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AIRCRAFT SYSTEMS
OXYGEN
PORTABLE OXYGEN SYSTEM - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-35-40-10 P 4/6
FCOM 19 AUG 10
USING THE HOOD
Applicable to:
,
,
MSN,,,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
OXYGEN
PORTABLE OXYGEN SYSTEM - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-35-40-10 P 5/6
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
OXYGEN
PORTABLE OXYGEN SYSTEM - DESCRIPTION
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A318/A319/A320/A321 FLEET DSC-35-40-10 P 6/6
FCOM 19 AUG 10
AIRCRAFT SYSTEMS
PNEUMATIC
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 FLEET DSC-36-PLP-TOC P 1/2
FCOM 19 AUG 10
DSC-36-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
DSC-36-10 DESCRIPTION
DSC-36-10-10 GENERAL
GENERAL............................................................................................................................................................1/2
DSC-36-10-20 ENGINE BLEED SYSTEM
GENERAL..........................................................................................................................................................1/10
ARCHITECTURE...............................................................................................................................................2/10
AIR BLEED SELECTION..................................................................................................................................6/10
PRESSURE REGULATION AND LIMITATION..................................................................................................9/10
TEMPERATURE REGULATION AND LIMITATION...........................................................................................9/10
DSC-36-10-30 APU BLEED AIR SUPPLY
GENERAL............................................................................................................................................................1/2
APU BLEED VALVE OPENING LOGIC...............................................................................................................2/2
DSC-36-10-40 CROSSBLEED
GENERAL............................................................................................................................................................1/4
X-BLEED VALVE CONTROL LOGIC................................................................................................................... 1/4
ECAM INDICATION............................................................................................................................................ 2/4
DSC-36-10-50 LEAK DETECTION
LEAK DETECTION............................................................................................................................................. 1/2
DSC-36-10-60 OPERATION FOLLOWING FAILURES
BMC FAILURE.................................................................................................................................................... 1/2
DSC-36-20 CONTROLS AND INDICATORS
OVERHEAD PANEL........................................................................................................................................... 1/8
ECAM BLEED PAGE..........................................................................................................................................2/8
DSC-36-30 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/4
DSC-36-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-36-PLP-TOC P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
DESCRIPTION - GENERAL
A318/A319/A320/A321 FLEET DSC-36-10-10 P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The pneumatic system supplies high-pressure air for :
‐ air conditioning
‐ engine starting
‐ wing anti-icing
‐ water pressurization
‐ hydraulic reservoir pressurization
High-pressure air has three sources :
‐ engine bleed systems
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 4(62)
