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DSC-36-10-60 LEAK DETECTION
LEAK DETECTION............................................................................................................................................. 1/4
DSC-36-10-70 OPERATION FOLLOWING FAILURES
BMC FAILURE.................................................................................................................................................... 1/2
DSC-36-20 CONTROLS AND INDICATORS
OVERHEAD PANEL......................................................................................................................................... 1/10
ECAM BLEED PAGE........................................................................................................................................4/10
DSC-36-30 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/4
DSC-36-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A330/A340 FLEET DSC-36-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
DESCRIPTION - GENERAL
A330/A340 FLEET DSC-36-10-10 P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to:
The pneumatic system supplies high pressure air for :
‐ Air conditioning
‐ Engine starting
‐ Wing anti-icing
‐ Water pressurization
‐ Hydraulic reservoir pressurization
‐ Pack bay ventilation turbofan actuation.
High pressure air is supplied from three sources :
‐ Engine bleed systems
‐ APU load compressor
‐ Two HP ground connections.
Engine bleed systems are interconnected by a crossbleed duct, to which the APU and ground
sources are connected.
A valve, mounted on the crossbleed duct, allows the left side (ENG 1 and ENG 2) and the right side
(ENG 3 and ENG 4) to be interconnected.
Pneumatic system operation is controlled and monitored by four Bleed Monitoring Computers (BMC
1, 2, 3 and 4), the overhead control panel and the ECAM. The APU bleed supply is controlled by the
APU Electronic Control Box (ECB).
A leak detection system is provided to detect any overheat in the vicinity of the hot air ducts.
GENERAL
Applicable to: ,
The pneumatic system supplies high pressure air for :
‐ Air conditioning
‐ Engine starting
‐ Wing anti-icing
‐ Water pressurization
‐ Hydraulic reservoir pressurization
‐ Pack bay ventilation turbofan actuation.
High pressure air is supplied from three sources :
‐ Engine bleed systems
‐ APU load compressor
‐ Two HP ground connections.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
DESCRIPTION - GENERAL
A330/A340 FLEET DSC-36-10-10 P 2/2
FCOM 19 AUG 10
Engine bleed systems are interconnected by a crossbleed duct, to which the APU and ground
sources are connected.
A valve, mounted on the crossbleed duct, allows the left side (ENG 1) and the right side (ENG 2) to
be interconnected.
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 3(150)
