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WARNINGS AND CAUTIONS.......................................................................................................................... 1/10
DSC-27-20-50 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET DSC-27-PLP-TOC P 3/4
FCOM 19 AUG 10
DSC-27-30 FLAPS AND SLATS
DSC-27-30-10 DESCRIPTION
GENERAL............................................................................................................................................................1/8
MAIN COMPONENTS.........................................................................................................................................1/8
ARCHITECTURE.................................................................................................................................................2/8
CONFIGURATIONS............................................................................................................................................ 3/8
AUTOMATIC RETRACTION SYSTEM (ARS)......................................................................................................3/8
FLAP LOAD RELIEF SYSTEM (FLRS)................................................................................................................3/8
RETRACTION/EXTENSION SCHEMATIC........................................................................................................... 5/8
SLATS ALPHA / SPEED LOCK FUNCTION........................................................................................................7/8
SIGNALS TO OTHER SYSTEMS........................................................................................................................ 7/8
DSC-27-30-20 CONTROLS AND INDICATORS
PEDESTAL..........................................................................................................................................................1/6
ECAM UPPER DISPLAY.................................................................................................................................... 3/6
DSC-27-30-30 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/2
DSC-27-30-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A330/A340 FLEET DSC-27-PLP-TOC P 4/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
GENERAL - GENERAL
A330/A340 FLEET DSC-27-10-10 P 1/10
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:
The flight control surfaces are all :
‐ Electrically-controlled, and
‐ Hydraulically-activated.
The stabilizer can be mechanically-controlled.
Pilots use the 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
maneuvers and exceedance of the safe envelope in pitch and roll axis.
However, as on conventional aircraft, the rudder has no such protection.
BASIC PRINCIPLE
Applicable to: ,
The flight control surfaces are all :
‐ Electrically-controlled, and
‐ Hydraulically-activated.
The stabilizer can also be mechanically-controlled.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
GENERAL - GENERAL
A330/A340 FLEET DSC-27-10-10 P 2/10
FCOM 19 AUG 10
Pilots use the 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
maneuvers and exceedance of the safe envelope in pitch and roll axis.
However, as on conventional aircraft, the rudder has no such protection.
　
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