A320 FLIGHT CONTROL LAWS Exam Questions With Accurate Answers Graded A+

A320 FLIGHT CONTROL LAWS Exam
Questions With Accurate Answers
Graded A+

Prevention of excessive maneuver - ANSWER-•In NORMAL Law does only include:

•Pitch

•Roll



*Rudder had NO protection.



FCCs - ANSWER-•Two ELACs

•Tree SECs

•Two FACs



ELAC (2) - ANSWER-ELevator and Aileron Computer

•Normal Elevator

•Stabilizer

•Aileron



SEC (3) - ANSWER-Spoiler and Elevator Computer

•Spoiler

•STANDBY Elivator

•STANDBY Stabilizer



FAC (2) - ANSWER-Flight Augmentation Computer

•Electrical rudder control

, Flight control laws - ANSWER-# Normal Law

# Alternate Law

# Direct Law

# Mechanical back-up

# Abnormal attitude Law



Reconfiguration - ANSWER-•aka degradation of control law.

•Multiple failures of f-cnt, HYD syst, ELEC syst.



Normal Law Modes - ANSWER-•Ground Mode

•Flight Mode

•Flare Mode



NORMAL LAW Ground Mode - ANSWER-• Active until shortly after liftoff.



• Direct proportional relationship between the sidestick deflection and deflection of the
flight controls. (Direct Law)



• After touchdown, ground mode is reactivated and resets the stabilizer trim to zero.



NORMAL LAW Flight Mode - ANSWER-• Active shortly after takeoff until shortly before
touchdown



• Sidestick deflection and load factor imposed on the aircraft are directly proportional,
regardless of airspeed.




Pitch:

• G-Load demand.

• With sidestick neutral and wings level, system maintains a 1G load in pitch.