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
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┣━━━━┫ ┃ ┃
┃FCDC 1 (2) FAULT ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
┃SIDESTICK PRIORITY ┃ ┃ ┃NIL ┃ ┃3,4,5,6, ┃
┃Failure in a sidestick priority logic circuit ┃ ┃ ┃ ┃ ┃ 7,8,9 ┃
┗━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┻━━━━┻━━━━┻━━━━┻━━━━━┻━━━━━┛
"SPEED BRK" appears in green if the speed brakes are extended. It flashes amber if,
during flight, one engine's N1 is above 50 %.
"GND SPLRS ARMED" appears in green if ground spoilers are armed.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━┓
┃I ~-~ A318 ┃FLIGHT CONTROLS ┃1.27.50 P 1 ┃
┃ aw aw ,, ~% A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃FLAPS AND SLATS ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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GENERAL
Each wing has the following lift augmentation devices :
- two flap surfaces
- five slat surfaces.
These surfaces are electrically controlled and hydraulically operated.
The pilot extends slats and flaps by moving the FLAPS lever on the center pedesta
It has five positions.
MAIN COMPONENTS
The slat and flap systems are similar, comprising :
- Two slat flap control computers (SFCCs), each containing one slat channel and one flap
channel.
- A power control unit (PCU) consisting of two independent hydraulic motors coupled by
a differential gearbox.
The motors use green and blue hydraulic power for the slats and yellow and green
power for the flaps.
Pressure-off brakes (POBs) lock the transmission when the slat or flap surfaces have
reached the selected position or if hydraulic power fails.
- Five slat surfaces and two flap surfaces per wing.
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(111)
