Explore the hydraulic and landing gear systems of the A320 in this focused quiz. Assess key skills in system operations, troubleshooting, and safety protocols, essential for maintenance and engineering professionals.
A significant pressure loss occurs in any of the tree hydraulics systems.
A significant pressure loss occurs in the green or yellow hydraulic system.
Both A and B are correct.
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The PTU will be inhibited.
The crew must select the PTU ON .
The PTU fault light will remain illuminated as long as the problem exists. The PTU should be selected OFF.
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Numerous times during each flight.
During the first engine start.
During the second engine start.
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During the first engine start.
When the first engine MASTER switch is moved to the ON position.
Only when the RAT is deployed.
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Automatically with the failure of both the green and blue hydraulic systems.
Automatically with the failure of both the green and yellow hydraulic systems.
Only when the guard RAT MAN ON push button is selected by the crew.
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When the first engine MASTER switch is moved to the ON position.
If any N2 RPM is less than 45 %.
When the yellow electric system ELEC PUMP push button is selected to ON or the ground crew activates a cargo door switch.
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An engine driven pump , an electric pump , the PTU using the green system and , for the cargo doors only , a hand pump.
An engine driven pump , electric pump , the PTU using the blue system and , for the cargo doors only , a hand pump.
An engine driven pump , an electric pump , and the PTU using the green system.
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Only the blue system.
The blue and green system.
The blue and yellow system.
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Yes , select the ECAM ELEC page
NO
Yes , select the ECAM HYD page .
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5 only.
1, 3 , 4.
1 , 2, 3 , 4 .
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Extends RAT , pressurizes BLUE system , starts Emergency Generator .
Extends RAT , pressurizes BLUE system , does not start Emergency Generator .
Extends RAT . Must push RAT MAN ON again to pressurize BLUE system .
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Speed Brakes .
Nosewheel steering , Autobrakes.
Alternate Brakes.
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Low power above 18,000 feet.
High power while airborne .
Shifts from low to high as window temperature requires.
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If the PROBE / WINDOW HEAT push button is selected ON by the prior to engine start.
Automatically after the first engine start.
Both A and B are correct .
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The engine nacelles and three outboard wing slats.
The engine nacelles three outboard wing slats and the horizontal stabilizer.
The engine nacelles three outboard slats , horizontal stabilizer and vertical stabilizer .
Warm bleed air blowing across the windshield.
Rain repellent and windshield wipers.
Both A and B.
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Fail in their current position.
Fail to the open position.
Fail to close position.
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Fail in their current position.
Fail to the open position.
Fail to the close position.
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No.
Yes, valves only open for 30 seconds.
Yes , valves stay open till selected off .
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Both indicate valve in transit , or valve position disagrees with selected position .Wing light also could indicate low pressure .
Both indicate low pressure or valve position disagrees with selected position, Wing light might indicate valve in transit .
Both indicate valve in transit or low pressure .Wing light also could indicate valve position disagree with selected position.
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Landing gear indications depicted on the ECAM and if available , the center panel LDG GEAR indicator panel light .
The landing gear viewers.
Option 4
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Green
Blue
Yellow and Blue .
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Below 100 knots.
Above 260
Below 100 knots and above 260 Knots.
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3
5
2
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No.
Only if the A/SKID AND N/W STRG switch is selected ON.
Limited nose wheel steering is available only through the captain's rudder pedals.
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Restoration is always possible .
It may be possible if the gravity extension was not caused by a failure of the landing gear mechanism.
No , only maintenance can restore normal operation.
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Nose wheel steering .
Anti skid and auto braking .
Nose wheel steering and anti skid .
Option 4
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Green
Blue
Yellow
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Auto brakes and Anti skid.
Only Auto brakes.
Anti skid.
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Auto brakes and Anti skid .
Anti skid .
Seven applications of the brake pedals .
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Airplane deceleration is 50 % of selected rate .
Airplane deceleration is 100% of selected rate .
Airplane deceleration 80% of selected rate .
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Yellow brake accumulator and yellow brake system pressure to the left and right brakes.
Yellow brake accumulator and green brake system pressure to the left and right brakes.
Yellow brake accumulator and green or yellow brake system pressure to the left and right brakes.
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Open gear doors , drop gear shut doors.
Open gear doors , unlock gear ,drop gear.
Shutoff hydraulic pressure ,open doors , unlock gear.
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Green , Blue.
Yellow , Green.
Green , Yellow
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Green hydraulic pressure available , anti skid , no failures in the braking system.
Landing gear lever selected down and selection of an auto breaking rate.
Both A and B are required.
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The struts being compressed.
The brake pedals being depressed.
The ground spoiler extension command.
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The crew will be notified with an ECAM message .
The crew will be notified with an ECAM message after touchdown if the brake system does malfunction.
The crew must manually select alternate brakes.
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Bake system pressure.
Brake accumulator pressure .
Neither A or B .
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With the Yellow electrical pump.
Whit the blue electrical pump.
A and B.
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Quiz Review Timeline (Updated): Apr 21, 2023 +
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