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┃)P, MAL OPERATION ┃ MEMO ┃
┃3 OR LDG MEMO ┃ ┃
┃-Y ITEMS FOR T.O ┃ or ┃
┃ LDG) ┃WARNING / CAUTIOI~ messages ┃
┃ ┃ I ┃
┃ ┃\ s ┃
┗━━━━━━━━━━┻━━━━━━━━━━━━━━━━━━━┛
WARNING/CAUTION MESSAGES
- TITLE OF THE FAILURE
- CORRESPONDING PROCEDURES
(ACTIONS TO BE PERFORMED)
STATUS
OPERATIONAL STATUS
OF THE AIRCRAFT
AFTER FAILURE INCLUDING
RECOVERY PROCEDURES
PERMANENT DATA
- TAT
- SAT
- UTC
-G.W
CCM ALL
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┃I -~ A318 ┃FLIGHT CONTROLS ┃1.27.20 P 5 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃ NORMAL LAW ┃SEQ 001 ┃REV 30 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━┻━━━━┛
HIGH-SPEED PROTECTION
The aircraft automatically recovers following a high speed upset. Depending on the flight
conditions (high acceleration, low pitch attitude), the High Speed Protection is activated
at/or above VMO/MMO.
When it is activated, the pitch trim is frozen. Positive spiral static stability is introduced to
0~ bank angle (instead of 33~ in normal law), so that with the sidestick released, the aircraft
always returns to a bank angle of 0~. The bank angle limit is reduced from 67~ to 45~.
As the speed increases above VMO/MMO, the sidestick nose-down authority is
progressively reduced, and a permanent nose-up order is applied to aid recovery to normal
flight conditions.
The High Speed Protection is deactivated when the aircraft speed decreases below
VMO/MMO, where the usual normal control laws are recovered.
The autopilot disconnects when high speed protection goes active.
High speed protection ~y~boL:lJ
Two green bars at VMO
Note : The ECAM displays an "O/SPEEO" warning at VMO + 4 knots and MMO + 0.006
LOW ENERGY WARNING <~
The low energy warning is computed by the FAC, see 1.22.40
CCM ALL
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual3(86)
