ATA 22 A320 ESCALAFON 2026

1.What is the name purpose of the Automatic Flight System (AFS)?. A. Increase aircraft speed. B. Reduce pilot workload and enhance safety. C. Minimize fuel consumption. D. Control in-flight entertainment.

2. Which display primarily shows guidance commands and flight mode status?. A. ND. B. FCU. C. PFDs. D. MCDUs.

3. What is the purpose of the ECAM/EWD page?. A. Display flight plan information. B. Show passenger announcements. C. Present warning messages and computer failures. D. Control engine thrust.

4. What function is responsible for calculating optimized speed for guidance purposes?. A. FCU. B. FIDS. C. FAC. D. FMGC.

5. What components is the AFS designed around ?. A. FMGC and FCU. B. MCDUs and FACs. C. Wings and engines. D. Radar and altimeter.

6. What role do the MCDUs play in aircraft control?. A. Short-term control of the aircraft. B. Long-term interface between crew and FMGCs. C. Engine management. D. Landing gear control.

7. Which part of AFS serves as the interface for transmitting engine data to FADEC?. A. FCU. B. MCDUs. C. FMGCs. D. FACs.

8. What are the primary functions of the Flight Augmentation Computer (FAC)?. A. Rudder control and flight envelope protection. B. Engine maintenance. C. Passenger comfort control. D. Airspeed management.

9. Which system centralizes failure information for maintenance purposes?. A. FMGC. B. FIDS. C. FCU. D. FMGS.

10. What is the main function of the Fault Isolation and Detection System (FIDS) in the Flight Augmentation Computer (FAC) 1?. A. To engage the Auto Flight System (AFS). B. To control rudder during landing. C. To detect lateral mode failures. D. To concentrate maintenance information.

11. What is the type of communication the Auto Flight System (AFS) maintains with the Centralized Fault Display Interface Unit (CFDU)?. A. One-way communication. B. Two-way communication. C. One-way communication with sensors. D. Two-way communication with FACs.

12. The Auto Flight System (AFS) maintains a ______ communication with the Centralized Fault Display Interface Unit (CFDIU). A. One-way. B. Two-way. C. Direct. Complex.

13. The Autothrust (A/THR) function is engaged automatically when the aircraft's ______ is detected, inhibiting it below 100 feet RA, except during 15 seconds after lift-off. A. Speed decreases. B. Altitude increases. C. Alpha-floor is detected. D. AP is engaged.

14. In cruise, which controls execute the orders of lateral modes, while the elevators and THS execute the orders of vertical modes? The ______. A. Ailerons and rudder. B. Rudder and nose wheel. C. Ailerons and Spoilers. D. Elevators and THS.

15. the engagement status of Flight Director (FD) is displayed on the ______ on the Flight Control Unit (FCU). A. FCU P/BSW. B. AP P/BSW. C. FAC P/BSW. D. A/THR P/BSW.

16. The Auto Flight System (AFS) can engage AP in flight if the aircraft has been airborne for at least ______ seconds. A. 2. B. 5. C. 10. D. 15.

17. When the AP is engaged, the load thresholds on the rudder pedals and the ______ are increased, and if overridden, the AP disengages. A. Side sticks. B. Throttles. C. Spoilers. D. Ailerons.

18. The Flight Director (FD) automatically engages when the system is electrically supplied and logic conditions are met, and the engagement is indicated by the FD P/BSW ______ . A. Blinking. B. Red bars. C. Green bars. D. White bars.

19. The Autothrust (A/THR) function sends computed thrust commands to the Fully Authority Digital Engine Control (FADEC) for ______ engine control. A. Manual. B. Automatic. C. Remote. D. Partial.

20. During take-off, the AP can be engaged in flight after the aircraft has been airborne for at least ______ seconds. A. 2. B. 5. C. 10. D. 15.

21. the primary goal of the Automatic Flight System (AFS) is to enhance flight safety by reducing pilot workload and providing functions that improve ______. A. Flight entertaiment. B. Fuel efficiency. C. Flight consistency. D. Passenger comfort.

22. The AFS is designed around various components, including 2 Flight Management and Guidance Computers (FMGCs), 2 Flight Augmentation Computers (FACs), 2 Multipurpose Control and Display Units (MCDUs), and ______. A. 1 Radar Control Unit (RCU). B. 1 Navigation Control Unit (NCU). C. 1 Flight Control Unit (FCU). D. 1 Avionics Control Unit (ACU).

23. The FCU and MCDUs play a crucial role in allowing pilots to control the functions of the ______. A. Aircraft Fuel Management System (AFMS). B. Flight Data Monitoring System (FDMS). C. Flight Management and Guidance Computers (FMGCs). D. Flight Analisys and Reporting System (FARS).

24. One of the primary functions of the Flight Augmentation Computers (FACs) is to control ______. A. Cabin lighting. B. Engine thrust. C . Wings flaps. D. Rudder and flight envelope protection.

25. the Fault Isolation and Detection System (FIDS) is active only in ______ . A. FAC 1. B. FAC 2. C. FMGC1. D. FMGC2.

26. The yaw damper, operated by yaw damper actuators, performs several functions, includind dutch roll damping, turn coordination in cruise, and compensation for______. A. Cabin pressure fluctuations. B. Loss of radio communications. C. Engine failure during auto flight. D. Turbulence.

27. Rudder trim orders can originate from the Rudder Trim Selector or the ______ to control de rudder. A. Air Data/Inertial Reference System (ADIRS). B. Navigation Control Unit (NCU). C. Flight Management and Guidance Computer (FMGC). D. Aircraft Fuel Management System (AFMS).

28. Which of the following is a fundamental component of the AFS?. A. Autopilot. B. SFCC. C. Ailerons. D. Multipurpose Control and Display Unit (MCDU).

29. What is the primary function of the MCDUs?. A. Short-term aircraft control. B. Engine control. C. Ground navigation control. D. Long-term interface between the crew and FMGCs.

30. What is the main purpose of the Automatic Flight System (AFS). A. Increase aircraft speed. B. Reduce pilot workload and enhance safety. C. Minimize fuel consumption. D. Control in-flight entertainment.