 (from FMGC 2) is active on both PFDs, indicating that FMGC 1 has failed.

In this case:
- FMGC 2 becomes the master FMGC, providing guidance to both flight directors.
- The message confirms that FD 1 is no longer available due to the FMGC 1 failure.
- Lateral and vertical guidance are now entirely based on FMGC 2 data.

What does SRS mode do during takeoff?

SRS (Speed Reference System) mode provides vertical guidance through pitch control via the elevators, both during takeoff (SRS TO) and go-around (SRS GA). Although the logic is similar, there are key differences between the two:

During takeoff (SRS TO):
- Minimum vertical speed is protected at 120 ft/min, ensuring the aircraft maintains a positive climb gradient.
- Pitch angle is limited to 18° nose-up (or 22.5° in case of windshear).
- Speed target is limited to $V_{2}$ + 15 kt.

During go-around (SRS GA):
- Only a positive rate of climb is required (no specific minimum value).
- Same pitch protection as in TO: 18° max or 22.5° with windshear.
- Speed is protected to prevent exceeding VFE.
- Target speed is the greater of $V_{APP}$ or the speed at SRS engagement, limited to:
- 25 kt above VLS (15 kt if one engine inoperative),
- and 5 kt below $V_{MAX}$.

These protections ensure safe trajectory and speed management during both takeoff and go-around.

What is the minimum autopilot disconnection altitude for an ILS CAT II manual landing?

During an ILS CAT II manual landing, the autopilot must be disconnected by 80 ft AGL.

What are the main components of the Flight Management Guidance System (FMGS) on the A320?

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What are the two main functional parts of each FMGC, and what are their respective roles?

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How many Flight Management Guidance Computers (FMGCs) are installed on the A320?

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What are the modes of operation of the FMGC?

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You are preparing for an RNP approach, but the temperature is below the Baro-VNAV minimum limit. What do you do, and which vertical mode should you use?

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On the A320, what is the benefit of disconnecting the autopilot when using speedbrakes?

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What are the main lateral modes of the A320 autoflight system?

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What are the different vertical modes of the A320 autoflight system?

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What are the conditions required to engage the autopilot after takeoff?

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What is the minimum height to use the autopilot during an approach with F-G/S mode?

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What is the minimum height to use the autopilot during an approach in FINAL APP, V/S, or FPA mode?

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What is the minimum autopilot disconnection altitude in a circling approach?

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What is the minimum autopilot disconnection altitude for an ILS/MLS CAT I approach?

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What is the minimum autopilot disconnection altitude for an ILS/MLS CAT II or CAT III approach with autoland?

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What is the minimum autopilot disconnection altitude for an LPV approach with SLS and APPR 1 displayed on the FMA?

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What is the minimum height to re-engage the autopilot after a manual go-around?

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What is the minimum height to use the autopilot during all other phases of flight?

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ELEC

How many TRs are installed on the A320 and which buses do they supply?

There are 3 TRs: TR1 supplies DC BUS 1, TR2 supplies DC BUS 2, and ESS TR can power the essential DC circuit from the emergency generator, if the engine and APU generators all fail, or if TR 1 or TR 2 fails.

How many AC generators does the A320 have?

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What are the primary sources of AC power on the A320 while both engines are running?

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What is the function of the TRs (transformer rectifiers) on the A320?

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What are the DC sources available during normal operation?

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What is the role of the static inverter on the A320?

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What happens when both AC BUS 1 and AC BUS 2 are lost in flight?

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Which electrical sources are available on the ground with only batteries connected?

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What is the minimum battery voltage required before starting the APU?

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Which bus powers the APU starter?

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What is the function of the Bus Tie Contactors (BTCs)?

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What does the electrical system do automatically in case of generator overload?

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How is the electrical system split when operating on only one generator?

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What is the function of the Emergency Generator?

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When does the Emergency Generator automatically come online?

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How is the Emergency Generator powered?

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What is the priority order for AC power sources?

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Which bus does the RAT-powered Emergency Generator supply?

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What happens to the electrical system when the EMER ELEC config is set while the avionics smoke procedure is applied?

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Which bus powers the captain’s PFD and ND in emergency electrical configuration?

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What happens if both TRs 1 and 2 fail?

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How is DC ESS BUS powered if TR 1 fails?

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Can the APU supply electrical power in flight?

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What is the maximum altitude at which you can start the APU with batteries only?

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FCTL

Describe the high speed protection.

When high speed protection activates (VMO/MMO exceeded), the flight control law introduces positive spiral static stability toward 0° bank (instead of 33° in normal law). With the sidestick released, the aircraft will return to wings level.

Additional effects include:
- The bank angle limit is reduced from 67° to 40°.
- Pitch-down authority is progressively reduced as speed increases above VMO/MMO.
- A permanent nose-up input is introduced to help recover the aircraft.

In a dive:
- If the sidestick is neutral, the aircraft will slightly overshoot VMO/MMO and return to the safe envelope.
- If full forward sidestick is maintained, the aircraft can exceed VMO by ~16 kt or MMO by ~0.04 Mach. At that point, pitch-down authority gradually reduces to zero, preventing further acceleration (though the aircraft does not stabilize at that speed).

These protections aim to recover the aircraft to safe flight without requiring pilot intervention.

How many flight control computers are there on the A320? Name them.

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What are the primary flight control surfaces on the A320?

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What are the secondary flight control surfaces on the A320?

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What are the different flight control laws?

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What is the difference between normal law and alternate law on the A320?

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What happens if all flight control computers fail?

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What protections are available in normal law?

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Describe the load factor protection.

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Describe the high angle-of-attack protection.

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Describe the bank angle protection.

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What is the abnormal attitude law?

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What is Alpha Floor protection?

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How are the flight control surfaces actuated on the A320?

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Describe the direct law.

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What effect does a dual radio altimeter failure have on the flight control laws?

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What are the backup modes of control if the sidesticks are not functional?

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How does the aircraft determine which pilot has control when both sidesticks are moved?

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Fuel

What is the normal fuel usage sequence on the A320, including when ACTs are installed?

When ACTs are installed, fuel is consumed in the following order:

  1. ACT2 (if installed): fuel transfers into the center tank.
  2. ACT1 (if installed): fuel transfers into the center tank.
  3. Center tank: fuel is supplied to the engines via center tank pumps.
  4. Inner wing tanks: each inner tank empties down to 750 kg.
  5. Outer wing tanks: fuel transfers into the inner tanks to maintain the minimum level.

This sequence ensures center of gravity control and fuel management efficiency.

What is the fuel gravity feed ceiling?

Current FL if flight time above FL300 > 30 min, FL300 if flight time above FL300 < 30 min, highest of FL150 and 7000 ft above take-off aerodrome if FL300 never exceeded, FL100 for Jet B.

How many fuel tanks are there on the A320, and how are they configured?

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How is fuel transferred from the center tank to the engines?

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How many fuel pumps are there in total, and how are they distributed across the tanks?

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What happens if both center tank pumps fail in flight?

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What happens if both fuel pumps on one side fail in flight?

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Is crossfeed possible on the A320?

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Can fuel be transferred from one tank to another manually in flight?

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How is refueling controlled on the A320?

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What triggers a 'CTR TK FUEL LO' ECAM warning?

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After a low level is detected in the center tank, how long does it take for the center tank pumps to shut off automatically?

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Hydraulic

Which dual hydraulic failure has the biggest impact on landing distance, and why?

A dual failure of the green and yellow hydraulic systems has the greatest impact on landing distance. This results in the loss of normal and alternate braking, leaving only accumulator braking available. In this case, anti-skid may also be unavailable, and only one thrust reverser remains operational. These limitations significantly increase the required landing distance.

In case of a green system failure, how are the landing gear and brakes affected, and which alternate systems take over?

With a green system failure, landing gear extension must be performed via gravity extension, and normal braking is lost. Alternate braking via the yellow system remains available. Anti-skid protection is still available provided yellow hydraulic pressure is present.

How many hydraulic circuits are there on the A320?

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What is the normal operating pressure of each hydraulic circuit?

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How many pumps are there in the yellow hydraulic system, and what types are they?

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Describe how the three hydraulic circuits power the flight control surfaces. What protection remains in case of a dual hydraulic failure?

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While taxiing with only one engine running, the PTU fails. How could nosewheel steering or braking be affected?

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Under what conditions does the RAT automatically deploy, and what hydraulic power is available once it is active?

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What is the typical pressure delivered by the blue hydraulic circuit when powered by the RAT?

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Is there any backup method to pressurize the blue hydraulic circuit if the blue electric pump fails?

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Can the aircraft be dispatched with one hydraulic system inoperative?

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What condition triggers PTU activation during normal operation?

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What happens hydraulically when both engines are off and ground service is required (e.g., for brake pressure or door operation)?

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If you experience a dual hydraulic failure in flight, how would you manage flight controls, landing gear, and braking?

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PRESS

What are the cabin altitude thresholds for the cabin altitude advisory, CAB PR EXCESS CAB ALT ECAM warning, and cabin oxygen mask deployment?
  • A cabin altitude advisory is triggered when the cabin altitude exceeds approximately 8,800 ft.
  • A cabin altitude warning (ECAM warning: CAB PR EXCESS CAB ALT) is triggered at around 9,550 ft.
  • The passenger oxygen masks automatically deploy when cabin altitude reaches approximately 14,000 ft.
How is cabin pressure regulated on the A320?

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What are the main components of the A320 pressurization system?

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How many outflow valves are installed on the A320?

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How many motors power the outflow valve?

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What is the function of the safety valves in the pressurization system?

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How does the system transition from ground to flight mode?

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What happens if the automatic pressurization system fails?

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How does the manual mode of the pressurization system work?

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What is the maximum cabin altitude allowed before an ECAM warning is triggered?

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What is the maximum cabin altitude at cruise level in normal operations?

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Is it possible to switch the active Cabin Pressure Controller (CPC) in flight?

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What is the purpose of the ram air inlet in abnormal operations?

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When can the ram air valve be opened?

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What is the maximum altitude at which both air conditioning packs can operate when supplied by the APU?

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General

What is the wingspan of the A320 family with different wingtip devices?

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What is the fuselage length of the A319 / A320 / A321?

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What is the maximum operating speed (VMO/MMO) of the A320?

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What is the maximum ground speed allowed due to tire limitations?

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What is the maximum operating speed of the windshield wipers?

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What is the maximum speed with the landing gear extended (VLE)?

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What is the maximum speed for landing gear extension (VLO extension)?

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What is the maximum speed for landing gear retraction (VLO retraction)?

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What is the maximum operating speed of the windshield wipers?

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