曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

┃                      ┃    pitch control       ┃                      ┃                          ┃
┣━━━━━━━━━━━╋━━━━━━━━━━━━╋━━━━━━━━━━━╋━━━━━━━━━━━━━┫
┃"DUAL INPUT"          ┃ Both sidesticks are    ┃                      ┃                          ┃
┃(synthetic voice)     ┃moved simultaneously    ┃Every5 seconds        ┃One sidestick deactivated ┃
┗━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━━━━━━━━┻━━━━━━━━━━━━━┛
*  The pilot can cancel any aural warning by pressing ~
    - The EMER CANC pushbutton on the ECAM control panel,
    -The MASTER WARN pushbutton, except for OVERSPEED or L/G NOT DOWN
       warnings.
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━┓
┃I  ~-~ A318                     ┃INDICATING/RECORDING SYSTEMS  ┃1.31.15     P 1   ┃
┃ aw aw ,, ~L,~ A319             ┃                              ┃                  ┃
┃ Lli,~ A320                     ┃                              ┃                  ┃
┃                                ┃                              ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃       INDICATIONS ON E/WD    ┃SEQ 001 ┃REV 26  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                              ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━┻━━━━┛
The E/WD appears on the upper ECAM display unit (DU).
- The upper part of this DU displays :
   ~ Engine parameters (refer to 1.70.90)
   ~ Fuel on board (FOB)(refer to 1.28.20)
   ~ Position of slats and flaps (refer to 1.27.40)
- The lower part of this DU displays messages generated by the FWC
   ~ Warning and caution messages when a failure occurs
   ~ Memos when there is no failure
  ENGINE
PARAMETERS
The lower part, which is dedicated to ECAM messages, is divided into two parts of severa
lines each.
Left part
Right part
Primary or independent warnings and cautions, or
Memo information
Title of system affected by a primary or independent warning or caution in
case of overflow on the left part, or
Secondary failure, or
Memo, or
              - Special lines (such as "AP OFF", "LAND ASAP")
As soon as the FWC detects a failure, and if there is no flight phase inhibition active, the
E/WD displays the title of the failure and actions to be taken.
The action line clears automatically when the flight crew has executed the required action.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual4(25)