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┃ A~7-~'M" A321 ┃CONTROLS AND INDICATORS ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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┃ ┃ ┃1.27.40 P 6 ┃
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┃I -~ A318 ┃I CONTROLSTANDNINDICATORS ┃SEQ 100 1 ┃I REV 24 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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O ELAC 1(2) pb sw
Controls the elevator and aileron control (ELAC) computer 1(2).
ON ELAC 1(2) performs the following functions :
- normal pitch and roll
- alternate pitch
- direct pitch and roll
- abnormal attitude
- aileron droop
- acquisition of autopilot orders.
OFF The corresponding computer is not active. Switching it OFF and then ON resets
the computer.
FAULT Lights up in amber, along with a "CAUTION" advisory on ECAM :
- when a failure is detected
- during ELAC power-up test (eight seconds).
Note : ELAC power-up test occurs when electrical power is turned on or after
the occurrence of an electrical transient lasting longer than 25
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(97)
