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DSC-70-80-20 ARCHITECTURE
ARCHITECTURE.................................................................................................................................................1/2
DSC-70-80-30 IGNITION SYSTEM
GENERAL............................................................................................................................................................1/4
IGNITION FOR STARTING................................................................................................................................ 2/4
CONTINUOUS IGNITION................................................................................................................................... 3/4
DSC-70-80-40 ENGINE STARTING SYSTEM
GENERAL..........................................................................................................................................................1/20
AUTOMATIC STARTING.................................................................................................................................. 1/20
AUTOMATIC STARTING SEQUENCE...............................................................................................................3/20
MANUAL STARTING...................................................................................................................................... 11/20
ENGINE VENTILATION (DRY CRANKING).....................................................................................................12/20
MANUAL STARTING SEQUENCE...................................................................................................................13/20
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 FLEET DSC-70-PLP-TOC P 4/4
FCOM 19 AUG 10
DSC-70-90 CONTROLS AND INDICATORS (CFM)
PEDESTAL........................................................................................................................................................1/24
OVERHEAD PANEL......................................................................................................................................... 4/24
MAINTENANCE PANEL................................................................................................................................... 5/24
ECAM................................................................................................................................................................ 5/24
WARNINGS AND CAUTIONS .........................................................................................................................17/24
DSC-70-95 CONTROLS AND INDICATORS (IAE)
PEDESTAL .......................................................................................................................................................1/28
OVERHEAD PANEL......................................................................................................................................... 3/28
MAINTENANCE PANEL................................................................................................................................... 5/28
ECAM................................................................................................................................................................ 5/28
WARNINGS AND CAUTIONS .........................................................................................................................21/28
DSC-70-98 ELECTRICAL SUPPLY
ELECTRICAL SUPPLY.......................................................................................................................................1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
ENGINE
A318/A319/A320/A321 FLEET DSC-70-10 P 1/4
FCOM 19 AUG 10
GENERAL
Applicable to:
, ,
MSN
The CFM 56-5B engine is a high bypass ratio turbofan.
GENERAL
Applicable to: MSN
4566,,,
The V2500-A5 engine is a high bypass ratio turbofan.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
ENGINE
A318/A319/A320/A321 FLEET DSC-70-10 P 2/4
FCOM 19 AUG 10
DESCRIPTION
Applicable to:
, ,
MSN
LOW-PRESSURE (LP) COMPRESSOR/TURBINE
The low-speed rotor (N1) consists of a front fan (single-stage) and a four-stage LP compressor
connected to a four-stage LP turbine.
HIGH-PRESSURE (HP) COMPRESSOR/TURBINE
The high-speed rotor (N2) consists of a nine-stage HP compressor connected to a single-stage HP
turbine.
COMBUSTION CHAMBER
The annular combustion chamber is fitted with 20 fuel nozzles and 2 igniters.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
　
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