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system. The main components, controls and indications are described. The cautions and
warnings associated with each system are included in each chapter as is the electric bus
distribution.
In volume 1 the chapter numbers correspond to the ATA (Air Transport Association) 100
BREAKDOWN chapter numbers. This represents the official reference for the classification
of airplane systems and/or functions. The ATA breakdown consists of six digits, the first two
of which refer to a particular aircraft system. The full six digits are used in the MEL and the
MMEL. The list below details the ATA chapter numbers used in FCOM Vol. 1.
A319/A320/A321
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GENERAL
CHAP02\01
AIRBUS DOCUMENTATION (CONT’D)
05 - TRAINEES’ ACTIONS (CONT’D)
Chapter System
21 AIR CONDITIONING, PRESSURIZATION & VENTILATION
22 AUTO FLIGHT
23 COMMUNICATIONS
24 ELECTRICAL
25 EQUIPMENT
26 FIRE PROTECTION
27 FLIGHT CONTROLS
28 FUEL
29 HYDRAULIC
30 ICE AND RAIN PROTECTION
31 INDICATING/ RECORDING SYSTEMS
32 LANDING GEAR
33 LIGHTS
35 OXYGEN
36 PNEUMATIC
38 WATER & WASTE SYSTEM
49 AUXILIARY POWER UNIT
52 DOORS
70 POWER PLANT
The classification of the systems is in alphabetical order apart from the last four systems.
This volume will be of use in the VACBI phase of the course to reinforce and compliment the
lessons learnt on VACBI. However the VACBI should be considered the prime source of
technical information. Once the VACBI phase is successfully completed and upon
completion of training, FCOM Vol. 1 will become the prime source of information on aircraft
systems.
FCOM VOLUME 2
This manual contains information on loading, performance and pre-flight planning. Also
included is performance information for special operations (contaminated runway, ETOPS,
etc.).
This volume is of use during the performance course, and during Line Orientated Flight
Training (LOFT) exercises. It will continue to be of use in line operations. This volume is not
normally used in flight with the exception of certain specific circumstances.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.02.01 Page 6
REV 21 MAY 98
NORMAL OPERATION BRIEFINGS
GENERAL
CHAP02\01
AIRBUS DOCUMENTATION (CONT’D)
05 - TRAINEES’ ACTIONS (CONT’D)
FCOM VOLUME 3
This volume contains chapters on operating limitations, abnormal/emergency procedures,
standard operating procedures (SOPs), supplementary techniques, in-flight performance and
single engine operation.
· Operating Limitations - this chapter includes limitations required by the regulating authority
and contained in the flight manual. You will not be tested on these limitations unless
specified by VACBI or regulatory authorities.
· Abnormal and Emergency Procedures - the contents to this chapter constitute a complete
list of all the ECAM failure messages and other failures requiring the use of the QRH. Each
section in the main body of this chapter corresponds to the relevant ATA chapter number.
In the chapter introduction there is information on ECAM use and task sharing. The section
on operating techniques contains information on such topics as rejected take-off, engine
failure after V1 etc. Within each ECAM procedure there are notes which amplify and clarify
the procedure. These do not appear on ECAM and it is not necessary to consult this
volume during ECAM procedures.
· Normal Procedures - this chapter contains all information on SOPs, and techniques
required for the conduct of a normal flight.
· Supplementary Techniques - this chapter begins with a definition of operating speeds such
as green dot, ’S’ speed etc. The rest of the chapter contains valuable information
concerning systems and operational situations. Most of the sections conform to the ATA
100 breakdown.
· In Flight Performance - contains information on performance for use in flight.
· Single Engine Operations - this chapter details the three strategies possible following an
engine failure in flight. Further information is given to assist in planning and preparing for a
single engine landing.
· OEBs - these are used as the fastest way to advise operators of revised or significant new
technical information, flight crew procedures or changes to limitations. OEBs are not
approved by the airworthiness authorities and will be superseded by a modification or
service bulletin. Some OEBs may have an impact on the safe conduct of flight operations
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