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BLUE HYDRAULIC LOW LEVEL
Start the APU to ensure availability of the APU generator.
ENGINE OR IDG FAILURE
Start the APU and use the APU electrical channel.
ABN AND EMER PROCEDURES
Applicable to: MSN,,,
ELECTRICAL EMERGENCY CONFIGURATION
In case of electrical emergency configuration, it may be better to study the STATUS on the paper
checklist, after having applied ECAM actions.
The flight crew must complete the ECAM procedure using the following :
AIR CONDITIONING
As cockpit and cabin temperature control is lost, it is recommended to open the cockpit door.
PRESSURIZATION
If one engine (or one bleed system) is failed, forward cargo ventilation must be closed to avoid
CAB PR EXCESS CAB ALT from being triggered on the ECAM during descent or cruise.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
EXTENDED RANGE OPERATIONS - PROCEDURES
A318/A319/A320/A321 FLEET PRO-SPO-40-50 P 4/6
FCOM 19 AUG 10
FUEL
As all fuel pumps are lost, the engines are fed by gravity.Refer to STLO-ABN-28 GRVTY FUEL
FEEDING Fuel gravity feed procedure).
ENGINE ANTI-ICE
Engine anti-ice valves are permanently open, although the ECAM memo ENG A. ICE is not
displayed on the ECAM (except if the ENG A. ICE pushbutton is at ON).
WING ANTI-ICE
If only one ENG BLEED is available, PACK 1 must be switched OFF, to avoid having both
packs and wing anti-ice supplied by a single bleed source.
ENGINE
As the engines are in N1 unrated mode, the power setting has to be done using tables given in
Refer to PER-THR-N1 N1 MODE THRUST CONTROLand following.
BLUE HYDRAULIC LOW LEVEL
Start the APU to ensure availability of the APU generator.
ENGINE OR IDG FAILURE
Start the APU and use the APU electrical channel.
ABN AND EMER PROCEDURES
Applicable to: ,
, MSN
ELECTRICAL EMERGENCY CONFIGURATION
In case of electrical emergency configuration, it may be better to study the STATUS on the paper
checklist, after having applied ECAM actions.
The flight crew must complete the ECAM procedure using the following :
AIR CONDITIONING
As cockpit and cabin temperature control is lost, it is recommended to open the cockpit door.
PRESSURIZATION
If one engine (or one bleed system) is failed, forward cargo ventilation must be closed to avoid
CAB PR EXCESS CAB ALT from being triggered on the ECAM during descent or cruise.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
EXTENDED RANGE OPERATIONS - PROCEDURES
A318/A319/A320/A321 FLEET PRO-SPO-40-50 P 5/6
FCOM 19 AUG 10
FUEL
As all fuel pumps are lost, the engines are fed by gravity.Refer to STLO-ABN-28 GRVTY FUEL
FEEDING Fuel gravity feed procedure).
ENGINE ANTI-ICE
Engine anti-ice valves are permanently open, although the ECAM memo ENG A. ICE is not
displayed on the ECAM (except if the ENG A. ICE pushbutton is at ON).
WING ANTI-ICE
If only one ENG BLEED is available, PACK 1 must be switched OFF, to avoid having both
packs and wing anti-ice supplied by a single bleed source.
BLUE HYDRAULIC LOW LEVEL
Start the APU to ensure availability of the APU generator.
ENGINE OR IDG FAILURE
Start the APU and use the APU electrical channel.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
EXTENDED RANGE OPERATIONS - PROCEDURES
Intentionally left blank
A318/A319/A320/A321 FLEET PRO-SPO-40-50 P 6/6
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
EXTENDED RANGE OPERATIONS - PERFORMANCES
A318/A319/A320/A321 FLEET PRO-SPO-40-60 P 1/14
FCOM 19 AUG 10
GENERAL
Applicable to: MSN
4566,,,
In case of electrical emergency configuration, the remaining engine reverts to N1 unrated mode.
Consequently the penalties on net ceilings Refer to PER-THR-N1 TAKEOFF N1must be taken into
account for ETOPS part of the flight.
The two following cases result in a fuel consumption increase :
‐ RAT extended Refer to STLO-ABN-24-V ELEC EMER CONFIG SYS REMAINING - AIR COND
PRESS.
‐ in electrical emergency configuration, the engine anti-ice valves are permanently open.
GENERAL
Applicable to:
, ,
MSN
The two following cases result in a fuel consumption increase :
‐ RAT extended Refer to STLO-ABN-24-V ELEC EMER CONFIG SYS REMAINING - AIR COND
PRESS.
‐ in electrical emergency configuration, the engine anti-ice valves are permanently open.
MAXIMUM DISTANCE (STILL AIR) TO DIVERSION AIRPORT IN NAUTICAL MILES
Applicable to:
DETERMINATION OF 60 MIN MAXIMUM DIVERSION DISTANCE (JAR-OPS 1.245)
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 14(32)
