ATA 27 A320 NIVEL AVIANCA

What is the primary function of the Trimmable Horizontal Stabilizer (THS)?. Short-term pitch control. Long-term pitch control. Roll control. Yaw control.

Which components achieve roll control on the Airbus A320 family aircraft?. Ailerons and spoilers. Elevators and THS. Rudder and yaw damper. Speed brakes and ground spoilers.

What is the purpose of the speed brake function?. To decrease aircraft drag. To increase aircraft drag. To control engine thrust. thrust To improve fuel efficiency.

How many slats are there on each wing of the Airbus A321?. 2. 5. 4. 7.

What is the function of the Slats and Flaps Control Computers (SFCCs)?. To control and monitor slats and flaps. To control the THS. To control ailerons. To control the rudder.

How are the slat and flap systems powered?. Electrically and hydraulically. Manually. Pneumatically. Mechanically.

What locks the transmission when the slat and flap surfaces reach the selected position?. Power Control Unit (PCU). Torque shafts. Pressure Off Brake (POB). Wing Tip Brakes (WTBs).

What is the purpose of the Alpha/speed lock function in relation to slats?. To prevent slats from extending at high angles of attack or low speeds. To prevent slats from retracting during low speeds. To increase slat extension speed. To improve overall aircraft performance.

How many positions does the FLAPS lever have?. 3. 4. 5. 6.

Which computers are responsible for pitch and roll control on the Airbus A320 family aircraft?. Elevator Aileron Computers (ELAC). Spoiler Elevator Computers (SEC). Flight Augmentation Computers (FAC). Flight Control Data Concentrators (FCDC).

In case of a double ELAC failure, what happens to aileron actuators?. They switch to damping mode. They become inoperative. They disconnect from the aircraft. They lock in their current position.

What is the role of the sidestick in the aircraft's control system?. It controls the rudder. It sends electrical orders to ELACs and SECs. It operates the ailerons. It controls the THS.

The Flight Management Guidance Computer (FMGC) sends roll commands directly to the SECs. True. False.

Spoilers 1 are used for roll control. True. False.

In case of a hydraulic power loss, spoiler surfaces remain extended. True. False.

What is the purpose of the ground spoiler function?. To increase lift during landing. To decrease lift during landing. To increase lift during take-off. To decrease drag during flight.

Which components control the slat and flap systems on the A320 family aircraft?. Slats. Slats. Slat Flap Control Computers (SFCCs). Landing Gear Control and Interface Units (LGCIUs).

How many positions are there for the FLAPS lever on the aircraft?. 2. 3. 4. 5.

A computer failure can engage a lateral ___________ configuration. Abnormal. Normal. Direct. Alternate.

In case of loss of both ELevator Aileron Computers (ELACs) only ___________ are available. Elevators. Ailerons. Spoilers. Rudder.

If the normal law of both ELACs fails, the ___________ law takes over. Normal. Direct. Alternate. Mechanical.

When half speed is detected, a level 1 caution is generated and a fault message is displayed on the ___________. Landing Gear Control. ECAM control panel. EWD. Mechanical trim.

In this example Slat Flap Control Computer (SFCC) 2 flap channel is inoperative and SFCC 1 operates normally. Each flap channel lane of SFCC 1 generates ___________ signals. Pitch. Command. Drive. Hydraulic.

Two flap disconnect sensors are fitted on the interconnecting strut between inner and outer flaps on each wing. The flap disconnect sensors are ___________ sensors. Pressure. Proximity. Hydraulic. Temperature.

In case of total electrical loss, induced roll is obtained by using the ___________, which have a mechanical control. Throttle levers. Rudder pedals. Joysticks. Elevator levers.

In case of loss of both servo controls of the same aileron, the other aileron is still operated. True. False.

If the alternate law is lost, the direct law computed in ELAC 1 or 2 becomes active. The pitch direct law is active in case of ___________. Dual IR failure. Triple IR failure. Failure of the RA. Dual FAC failure.