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Extra resources for Airbus A319, A320, A321 Flight deck and systems briefing for pilots
Control inputs are made to alter the flight path, not to hold it. 11 A319/A320/A321 normal law – pitch axis z Adaptation of basic control law objectives to : - Ground phase : ground mode Direct relationship between stick and elevator available before lift-off and after touch-down - Take-off phase : take-off mode For smooth transition, blend of ground phase law and Nz command law over 5 seconds after lift off. - Landing phase : landing mode At 50ft the attitude is memorized as reference pitch attitude.
In addition - two SFCCs (Slats Flaps Control Computer) - two FCDCs (Flight Control Data Concentrator) acquire data from ELACs and SECs and send them to ECAM and CFDS. 7 Classic and Fly-by-Wire (FBW) controls compared Classic flight controls Fly-by-wire controls z Directly proportional relationship between pilot stick input and control surface position. z No directly proportional relationship between pilot stick input and control surface position. z Aircraft response depending on aircraft dynamics and flight envelope area coverage.
The EMER GEN supplies the AC ESS BUS and the DC ESS BUS via the ESS TR. The ECAM WD remains powered, with associated procedures presented. Alternate law is operative through ELAC 1 and SEC 1. 9 4. 2 A319/A320/A321 hydraulic system - general z Three fully independent systems : Green, Yellow, Blue. z Normal operation : - two engine-driven pumps (one each - Green and Yellow systems) - one electric pump (Blue system) z On ground : - Blue and Yellow systems may be pressurized by electric pumps. A handpump (operated from the ground on the yellow system) facilitates manoeuvring of the cargo doors.