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computing predictions. The airline does not have access to this database.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃I  -~ A318                      ┃AUTO FLIGHT ┃1.22.10     P 3   ┃
┃  .*,,.8, ,, ~L,~ A319          ┃            ┃                  ┃
┃ Lli,~ A320                     ┃            ┃                  ┃
┃                                ┃            ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃  GENERAL   ┃SEQ 001 ┃REV 25  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
MULTIPURPOSE CONTROL AND DISPLAY UNIT (MCDU)
Two MCDUs are installed on the pedestal for flight crew loading and display of data. The
use MCDU allows the flight crew to interface with the FMGC by selection of a flight plan
for lateral and vertical trajectories and speed profiles. The crew may also modify selected
navigation or performance data and specific functions of Flight Management (revised flight
plan, engine-out, secondary flight plan, etc.). Additional data from peripherals (Centralized
Fault Display System (CFDS), ARINC Communications, Reporting System (ACARS) can also
be displayed. Data that is entered into the MCDU that is illogical or beyond the aircraft
capabilities will either be disregarded or will generate an advisory message.
FLIGHT CONTROL UNIT (FCU)
The FCU located on the glareshield, is the short-term interface between the crew and the
FMGC. It is used to select any flight parameters or modify those selected in the MCDU. The
autopilots and autothrust functions may be engaged or disengaged. Different guidance
modes can be selected to change various targets (speed, heading, track, altitude, flight
path angle vertical speed).
FLIGHT AUGMENTATION COMPUTER (FAC)
The FAC controls rudder, rudder trim and yaw damper inputs. It computes data for the flight
envelope and speed functions. The FAC also provides warning for low-energy and
windshear detection if these functions are installed.
OTHER CREW INTERFACES
THRUST LEVERS
The thrust levers are the main interface between the Flight Management Guidance
Computer, the Full Authority Digital Engine Control System (FADEC), and the flight crew.
They :
- arm the autothrust at takeoff, when "FLX " or "TOGA" is selected,
- limit the maximum thrust by their position when autothrust is active,
- disconnect the autothrust system when the flight crew sets them to "IDLE",
- command the thrust manually when autothrust is not active,
engage the common modes (takeoff or go-around) when TOGA (or "FLX" for takeoff) is
set,
when positionned between IDLE and CL detent (MCT in engine out), set the autothrust
to the active mode.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                          ┃1.22.10     P 4       ┃
┃                                ┃                          ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃l          AUTO FGENERAL  ┃SEQ 001 1 ┃I REV 25  ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual1(140)