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
┃ ┃ ┃1.27.20 P 6 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I FLIGHNORMALRLAW ┃SEQ 001 1 ┃I REV 30 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
NORMAL LAW
When the aircraft is on the ground (in "on ground" mode), the sidestick commands the
aileron and roll spoiler surface deflection. The amount of control surface deflection that
results from a given amount of sidestick deflection depends upon aircraft speed. The pedals
control rudder deflection through a direct mechanical linkage.
When the aircraft is in the "in flight" mode, normal law combines control of the ailerons,
spoilers (except N~ 1 spoilers), and rudder (for turn coordination) in the sidestick. While the
system thereby gives the pilot control of the roll and heading, it also limits the roll rate and
bank angle, coordinates the turns, and damps the dutch roll.
The roll rate requested by the pilot during flight is proportional to the sidestick deflection,
with a maximum rate of 15~ per second when the sidestick is at the stop.
When the aircraft is in "flare" mode, the lateral control is the same as in "in flight" mode.
BANK ANGLE PROTECTION
Inside the normal flight envelope, the system maintains positive spiral static stability for
bank angles above 33~. If the pilot releases the sidestick at a bank angle greater than 33~,
the bank angle automatically reduces to 33~. Up to 33~, the system holds the roll attitude
constant when the sidestick is at neutral. If the pilot holds full lateral sidestick deflection,
the bank angle goes to 67~ (indicated by a pair of green bar lines "=" on the PFD) and no
further.
If the angle-of-attack protection or high speed protection is operative, the bank angle goes
to 45~ and no further, if the pilot holds full lateral sidestick deflection. If high speed
protection is operative, the system maintains positive spiral static stability from a bank
angle of 0~, so that with the sidestick released, the aircraft always returns to a bank angle
of 0~.
When bank angle protection is active, auto trim is inoperative.
If the bank angle exceeds 45~, the autopilot disconnects and the FD bars disappear. The FD
bars return when the bank angle decreases to less than 40~.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I ~-~ A318 ┃FLIGHT CONTROLS ┃1.27.20 P 7 ┃
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(87)
