TEST A320 SERIES

Which hydraulic system(s) supply pressure to the landing gear system?. Green. Blue. Yellow and Blue. Green and blue.

The braking modes are: Green or Yellow with anti-skid, Yellow without anti-skid, parking brake. Green with or without anti-skid, Blue without anti-skid. Green with anti-skid, Yellow without anti-skid, Parking brake.

If the brake system automatically transitions to alternate brakes with the A/SKID & N/W STRG switch in the ON position, which of the following will be available?. Anti-skid. Brakes, auto brakes, anti-skid. Only auto brakes. Auto brakes and anti-skid.

What is indicated by the autobrake DECEL lights?. Airplane deceleration is 80% of selected rate. Airplane deceleration is 100% of selected rate. Airplane deceleration is 50% of selected rate. Airplane deceleration is 25% of selected rate.

On the E/WD, you notice the NW STRG DISC memo. What does it mean?. The nose wheel steering has been disconnected by ground personnel. A failure in the nose wheel steering system has been detected. There is a discrepancy between the two nose wheel steering handwheel positions. The nose wheel sterring computer has finished its self test.

During pushback, you start engine #2. You observe the NW STRG DISC memo has changed to amber. Why?. 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. The NW STRG disconnect mechanism has failed.

Landing Gear position is indicated by: One panel on center instrument panel and ECAM. One panel on center instrument panel, ECAM, visual means on the wing. ECAM only. One panel on center instrument panel, one panel on overhead panel.

If the landing gear was gravity extended using the hand crank on the center pedestal, landing gear position must be verified through: The landing gear indications depicted on the ECAM and, if available, the center panel LDG GEAR indicator panel lights. Both are correct. The landing gear viewers.

Landing gear operation is inhibited at speeds: Above 260 knots +/- 5 knots. Below 100 knots. below 100 knots and above 260 knots. Above 250 knots.

Can the gear be extended above 260 kts if necessary?. Yes, but only manually. Never. Yes, but the ultimate limit is 285 kt CAS.

How can the brake accumulator be re-pressurized?. With the yellow electric hydraulic pump. With the blue electric hydraulic pump. Both are correct.

You are ready to taxi. You apply the toe brakes on the rudder pedals and release the PARK BRK. The BRAKES pressure falls to zero. What should you do?. Nothing as this is normal. The BRAKES pressure indicator only indicates alternate (yellow) brake pressure. This should not happen and you must assume that the BRAKES pressure indicator has failed. You must re-apply the PARK BRK and call for maintenance personnel as the main system pressure has failed. The indication is normal because once the AUTO BRK is set to MAX the BRAKES indicator is by-passed.

Which hydraulic system supplies pressure to the nose wheel steering?. Green. Yellow. Blue. Green and Blue.

The anti deactivates when ground speed is less than ______. 20 kts. 10 kts. 25 kts. 30 kts.

If the BSCU detects a brake system malfunction in flight with the A/SKID & N/W STRG switch in the ON position: 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. All of the above.

What is required to arm the auto brakes?. Green hydraulic pressure available, anti-skid, no failures in the braking system. Landing gear lever selected down and selection of an autobraking rate. Both are correct.

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, drop gear, shut doors. Open gear doors, unlock gear, drop gear.

How many turns are required on the gravity extension hand crank to extend the landing gear?. 2. 3. 5. 6.

How do you manually extend the landing gear?. Lift the red handle and turn clockwise a 3 turns. Lift the red handle and turn clockwise a minimum of 4 turns. Lift the red handle and turn anticlockwise a minimum of 2 turns. Lift the red handle and turn anticlockwise 4 turns.

If the Landing Gear was gravity extended using the hand crank on the center pedestal, what other systems will be inoperative?. Nose wheel steering only. Nose wheel steering and auto braking. Anti-skid and auto braking. Nose wheel steering and anti-skid.

Auto brake may be armed with the parking brake on. True. False.

Can normal landing gear operation be restored after a gravity extension if green hydraulic pressure is available?. It may be possible if the gravity extension was not caused by a failure of the landing gear mechanism. Restoration is always possible. No, only maintenance can restore normal operation.

When the landing gear is gravity extended, will nose wheel steering be available?. No. Limited nose wheel steering is available only through the captain's rudder pedals. Only if the A/SKID & N/W STRG switch is selected ON.

Auto brakes, if selected, will only be activated by: The ground spoiler extension command. The brake pedals being depressed. The struts being compressed. The wheels spinning up.

There are two triangles for each gear on the ECAM WHEEL page. What do they represent?. Each triangle represents the position detected by one of the two computers systems. 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 one of the braking systems available for that gear. Each triangle represents one wheel on the gear.

What system pressure does the ACCU PRESS and BRAKES pressure indicator indicate?. 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. Blue brake accumulator and green brake system pressure to the left and right brakes.

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

Wheel page of ECAM: if you see a green arc shown over a wheel indication: It marks the hottest brake with a temperature of more than 100°C. It indicates an abnormal high temperature. The A/SKID system is automatically releasing the pressure of that brake. The L/G control system has detected a low tire profile.

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

With the A/SKID & N/W STRG switch in the ON position, if the BSCU detects a brake system malfunction and/or normal braking is not available: Transition to the alternate brake system is automatic. The crew will be notified with an ECAM message only if after touchdown the brake system does actually malfunction.

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. No. It is not possible to press hard enough to obtain an accurate reading. Yes. As soon as you press the brake pedals the BRAKES indicator will read main system pressure.

If the accumulator on the alternate brake system is your only source pressure, which of the following will be available?. Seven applications of the brake pedals. Three applications of the brake pedals. Antiskid. Auto brakes and antiskid.

The gear doors remain open after a manual extension. True. False.

The steering handwheels, which are interconnected, can steer the nose wheel up to _____ in either direction. 75°. 55°. 65°. 90°.