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
‐ . If APU start is unsuccessful, a windmilling relight can be performed, as long as the speed
is above 360 kt (corresponding N2 above 18 %). In this case, increase the aircraft speed
and disregard VMO warning.
If APU is available : perform an assisted relight, when below FL 200.
‐ Flight controls are in direct laws. Use manual pitch trim as necessary (not indicated on PFD
if APU GEN not available).
‐ In approach, set CONF 1 at or above 200 kt. Do not select flaps/slats below 200 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A318/A319/A320/A321 FLEET PRO-SPO-25-40 P 1/60
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
Consider the increase in drag to determine the takeoff weight and fuel consumption.
CONF 1 + F is the recommended takeoff configuration.
Note: Takeoff with tail wind is not recommended.
Penalties on takeoff performance affect second segment gradient condition, final takeoff condition
and en-route conditions. The takeoff weight to be retained is the most limiting of these three
conditions.
SECOND SEGMENT GRADIENT CONDITION
Applicable to: MSN
The RTOW charts or the quick reference tables give the basic information for normal takeoff. To
simplify, a constant weight reduction is applied whatever the limitation. This weight reduction covers
the most critical case presented for flying over an obstacle.
Takeoff configuration 1 + F 2 3
Weight reduction 22 % 18 % 18 %
METHOD
Use the RTOW chart or the quick-reference tables to define the maximum takeoff weight for the
conditions on the airport (temperature, pressure, wind, runway...), then apply the above weight
reduction.
SECOND SEGMENT GRADIENT CONDITION
Applicable to:
The RTOW charts or the quick reference tables give the basic information for normal takeoff. To
simplify, a constant weight reduction is applied whatever the limitation. This weight reduction covers
the most critical case presented for flying over an obstacle.
Takeoff configuration 1 + F 2 3
Weight reduction 22 % 19 % 19 %
METHOD
Use the RTOW chart or the quick-reference tables to define the maximum takeoff weight for the
conditions on the airport (temperature, pressure, wind, runway...), then apply the above weight
reduction.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A318/A319/A320/A321 FLEET PRO-SPO-25-40 P 2/60
FCOM 19 AUG 10
SECOND SEGMENT GRADIENT CONDITION
Applicable to:
The RTOW charts or the quick reference tables give the basic information for normal takeoff. To
simplify, a constant weight reduction is applied whatever the limitation. This weight reduction covers
the most critical case presented for flying over an obstacle.
Takeoff configuration 1 + F 2 3
Weight reduction 20 % 18 % 18 %
METHOD
Use the RTOW chart or the quick-reference tables to define the maximum takeoff weight for the
conditions on the airport (temperature, pressure, wind, runway...), then apply the above weight
reduction.
SECOND SEGMENT GRADIENT CONDITION
Applicable to: MSN
The RTOW charts or the quick reference tables give the basic information for normal takeoff. To
simplify, a constant weight reduction is applied whatever the limitation. This weight reduction covers
the most critical case presented for flying over an obstacle.
Takeoff configuration 1 + F 2 3
Weight reduction 18 % 15 % 14 %
METHOD
Use the RTOW chart or the quick-reference tables to define the maximum takeoff weight for the
conditions on the airport (temperature, pressure, wind, runway...), then apply the above weight
reduction.
SECOND SEGMENT GRADIENT CONDITION
Applicable to:
The RTOW charts or the quick reference tables give the basic information for normal takeoff. To
simplify, a constant weight reduction is applied whatever the limitation. This weight reduction covers
the most critical case presented for flying over an obstacle.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A318/A319/A320/A321 FLEET PRO-SPO-25-40 P 3/60
FCOM 19 AUG 10
Takeoff configuration 1 + F 2 3
Weight reduction 24 % 22 % 21 %
METHOD
Use the RTOW chart or the quick-reference tables to define the maximum takeoff weight for the
conditions on the airport (temperature, pressure, wind, runway...), then apply the above weight
reduction.
SECOND SEGMENT GRADIENT CONDITION
Applicable to:
The RTOW charts or the quick reference tables give the basic information for normal takeoff. To
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 14(19)
