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┃ RECORDER ┃CVR ┃ ┃ ┃SHED ┃ ┃ ┃
┣━━━━━━━━━━━━━━━╋━━━━━━━━━╋━━╋━━━━╋━━━╋━━━╋━━━┫
┃ACARS<~ ┃ ┃AC1 ┃ ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━┻━━━━━━━━━┻━━┻━━━━┻━━━┻━━━┻━━━┛
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.27.20 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-~ A318 ┃I FLIGHNORMALRLAW ┃SEQ 001 1 ┃I REV 23 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
HIGH ANGLE OF ATTACK PROTECTION
Under normal law, when the angle of attack becomes greater than c~prot, the system
switches elevator control from normal mode to a protection mode in which angle of attack
is proportional to sidestick deflection. That is, in the ~prot range, from ~ prot to ~max, the
sidestick commands c~ directly. However, the angle of attack will not exceed c~max, even
if the pilot gently pulls the sidestick all the way back. If the pilot releases the sidestick, the
angle of attack returns to c~prot and stays there.
This protection against stall and windshear has priority over all other protections. The
autopilot disconnects at ~ prot + 1~.
┏━━━━━━━━━━━━━━━━━━┓
┃(LIFT ┃
┃COEFFICIENT) lg sta ┃
┣━━━━━━┳━━━━┳━━━━━━┫
┃ ┃ ┃4 ┃
┃ ┣━━━━╋━━━━━━┫
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(151)
