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┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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PITCH CONTROL - SCHEMATIC
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┃l ~_~-~ .4318 ┃FLIGHT CONTROLS ┃1.27.10 P g ┃
┃ ~ ~ ,, ~r~ .43"19 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lll,~ A320 ┃ ┃SEQ 105 I ┃J REV 28 ┃
┃ A~7-~'M" .4321 ┃ DESCRIPTION ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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BOLL CONTROL
AILERONS HYDRAULIC
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┃ ┃
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┃~NDS ZI ELAC ,k2~ "Tx I I ┃
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┃ ┃ I,~lIIIIII ~')~ ~ SPOILERS 2,3,4~& ┃
┗━┻━━━━━━━━━━━━━━━━━━━━━━━━━━━┛
One aileron and four spoilers on each wing control the aircraft about the roll axis
The maximum deflection of the ailerons is 25~.
The ailerons extend 5~ down when the flaps are extended (aileron droop).
The maximum deflection of the spoilers is 35~.
ELECTRIC CONTROL
S
The ELAC 1 normally controls the ailerons.
If ELACl fails, the system automatically transfers aileron control to ELAC2.
If both ELACs fail, the ailerons revert to the damping mode.
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(77)
