Airbus A320 – Landing Gear - SmartCockpit - Airline training guides, Aviation, Operations, Safety

On wheel page of ECAM, Autobrake is flashing green. What does it mean?

Autobrake is disengaged.

Anti-skid failure.

Autobrake in operation.

Autobrake failure.

Correct! Wrong!

System page WHEEL - L/G position indicators (triangles), first line shows green triangles, second line behind shows amber crosses. Is the landing gear down?

No.

Left hand gear only is down.

Right hand gear only is down.

Yes.

Correct! Wrong!

The Hot light on the brake fan pushbutton illuminates when brake temperature reaches:

300 deg C.

350 deg C.

400 deg C.

250 deg C.

Correct! Wrong!

Each main wheel has an antiskid brake.

True.

False.

Correct! Wrong!

WHEEL SD PAGE - The landing gear positions are indicated by 2 triangles for each gear. Only one green triangle on each landing gear strut is sufficient to confirm that the landing gear is downlocked.

False.

True.

Correct! Wrong!

The normal brake system uses _ hydraulic pressure and the alternate brake system uses _ hydraulic pressure backed up by the hydraulic brake accumulator.

Green - Yellow.

Green - Blue

Yellow - Blue

Yellow - Green

Correct! Wrong!

WHEEL SD PAGE - The landing gear positions are indicated by 2 triangles for each gear. A red triangle indicates that:

One LGCIU (Landing Gear Control and Interface Unit) detects a landing gear in transit.

LGCIU 1 (Landing Gear Control and Interface Unit) or LGCIU 2 has failed.

One LGCIU (Landing Gear Control and Interface Unit) detects a landing gear uplocked.

Correct! Wrong!

Can normal landing gear operation be restored after a gravity extension if green hydraulic pressure is available?

No, only maintenance can restore normal operation.

Restoration is always possible.

It may be possible if the gravity extension was not caused by a failure of the landing gear mechanism.

Correct! Wrong!

Landing gear indicator panel UNLK light illuminates red if:

Gear is not selected down by 1,000 ft RA.

Gear is not locked in selected position.

Gear is extended by gravity and doors are not closed.

Gear is extended normally and doors are not closed.

Correct! Wrong!

Nose wheel steering by rudder pedals is limited to:

Maximum plus or minus 6 degrees depending on aircraft speed.

Plus or minus 75 degrees.

Plus or minus 90 degrees.

Plus or minus 6 degrees under all conditions.

Correct! Wrong!

During the approach you get master warning and ECAM "GEAR NOT DOWN". What is the true statement?

Landing gear is not down locked, flaps at 3 and radio height lower than 750 ft

All statements are correct.

Landing gear is not down locked and flaps 3 or full and both radio altimeters failed

Correct! Wrong!

Auto brake may be armed with the parking brake on.

True.

False.

Correct! Wrong!

If a tire damage is suspected, an inspection of the tires is required before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed. If two tires are deflated on the same main gear (the other main gear tires not being deflated), speed should be limited to _____ and the nose wheel steering angle limited to 30 degrees.

2 kt.

3 kt.

5 kt.

6 kt.

Correct! Wrong!

The steering system centers the nose wheel automatically:

When the landing gear lever is set to UP.

When the hydraulic pressure is released after takeoff.

After liftoff.

Correct! Wrong!

Nose wheels and main wheels have fusible plugs that prevent the tires from bursting if they overheat.

False.

True.

Correct! Wrong!

Only main wheels have fusible plugs.

Nose wheel steering is available when:

The Push button on either steering hand wheel is depressed.

All gear doors are closed.

Gear doors are open.

Nose gear doors are closed.

Correct! Wrong!

Autobraking is initiated by:

Main gear oleo compression.

Ground spoilers extension.

Nose gear oleo compression.

Reverse thrust selection.

Correct! Wrong!

The red arrow, near the landing gear lever illuminates when:

Landing gear is not down locked in approach configuration.

Landing gear is not up locked after retraction.

Landing gear is in transit.

Landing gear is in abnormal position.

Correct! Wrong!

Automatic braking is activated when the command for ground spoilers extension is detected for LO and MED mode, or the command for ground spoilers extension is detected, and the aircraft speed is _____, for MAX mode.

Above 50 kt.

Above 55 kt.

Above 40 kt.

Above 30 kt.

Correct! Wrong!

What system pressure does the ACCU PRESS and BRAKES pressure indicator indicate?

Yellow brake accumulator and green or yellow brake system pressure to the left and right brakes.

Yellow brake accumulator and yellow brake system pressure to the left and right brakes.

Blue brake accumulator and green brake system pressure to the left and right brakes.

Yellow brake accumulator and green brake system pressure to the left and right brakes.

Correct! Wrong!

Maximum speed for landing gear retraction is:

235 kt.

250 kt.

200 kt.

220 kt.

Correct! Wrong!

The antiskid deactivates when ground speed is less than _____.

30 kt.

20 kt.

10 kt.

25 kt.

Correct! Wrong!

The antiskid system gets its reference speed from:

The LGCIU’s.

A wheel tachometer.

The ADIRS.

The BSCU’s.

Correct! Wrong!

The parking brake accumulator is designed to maintain the parking pressure for at least _____.

12 hours.

6 hours.

24 hours.

18 hours.

Correct! Wrong!

During pushback, the engine 2 has been started and the NW STRG DISC memo has changed to amber. What does it mean?

The NW STRG disconnect mechanism has failed.

The memo has become amber because one engine is running.

The nose wheel steering is being reconnected by ground personnel. It is amber because the pin is removed.

The yellow hydraulic system is now pressurized and the amber caption is a warning not to move the handwheel.

Correct! Wrong!

If a tire damage is suspected, an inspection of the tires is required before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with one tire is deflated on one or more gears, then the speed should be limited to _____.

7 kt and 3 kt when turning.

3 kt.

7 kt.

7 kt when turning.

Correct! Wrong!

The steering handwheels, which are interconnected, can steer the nose wheel up to _____ in either direction.

65 degrees.

55 degrees.

90 degrees.

75 degrees.

Correct! Wrong!

There are two triangles for each gear on the ECAM WHEEL page. What do they represent?

Each triangle represents one of the braking systems available for that gear.

The front triangle indicates the position of that gear, and the back triangle indicates the status of the brakes for that gear.

Each triangle represents the position detected by one of the two computers systems.

Each triangle represents one wheel on the gear.

Correct! Wrong!

What is required to arm the auto brakes?

Green hydraulic pressure available, antiskid available, at least one ADIRU in NAV mode.

Green hydraulic pressure available, anti-skid electrically powered, no failures in the braking system, one ADIRU available.

At least one ADIRU in NAV mode and no failures in the braking system.

Yellow hydraulic pressure above 2500 psi, at least one ADIRU in NAV mode and no failures in the braking system.

Correct! Wrong!

For autobrake to activate, at least two SEC’s (Spoiler Elevator Computers) must be operative.

False.

True.

Correct! Wrong!

Max braking has been selected. Takeoff being aborted, engines in reverse, you have forgotten to arm the ground spoilers. Is autobrake activated?

No because spoilers will not deploy if not armed.

Yes, provided speed is less than 72 knots.

Yes, but only if Yellow hydraulic pressure is available.

Yes, because spoilers will still deploy.

Correct! Wrong!

If the aircraft makes an acceleration stop and begins to decelerate when its speed is under _____, the automatic braking will not activate because the ground spoilers will not extend.

92 kt.

82kt.

78 kt.

72 kt.

Correct! Wrong!

On the E/WD, during pushback the NW STRG DISC memo is displayed. What does it mean?

There is a discrepancy between the two nose wheel steering handwheel position transducers.

The nose wheel steering has been disconnected by ground personnel.

The nose wheel steering computer has finished its self test.

A failure in the nose wheel steering system has been detected.

Correct! Wrong!

The autobrake will arm if at least one ADIRU is functioning.

False.

True.

Correct! Wrong!

If the landing gear was gravity extended using the hand crank on the center pedestal, landing gear position must be verified through:

All statements are correct.

The landing gear viewers.

The landing gear indications depicted on the ECAM and, if available, the center panel LDG GEAR indicator panel lights.

Correct! Wrong!

For towing and pushback, the nosewheel steering angle is limited to _____.

75 degrees.

85 degrees.

95 degrees.

90 degrees.

Correct! Wrong!

Hand wheel and pedals are operated simultaneously:

Hand wheel has priority.

Pedals have priority (depending on speed).

BSCU transforms these orders into nose wheel steering angle (signals are mathematically added).

Hand wheel input will not be affected by pedals.

Correct! Wrong!

In normal operation, the reference speed is determined by the BSCU from the horizontal acceleration of ADIRU 1, or ADIRU 2, or ADIRU 3. In case all ADIRUs fail, reference speed equals the minimum of either main landing gear wheel speeds.

True.

False.

Correct! Wrong!

On the ramp with APU running, parking brake is set on, message on ECAM memo shows PARK BRAKE.

In Yellow.

In White or Yellow.

In Green.

In White.

Correct! Wrong!

Brake pressure is only indicated when the yellow hydraulic system controls the brake pressure. This is when the:

Alternate braking system is activated, or Parking brake is applied.

Parking brake is applied.

Alternate braking system is activated.

Correct! Wrong!

Nose wheel steering is controlled by:

LGCIU 2 (Landing Gear Control Interface Unit).

LGCIU 1 (Landing Gear Control Interface Unit).

BSCU (Braking Steering Control Unit).

LGCIU 1 or 2 (Landing Gear Control Interface Unit).

Correct! Wrong!

Landing Gear position is indicated by:

One panel on center instrument panel, ECAM, visual means on the wing.

One panel on center instrument panel and ECAM.

ECAM only.

One panel on center instrument panel, one panel on overhead panel.

Correct! Wrong!

The gear doors remain open after a manual extension.

True.

False.

Correct! Wrong!

When the aircraft is flying faster than _____, a safety valve automatically cuts off hydraulic supply to the landing gear system.

250 kt

255 kt.

260 kt

265 kt.

Correct! Wrong!

Below 260 kt, the hydraulic supply remains cut off as long as the landing gear lever is up.

The alternate brake system uses:

The Yellow hydraulic system.

The Yellow hydraulic system and the hydraulic accumulator.

The Blue electric pump.

The hydraulic accumulator.

Correct! Wrong!

Wheel page on ECAM - if a Green arc becomes amber, and an ECAM caution appears, it means that the corresponding brake temperature exceeds:

350 deg.C.

250 deg.C.

300 deg.C.

400 deg.C.

Correct! Wrong!

The green DECEL light on the autobrake pushbutton illuminates when the actual airplane deceleration corresponds to what percentage of the selected rate?

92%.

80%.

90%.

95%.

Correct! Wrong!

When the flight crew operates the crank handle, the cutout valve shuts off hydraulic pressure to the landing gear system and depressurizes it.

False.

True.

Correct! Wrong!

If the parking brake is activated and no yellow hydraulic or accumulator brake pressure is available, then the normal braking system can be applied via the brake pedals.

False.

True.

Correct! Wrong!

Following failure of all 3 ADIRS, is antiskid available?

Only with Yellow hydraulics.

Yes, the speed for the fastest wheel becomes the reference in this case.

Only with Green hydraulics.

No.

Correct! Wrong!

What does each turn of the gravity gear extension handle do?

Shutoff hydraulic pressure, open doors, unlock gear.

Open gear doors, shutoffs hydraulics, unlock gear, drop gear.

Open gear doors, unlock gear, drop gear.

Open gear doors, drop gear, shut doors.

Correct! Wrong!

Which hydraulic system(s) supply pressure to the landing gear system?

Green.

Green and Blue.

Blue.

Yellow and Blue.

Correct! Wrong!

If the brake system automatically transitions to alternate brakes with the A/SKID and N/W STRG switch in the ON position, which of the following will be available?

Anti-skid.

Auto brakes and anti-skid.

Brakes, auto brakes, anti-skid.

Only auto brakes.

Correct! Wrong!

The LGCIUs (Landing Gear Control Interface Units) control the sequencing of gear and doors hydraulically.

True.

False.

Correct! Wrong!

The LGCIUs control the sequencing of gear and doors electrically.

After takeoff the left main landing gear shock absorber is stuck in the compressed position.

The gear can be retracted once the nose wheel steering is centered.

The gear can be retracted provided the nose gear is centered.

The gear can be retracted under all circumstances.

The gear cannot be retracted, gear lever is blocked (interlock mechanism).

Correct! Wrong!

MAX autobrake mode can be armed in flight.

False.

True.

Correct! Wrong!

MAX autobrake mode cannot be armed in flight.

The maximum speed with landing gear extended (VLE) is:

320 kt / M.72

280 kt / M.67

260 kt / M.65

300 kt / M.70

Correct! Wrong!

If the BSCU (Braking Steering Control Unit) detects a brake system malfunction in flight with the A/SKID and N/W STRG switch in the ON position:

The flight crew will be notified with an ECAM message after touchdown if the brake system does malfunction.

The flight crew will be notified with an ECAM message.

All statements are correct.

The flight crew must manually select alternate brakes.

Correct! Wrong!

The braking system is designed to hold the aircraft in a stationary position when a high thrust level is applied on at least one engine. It is not designed to hold the aircraft when high thrust level is applied on both engines. During ground procedures that require a thrust increase with braking, the flight crew must ensure that the aircraft remains stationary.

False.

True.

Correct! Wrong!

The braking system is not designed to hold the aircraft in a stationary position when a high thrust level is applied on at least one engine.

You have just set the parking brake handle to ON. Is it still possible to check the main brake system using the toe brakes?

No. When the PARK BRK is set, the other braking modes are deactivated.

Yes. As soon as you press the brake pedals the BRAKES indicator will read main system pressure.

No. It is not possible to press hard enough to obtain an accurate reading.

Correct! Wrong!

The braking modes are:

Green with anti-skid, Yellow without anti-skid, Parking brake.

Green or Yellow with anti-skid, Yellow without anti-skid, parking brake.

Green with or without anti-skid, Blue without anti-skid.

Correct! Wrong!

What is indicated by the autobrake DECEL lights?

Airplane deceleration is 90% of selected rate.

Airplane deceleration is 25% of selected rate.

Airplane deceleration is 80% of selected rate.

Airplane deceleration is 50% of selected rate.

Correct! Wrong!

Braking modes - There are _____ modes of operation:

Three: Normal braking, Alternate braking with antiskid, Parking brake.

Three: Normal braking, Alternate, Alternate braking and Parking brake.

Four: Normal braking, Alternate braking, Emergency braking, and Parking brake.

Four: Normal braking, Alternate braking with antiskid, Alternate braking without antiskid and Parking brake.

Correct! Wrong!

To put the landing gear down by gravity, the flight crew must pull the gear crank out, then turn it clockwise for _____ turns.

Four.

Six.

Three.

Five.

Correct! Wrong!

A hand crank on the center pedestal allows the flight crew to extend the landing gear if the aircraft loses hydraulic systems or electrical power.

ALTERNATE BRAKING WITHOUT ANTI-SKID - Autobrake and antiskid are inoperative. To avoid wheel locking and limit the risk of tire burst, brake pressure is automatically limited to:

2 000 PSI.

1 600 PSI.

800 PSI.

1 000 PSI.

Correct! Wrong!

The antiskid system provides maximum braking efficiency by maintaining the wheels at the limit of an impending skid. The antiskid system is deactivated _____

At or below 10 kt (ground speed).

At or below 20 kt IAS.

Below 15 kt IAS.

Below 20 kt (ground speed).

Correct! Wrong!

What happens to the other brake modes when parking brakes are applied?

There is no change.

All other braking modes and antiskid are deactivated.

Antiskid mode only is deactivated.

Correct! Wrong!

The brake and accumulator pressure gauge shows pressure from:

The Yellow hydraulic system.

The Green hydraulic system.

The Accumulator only.

Both Yellow brake system and the Brake Accumulator.

Correct! Wrong!

When both hand wheels are operated simultaneously, the signals are algebraically added.

False.

True.

Correct! Wrong!

Wheel page on ECAM - if you see a green arc shown over a wheel indication:

The A/SKID system is automatically releasing the pressure of that brake.

It marks the hottest brake with a temperature of more than 100 deg.C.

It indicates an abnormal high temperature.

The L/G control system has detected a low tire profile.

Correct! Wrong!

What is the maximum tire speed?

225 kt.

205 kt.

195 kt.

185 kt.

Correct! Wrong!

Which ADIRS close the safety valve of the green hydraulic supply when speed is above 260 kt.

ADIRS 1 and 3.

ADIRS 2 or 3.

ADIRS 1 and 2.

ADIRS 2 and 3.

Correct! Wrong!

AUTO/BRK panel - The springloaded MAX, MED, and LO pushbutton switches arm the appropriate deceleration rate. MED mode sends progressive pressure to the brakes _____ after the ground spoilers deploy.

Between two and four seconds.

Two seconds.

Between three and four seconds.

Correct! Wrong!

LO mode sends progressive pressure to the brakes 4 seconds after the ground spoilers deploy.

Auto brakes, if selected, will only be activated by:

The brake pedals being depressed.

The ground spoiler extension command.

The wheels spinning up.

The struts being compressed.

Correct! Wrong!

When is pressure in the nose wheel steering system shut off?

With towing lever in towing position or both engines are shut down or the A/SKID and N/W STRG switch is OFF.

When the aircraft is on the ground with speed above 100 kt.

During ground towing with one engine shut down or when aircraft speed is above 60 kt.

Correct! Wrong!

Landing gear operation is inhibited at speeds:

Above 260 knots plus or minus 5 knots.

Below 100 knots and above 260 knots.

Above 250 knots.

Below 100 knots.

Correct! Wrong!

The landing gear indicator panel receives the information from micro switches and proximity detectors connected to:

LGCIU 2 (Landing Gear Control and Interface Unit).

LGCIU 1 (Landing Gear Control and Interface Unit).

BSCU (Braking Steering Control Unit) and LGCIU 2.

BSCU (Braking Steering Control Unit).

Correct! Wrong!

Two Landing Gear Control and Interface Units (LGCIUs) control the extension and retraction of the gear and the operation of the doors. They also supply information about the landing gear to ECAM for display, and send signals indicating whether the aircraft is in flight or on the ground to other aircraft systems.

False.

True.

Correct! Wrong!

If a tire damage is suspected, an inspection of the tires is required before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with one tire is deflated on one or more gears, ie. a maximum of _____.

Four tires.

Three tires.

Two tires.

Correct! Wrong!

Alternate braking using the Yellow system. Autobrake is:

Still available with anti-skid.

Lost.

Still available without anti-skid.

Still available provided Yellow system hydraulic pressure is available.

Correct! Wrong!

Nose wheel steering is available:

Aircraft speed below 70 kt, both engines (required to be) running, Towing lever in normal position, aircraft on ground or in the air.

Aircraft speed below 70 kt, both engines (required to be) running), Towing lever in standby position, aircraft on ground.

Aircraft speed below 70 kt, one engine (required to be) running, Towing lever in normal position, aircraft on ground.

Aircraft speed below 70 kt, both engines (required to be) running, Towing lever in normal position, aircraft on ground.

Correct! Wrong!

If the accumulator on the alternate brake system is your only source pressure, which of the following will be available?

Antiskid.

Three applications of the brake pedals.

Seven applications of the brake pedals.

Auto brakes and antiskid.

Correct! Wrong!

Airbus A320 – Landing Gear

Airbus A320 – Landing Gear

On wheel page of ECAM, Autobrake is flashing green. What does it mean?

System page WHEEL - L/G position indicators (triangles), first line shows green triangles, second line behind shows amber crosses. Is the landing gear down?

The Hot light on the brake fan pushbutton illuminates when brake temperature reaches:

Each main wheel has an antiskid brake.

WHEEL SD PAGE - The landing gear positions are indicated by 2 triangles for each gear. Only one green triangle on each landing gear strut is sufficient to confirm that the landing gear is downlocked.

The normal brake system uses _____ hydraulic pressure and the alternate brake system uses _____ hydraulic pressure backed up by the hydraulic brake accumulator.

WHEEL SD PAGE - The landing gear positions are indicated by 2 triangles for each gear. A red triangle indicates that:

Can normal landing gear operation be restored after a gravity extension if green hydraulic pressure is available?

Landing gear indicator panel UNLK light illuminates red if:

Nose wheel steering by rudder pedals is limited to:

During the approach you get master warning and ECAM "GEAR NOT DOWN". What is the true statement?

Auto brake may be armed with the parking brake on.

The steering system centers the nose wheel automatically:

Nose wheels and main wheels have fusible plugs that prevent the tires from bursting if they overheat.

Nose wheel steering is available when:

Autobraking is initiated by:

The red arrow, near the landing gear lever illuminates when:

Automatic braking is activated when the command for ground spoilers extension is detected for LO and MED mode, or the command for ground spoilers extension is detected, and the aircraft speed is _____, for MAX mode.

What system pressure does the ACCU PRESS and BRAKES pressure indicator indicate?

Maximum speed for landing gear retraction is:

The antiskid deactivates when ground speed is less than _____.

The antiskid system gets its reference speed from:

The parking brake accumulator is designed to maintain the parking pressure for at least _____.

During pushback, the engine 2 has been started and the NW STRG DISC memo has changed to amber. What does it mean?

If a tire damage is suspected, an inspection of the tires is required before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with one tire is deflated on one or more gears, then the speed should be limited to _____.

The steering handwheels, which are interconnected, can steer the nose wheel up to _____ in either direction.

There are two triangles for each gear on the ECAM WHEEL page. What do they represent?

What is required to arm the auto brakes?

For autobrake to activate, at least two SEC’s (Spoiler Elevator Computers) must be operative.

Max braking has been selected. Takeoff being aborted, engines in reverse, you have forgotten to arm the ground spoilers. Is autobrake activated?

If the aircraft makes an acceleration stop and begins to decelerate when its speed is under _____, the automatic braking will not activate because the ground spoilers will not extend.

On the E/WD, during pushback the NW STRG DISC memo is displayed. What does it mean?

The autobrake will arm if at least one ADIRU is functioning.

If the landing gear was gravity extended using the hand crank on the center pedestal, landing gear position must be verified through:

For towing and pushback, the nosewheel steering angle is limited to _____.

Hand wheel and pedals are operated simultaneously:

In normal operation, the reference speed is determined by the BSCU from the horizontal acceleration of ADIRU 1, or ADIRU 2, or ADIRU 3. In case all ADIRUs fail, reference speed equals the minimum of either main landing gear wheel speeds.

On the ramp with APU running, parking brake is set on, message on ECAM memo shows PARK BRAKE.

Brake pressure is only indicated when the yellow hydraulic system controls the brake pressure. This is when the:

Nose wheel steering is controlled by:

Landing Gear position is indicated by:

The gear doors remain open after a manual extension.

When the aircraft is flying faster than _____, a safety valve automatically cuts off hydraulic supply to the landing gear system.

The alternate brake system uses:

Wheel page on ECAM - if a Green arc becomes amber, and an ECAM caution appears, it means that the corresponding brake temperature exceeds:

The green DECEL light on the autobrake pushbutton illuminates when the actual airplane deceleration corresponds to what percentage of the selected rate?

When the flight crew operates the crank handle, the cutout valve shuts off hydraulic pressure to the landing gear system and depressurizes it.

If the parking brake is activated and no yellow hydraulic or accumulator brake pressure is available, then the normal braking system can be applied via the brake pedals.

Following failure of all 3 ADIRS, is antiskid available?

What does each turn of the gravity gear extension handle do?

Which hydraulic system(s) supply pressure to the landing gear system?

If the brake system automatically transitions to alternate brakes with the A/SKID and N/W STRG switch in the ON position, which of the following will be available?

The LGCIUs (Landing Gear Control Interface Units) control the sequencing of gear and doors hydraulically.

After takeoff the left main landing gear shock absorber is stuck in the compressed position.

MAX autobrake mode can be armed in flight.

The maximum speed with landing gear extended (VLE) is:

If the BSCU (Braking Steering Control Unit) detects a brake system malfunction in flight with the A/SKID and N/W STRG switch in the ON position:

You have just set the parking brake handle to ON. Is it still possible to check the main brake system using the toe brakes?

The braking modes are:

What is indicated by the autobrake DECEL lights?

Braking modes - There are _____ modes of operation:

To put the landing gear down by gravity, the flight crew must pull the gear crank out, then turn it clockwise for _____ turns.

ALTERNATE BRAKING WITHOUT ANTI-SKID - Autobrake and antiskid are inoperative. To avoid wheel locking and limit the risk of tire burst, brake pressure is automatically limited to:

The antiskid system provides maximum braking efficiency by maintaining the wheels at the limit of an impending skid. The antiskid system is deactivated _____

What happens to the other brake modes when parking brakes are applied?

The brake and accumulator pressure gauge shows pressure from:

When both hand wheels are operated simultaneously, the signals are algebraically added.

Wheel page on ECAM - if you see a green arc shown over a wheel indication:

What is the maximum tire speed?

Which ADIRS close the safety valve of the green hydraulic supply when speed is above 260 kt.

AUTO/BRK panel - The springloaded MAX, MED, and LO pushbutton switches arm the appropriate deceleration rate. MED mode sends progressive pressure to the brakes _____ after the ground spoilers deploy.

Auto brakes, if selected, will only be activated by:

When is pressure in the nose wheel steering system shut off?

Landing gear operation is inhibited at speeds:

The landing gear indicator panel receives the information from micro switches and proximity detectors connected to:

If a tire damage is suspected, an inspection of the tires is required before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with one tire is deflated on one or more gears, ie. a maximum of _____.

Alternate braking using the Yellow system. Autobrake is:

Nose wheel steering is available:

If the accumulator on the alternate brake system is your only source pressure, which of the following will be available?

The normal brake system uses _ hydraulic pressure and the alternate brake system uses _ hydraulic pressure backed up by the hydraulic brake accumulator.