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FLIGHT CONTROLS LAW RECONFIGURATION............................................................................................. 2/10
ALTERNATE LAW............................................................................................................................................ 4/10
ALTERNATE LAW WITHOUT REDUCED PROTECTION.................................................................................7/10
DIRECT LAW.................................................................................................................................................... 7/10
ABNORMAL ATTITUDE LAWS.......................................................................................................................... 8/10
MECHANICAL BACK-UP..................................................................................................................................9/10
DSC-27-20-30 CONTROLS AND INDICATORS
PEDESTAL........................................................................................................................................................1/28
LATERAL CONSOLES..................................................................................................................................... 8/28
GLARESHIELD................................................................................................................................................10/28
OVERHEAD PANEL....................................................................................................................................... 13/28
SIDE STICK INDICATIONS ON PFD...............................................................................................................17/28
ECAM F/CTL PAGE........................................................................................................................................18/28
ECAM WHEEL PAGE.....................................................................................................................................26/28
DSC-27-20-40 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/8
DSC-27-20-50 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST .................................................................................................................................... 1/2
DSC-27-30 FLAPS AND SLATS
DSC-27-30-10 DESCRIPTION
GENERAL............................................................................................................................................................1/8
MAIN COMPONENTS.........................................................................................................................................1/8
ARCHITECTURE.................................................................................................................................................4/8
CONFIGURATIONS............................................................................................................................................ 7/8
ALPHA/SPEED LOCK FUNCTION (SLATS)........................................................................................................7/8
DSC-27-30-20 CONTROLS AND INDICATORS
PEDESTAL..........................................................................................................................................................1/8
ECAM UPPER DISPLAY.................................................................................................................................... 4/8
DSC-27-30-30 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/2
DSC-27-30-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST .................................................................................................................................... 1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
GENERAL - GENERAL
A318/A319/A320/A321 FLEET DSC-27-10-10 P 1/4
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The fly-by-wire system was designed and certified to render the new generation of aircraft even more
safe, cost effective, and pleasant to fly.
BASIC PRINCIPLE
Applicable to: ALL
Flight control surfaces are all :
‐ Electrically-controlled, and
‐ Hydraulically-activated.
The stabilizer and rudder can also be mechanically-controlled.
Pilots use sidesticks to fly the aircraft in pitch and roll (and in yaw, indirectly, through turn
coordination).
Computers interpret pilot input and move the flight control surfaces, as necessary, to follow their
orders.
However, when in normal law, regardless of the pilot’s input, the computers will prevent excessive
　
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