曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
‐ A refuel panel is located on the fuselage side beneath the right wing or under the right wing
adjacent to the refuel coupling.
A gallery connects the refuel coupling to each tank's refuel valve.
Refueling is normally automatic, the required fuel load being set on the preselector.
Manual control is also available.
Automatic refueling starts with the wing tanks. If the preselected fuel load exceeds the capacity of the
wing tanks, the center tank receives fuel simultaneously.
Refuel valves close automatically, when the tanks contain the preselected load, or when sensors
detect a high fuel level.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - REFUELING AND DEFUELING
A318/A319/A320/A321 FLEET DSC-28-10-70 P 3/6
FCOM 19 AUG 10
The aircraft can be refueled, when only battery power is available.
The wing tanks can be refueled by gravity, through refueling points on top of the wings.
A transfer valve, between the engine feed system and the refueling gallery, allows :
‐ The tank pumps to transfer fuel from one tank to another.
‐ Defueling through the refuel coupling.
Approximate refueling time at nominal pressure is :
‐ 17 min for wing tanks.
‐ 20 min for all tanks.
REFUELING - DEFUELING
Applicable to:
MSN,
‐ One (two) refueling point(s) is (are) installed under the wings, enabling the aircraft to be refueled
from either the right or left side.
‐ A refuel panel is located on the fuselage side beneath the right wing, or under the right or left wing
adjacent to the refuel coupling.
‐ Another refuel panel is located on the cockpit overhead maintenance panel.
‐ A "READY FOR FUELING" green light is installed adjacent to the refuel coupling.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - REFUELING AND DEFUELING
A318/A319/A320/A321 FLEET DSC-28-10-70 P 4/6
FCOM 19 AUG 10
A gallery connects the refuel coupling to each tank's refuel valve.
Refueling is normally automatic, the required fuel load being set on the preselector.
Manual control is also available.
Automatic refueling starts with the outer cells. If the selected fuel load exceeds the wing tank
capacity, the center tank is simultaneously refueled.
When an outer cell is full the fuel overflows into the inner cell through a spill pipe.
Refuel valves close automatically, when the tanks contain the preselected load, or when sensors
detect a high fuel level.
The aircraft can be refueled, when only battery power is available.
The wing tanks can be refueled by gravity, through refueling points on top of the wings.
A transfer valve, between the engine feed system and the refueling gallery, allows :
The tank pumps to transfer ‐ fuel from one tank to another.
‐ Defueling through the refuel coupling.
Approximate refueling time at nominal pressure is :
‐ 17 min for wing tanks.
‐ 20 min for all tanks.
REFUELING - DEFUELING
Applicable to: MSN,
‐ One (two) refueling point(s) is (are) installed under the wings, enabling the aircraft to be refueled
from either the right or left side.
‐ A refuel panel is located on the fuselage side beneath the right wing, or under the right or left wing
adjacent to the refuel coupling.
‐ Another refuel panel is located on the cockpit overhead maintenance panel.
‐ A "READY FOR FUELING" green light is installed adjacent to the refuel coupling.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
DESCRIPTION - REFUELING AND DEFUELING
A318/A319/A320/A321 FLEET DSC-28-10-70 P 5/6
FCOM 19 AUG 10
A gallery connects the refuel coupling to each tank's refuel valve.
Refueling is normally automatic, the required fuel load being set on the preselector.
Manual control is also available.
Automatic refueling starts with the wing tanks. If the preselected fuel load exceeds the capacity of the
wing tanks, the center tank receives fuel simultaneously.
Refuel valves close automatically, when the tanks contain the preselected load, or when sensors
detect a high fuel level.
The aircraft can be refueled, when only battery power is available.
The wing tanks can be refueled by gravity, through refueling points on top of the wings.
A transfer valve, between the engine feed system and the refueling gallery, allows :
‐ The tank pumps to transfer fuel from one tank to another.
‐ Defueling through the refuel coupling.
Approximate refueling time at nominal pressure is :
‐ 17 min for wing tanks.
‐ 20 min for all tanks.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 3(53)
