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ELAC    1  2                                             1  2    ELAC
SEC             2   1   1   3   3     3   3   1   1   2             SEC
            SFCC 1
SLATS IGISFCC 2
ELAC
SEC
THS HYDRAULIC       SFCC 2
    MOTORS
~ FLAPS
ELAC
 SEC
                                 FAC 1  2
                  YAW DAMPER     H B I  X
                    ACTUATOR      ~J~
FAcFAC 1 ~+~ RUDD~E~~  2
  MECH CONT          ~     ~FAcFAC I~RUD TRIM
Arrows indicate the control reconfiguration priorities
indicates the hydraulic power source (green. blue. or yellow)
for each servo control.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.27.10     P 6       ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃I        FLIGHTDESCRIPTION  ┃SEQ 001 1 ┃I REV 23  ┃
┃  .,,,.8, ,, ~L,~ A319          ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
PITCH CONTROL
Two elevators and the trimmable horizontal stabilizer (THS) control the aircraft in pitch. The
maximum elevator deflection is 30~ nose up and 15~ nose down. The maximum THS
deflection is 13.5~ nose up and 4~ nose down.
ELECTRICAL CONTROL
- In normal operations, the ELAC2 controls the elevators and the horizontal stabilizer, and
  the green and yellow hydraulic jacks drive the left and right elevator surfaces
   respectively.
   The THS is driven by N~ 1 of three electric motors.
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(75)