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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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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual2(151)