1
A32F SYSTEMS ACTUAL EXAM BANK WITH 200+
QUESTIONS AND CORRECT SOLUTIONS 2026-27
LATEST VERSION
• If flaps FULL is selected with the speedbrakes extended:
A. The flaps will not extend until the speedbrakes are fully retracted
B. The speedbrakes will automatically retract
C. The flaps will extend and the speedbrakes remain extended.
There will be an ECAM warning message
• The Alpha Lock feature of the Slat and Flap Control Computers (SFCCs)
prevents:
A. The extension of flaps at a speed greater than the maximum flap
extension speed
B. The retraction of the flaps during a high angle of attack/ low speed
situation
C. The retraction of the slats during a high angle of
attack/low speed situation
• Engine anti-ice is applied to what component of the engine?
A. The nacelle leading edges
B. The spinner and nacelle leading edges
C. The fan and nacelle leading edges
• If electrical power supply to the engine anti-ice valve fails, the engine anti-
ice valve:
A. Closes
B. Opens
C. Remains in its current position
• Is probe/window heat available prior to engine start?
A. No
B. Yes. The PROBE/WINDOW HEAT pb on the ANT ICE panel must be
selected to AUTO
C. Yes. The PROBE/WINDOW HEAT pb on the ANT ICE panel must
be selected
to ON
• What is the airspeed limit for operation of the windscreen wipers?
A. 230 knots
B. 250 knots
C. 200 knots
,2
• If electrical power supply to the wing anti-ice valve fails, the wing anti-ice
valve:
A. Closes
B. Opens
C. Remains in its current position
• The wing anti-ice system provides:
A. Anti-icing capability for only the outboard leading edge devices of
each wing
B. Anti-icing capability for all leading edge devices of each wing
C. Anti-icing capability for all leading edge and trailing edge devices of
each wing
• Which hydraulic system does the Landing Gear Control and Interface Unit
(LGCIU) use to extend and retract the landing gear?
A. GREEN
B. YELLOW
C. BLUE
• When does the alternate braking system become operational/active?
A. The failure of the Alternate Brake Control Unit (ABCU)
B. The failure of the autobrakes
C. The failure of the green hydraulic system
• Which hydraulic system does the alternate braking system use
A. GREEN
B. YELLOW
C. BLUE
• The crew performs a landing with autobrakes selected to MED. What
triggers the application of the autobrakes?
A. The application of the brake pedals by the pilot
B. The signal to extend the spoilers
C. Reverse thrust is selected
• Which is NOT a basic mode of GPWS?
A. Excessive rate of descent.
B. Excessive terrain closure rate
C. Altitude loss after takeoff, or go-around.
D. Deviation above the glideslope.
• During a manual start, how is the start valve opened?
A. It is automatic once the ENG MASTER is placed to the ON position.
B. By depressing the ENG MAN START pushbutton on the overhead
panel.
C. By depressing the ENG MAN START pushbutton on the
overhead panel while the ENG MODE selector is out of the NORM
position.
,3
• The message OUTER TK FUEL XFRD appears in the MEMO. What does this
mean?
A. It is a reminder to show that a transfer valve is open
B. Fuel is transferring from the center tank to the inner tank.
C. It is a reminder to open the outer tank transfer valve.
D. Fuel is transferring from the inner tank to the outer tank.
, 4
• On board the Wizz Air A-320 aircraft, there are .. identical ADIRUs
and ... GPS receivers.
A. 2,2
B. 3,2
C. 3,3
D. 3,1
• The APU may be started up to what altitude?
A. The APU can be started at any altitude provided normal aircraft
electrical power is available.
B. The APU can be started up to 35,000 feet using only the aircraft
batteries.
C. The APU can be started up to 30,000 feet using only the aircraft
batteries.
D. Both A and B are correct.
• What does pushing the APPR push button do?
A. Arms the Flight Guidance system to capture a localiser and glide
slope.
B. Arms managed navigation.
C. Allows the aircraft to slow to green dot speed.
D. Arms managed vertical navigation.
• What happens to the cockpit door with electrical power failure?
A. It operates normally on HOT BAT bus.
B. It automatically locks.
C. It automatically unlocks.
D. None of the above.
• If the lower ECAM DU fails, is there a way to retrieve that information?
A. By pressing and holding the related systems page push button
on the ECAM control panel, the page will be displayed on the
UPPER ECAM.
B. By rotating the ECAM/ND XFR switch on the switching panel, the
lower ECAM page will be transferred to either the Captain or FO's ND.
C. Both A and B are WRONG.
D. Both A and B are correct.
• What does illumination of the white SLIDE ARMED light represent on the
main cabin door?
A. This indicates that the slide has properly inflated and is sate for use.
B. This indicates that the slide is armed and the slide will inflate if
the door is opened from inside the aircraft.
C. This indicates that the main cabin door has not been properly closed.
D. This indicates that the main cabin door has not been properly closed
but the slide is properly armed.
• After a single MC failure, how could a crew member recover the display
A32F SYSTEMS ACTUAL EXAM BANK WITH 200+
QUESTIONS AND CORRECT SOLUTIONS 2026-27
LATEST VERSION
• If flaps FULL is selected with the speedbrakes extended:
A. The flaps will not extend until the speedbrakes are fully retracted
B. The speedbrakes will automatically retract
C. The flaps will extend and the speedbrakes remain extended.
There will be an ECAM warning message
• The Alpha Lock feature of the Slat and Flap Control Computers (SFCCs)
prevents:
A. The extension of flaps at a speed greater than the maximum flap
extension speed
B. The retraction of the flaps during a high angle of attack/ low speed
situation
C. The retraction of the slats during a high angle of
attack/low speed situation
• Engine anti-ice is applied to what component of the engine?
A. The nacelle leading edges
B. The spinner and nacelle leading edges
C. The fan and nacelle leading edges
• If electrical power supply to the engine anti-ice valve fails, the engine anti-
ice valve:
A. Closes
B. Opens
C. Remains in its current position
• Is probe/window heat available prior to engine start?
A. No
B. Yes. The PROBE/WINDOW HEAT pb on the ANT ICE panel must be
selected to AUTO
C. Yes. The PROBE/WINDOW HEAT pb on the ANT ICE panel must
be selected
to ON
• What is the airspeed limit for operation of the windscreen wipers?
A. 230 knots
B. 250 knots
C. 200 knots
,2
• If electrical power supply to the wing anti-ice valve fails, the wing anti-ice
valve:
A. Closes
B. Opens
C. Remains in its current position
• The wing anti-ice system provides:
A. Anti-icing capability for only the outboard leading edge devices of
each wing
B. Anti-icing capability for all leading edge devices of each wing
C. Anti-icing capability for all leading edge and trailing edge devices of
each wing
• Which hydraulic system does the Landing Gear Control and Interface Unit
(LGCIU) use to extend and retract the landing gear?
A. GREEN
B. YELLOW
C. BLUE
• When does the alternate braking system become operational/active?
A. The failure of the Alternate Brake Control Unit (ABCU)
B. The failure of the autobrakes
C. The failure of the green hydraulic system
• Which hydraulic system does the alternate braking system use
A. GREEN
B. YELLOW
C. BLUE
• The crew performs a landing with autobrakes selected to MED. What
triggers the application of the autobrakes?
A. The application of the brake pedals by the pilot
B. The signal to extend the spoilers
C. Reverse thrust is selected
• Which is NOT a basic mode of GPWS?
A. Excessive rate of descent.
B. Excessive terrain closure rate
C. Altitude loss after takeoff, or go-around.
D. Deviation above the glideslope.
• During a manual start, how is the start valve opened?
A. It is automatic once the ENG MASTER is placed to the ON position.
B. By depressing the ENG MAN START pushbutton on the overhead
panel.
C. By depressing the ENG MAN START pushbutton on the
overhead panel while the ENG MODE selector is out of the NORM
position.
,3
• The message OUTER TK FUEL XFRD appears in the MEMO. What does this
mean?
A. It is a reminder to show that a transfer valve is open
B. Fuel is transferring from the center tank to the inner tank.
C. It is a reminder to open the outer tank transfer valve.
D. Fuel is transferring from the inner tank to the outer tank.
, 4
• On board the Wizz Air A-320 aircraft, there are .. identical ADIRUs
and ... GPS receivers.
A. 2,2
B. 3,2
C. 3,3
D. 3,1
• The APU may be started up to what altitude?
A. The APU can be started at any altitude provided normal aircraft
electrical power is available.
B. The APU can be started up to 35,000 feet using only the aircraft
batteries.
C. The APU can be started up to 30,000 feet using only the aircraft
batteries.
D. Both A and B are correct.
• What does pushing the APPR push button do?
A. Arms the Flight Guidance system to capture a localiser and glide
slope.
B. Arms managed navigation.
C. Allows the aircraft to slow to green dot speed.
D. Arms managed vertical navigation.
• What happens to the cockpit door with electrical power failure?
A. It operates normally on HOT BAT bus.
B. It automatically locks.
C. It automatically unlocks.
D. None of the above.
• If the lower ECAM DU fails, is there a way to retrieve that information?
A. By pressing and holding the related systems page push button
on the ECAM control panel, the page will be displayed on the
UPPER ECAM.
B. By rotating the ECAM/ND XFR switch on the switching panel, the
lower ECAM page will be transferred to either the Captain or FO's ND.
C. Both A and B are WRONG.
D. Both A and B are correct.
• What does illumination of the white SLIDE ARMED light represent on the
main cabin door?
A. This indicates that the slide has properly inflated and is sate for use.
B. This indicates that the slide is armed and the slide will inflate if
the door is opened from inside the aircraft.
C. This indicates that the main cabin door has not been properly closed.
D. This indicates that the main cabin door has not been properly closed
but the slide is properly armed.
• After a single MC failure, how could a crew member recover the display
