空中客车PSS.A319.A320.A321系统手册.pdf

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+ TABLE OF CONTENTS

+ PANEL OVERVIEW

+ Panel views

- Full panel view

- Compact (“VFR”) panel view

- MCDU window open

- Expanded EFIS displays

- Overhead panel view

- Central pedestal window open

- Virtual cockpit view

+ MAIN PANEL COMPONENTS

+ GENERAL NOTES

- EFIS displays

- Thrust control

- Flight controls

+ PRIMARY FLIGHT DISPLAY

- General

- Flight Mode Annunciations

- Attitude data

- Specic indications on ground

- Guidance

- HDG-V/S Mode

- TRK-FPA Mode

- ILS Indications

- Airspeed

- Managed Descent speed range

- Altitude

- Heading

+ NAVIGATION DISPLAY

- General

- ND Modes

- ND Common information

- ROSE ILS Mode

- ROSE VOR Mode

- ROSE NAV Mode

- ARC Mode

- PLAN Mode

+ ENGINE / WARNING DISPLAY

- General

- Engine parameters - IAE engines

- Engine parameters - CFM engines

- Main control parameter

- Flaps / Slats indicator

- Warning / Memo display

- Takeoff Memo

- Landing Memo

+ SYSTEM DISPLAY

- General

- SD Page selection

- Phase of Flight

- System monitoring

- Manual page selection

- CRUISE page

- Permanent data display

+ AUTOFLIGHT

- Overview

- Flight Control Unit (FCU)

- Flight Directors

- Autopilots

- A/P and F/D indications on FMA

- Autothrust

- Thrust levers

- A/THR status

- Autothrust modes

- Autothrust Flight Mode Annunciations

- Thrust modes

- A/THR status

- Thrust reduction prompt

- Alpha Floor

- Speed guidance

- Selected speeds

- Managed speeds

- Using selector knobs in Flight Simulator

- Lateral guidance

- Selected lateral modes

- Managed NAV mode

- LOC mode

- LOC* mode

- RWY mode

- Vertical guidance

- Open Climb (OP CLB)

- Open Descent (OP DES)

- Expedite modes

- Vertical Speed (V/S)

- Flight Path Angle (FPA)

- Managed vertical guidance

- Altitude acquire modes

- Vertical mode reversions

- Speed Reference System

- Approach and landing modes

- LOC and G/S modes

- Autoland

- Flight Mode Annunciation

+ MCDU

- Overview

- Color use

- Keyboard

- General principles

- Vertical ight plan

- Performance data

- Flight phases

- MCDU Menu page

- INIT A page

- INIT B page

- FUEL PRED page

- FLIGHT PLAN A page

- Page Title

- Waypoints (Line 1..5)

- Destination (Line 6)

- Route modication

- Inserting a waypoint

- Deleting a waypoint

- Setting waypoint constraints

- FLIGHT PLAN B page

- Lateral Revision pages

- Departure pages

- Arrival pages

- Direct To page

- Vertical Revision pages

- PERF pages

- PERF TAKEOFF page

- PERF CLIMB page

- PERF CRUISE page

- PERF DESCENT page

- PERF APPROACH page

- PERF GO AROUND page

- PROG pages

- DATA INDEX page

- WAYPOINT page

- NAVAID page

- RUNWAY page

- STATUS page

- SAVE ROUTE page

- LOAD ROUTE page

- IMPORT FS ROUTE page

- POSITION MONITOR page

- RADIO NAV page

+ BACKUP INSTRUMENTS

- Standby instruments

- DDRMI

+ Landing Gear

- Gear panel

- ECAM WHEEL page

+ Controls on central pedestal

- Thrust levers

- Engine panel

- Speed brakes

- Flaps

- Parking brake

- Radio Management Panels

- Transponder

+ APU

- Overview

- APU Controls and indications

+ Electrical system

- Overview

- Controls and indications

+ Fuel system

- Overview

- Controls and indications

+ Powerplant

- Controls and indications

- Engine panel

- Manual engine start panel

- ECAM ENG page

- Engine startup requirements

- Automatic startup

- Manual startup

- Shutdown

+ Hydraulics

- Overview

- Controls and indications

+ Pneumatics

- Overview

- Controls and indications

+ Air Conditioning

- Overview

- ECAM BLEED page

- ECAM COND page

+ Pressurization

- Overview

- Automatic pressure control

- Controls and indications

- ECAM PRESS page

- ECAM CRUISE page

+ GPWS

- Overview

- Controls and indications

- GPWS - G/S button

+ Other controls

- Other controls on overhead panel

+ Chronometer

+ Panel cofiguration utility

- Startup tab

- Panel Sound Volume tab

- Keyboard Assignments tab

- MCDU Keyboard tab

- Finishing the setting up

PSS A319 / A320 / A321 Systems Manual February 23, 2002

Phoenix Simulation Software A319/320/321 Systems Manual TABLE OF CONTENTS P 2 SEQ 001 REV 01 Panel Overview Main Panel Components General Notes Primary Flight Display Navigation Display Engine / Warning Display System Display Autoight MCDU Backup Instruments Landing Gear Controls on Center Pedestal APU Electrical System Fuel System Powerplane Hydraulics Pneumatics Air Conditioning Pressurization GPWS Other Controls Chronometer Panel Conguration utility 3 5 6 7 15 24 28 30 40 66 67 68 71 72 74 76 77 79 81 83 85 86 87 88

Phoenix Simulation Software A319/320/321 Systems Manual Panel views PANEL OVERVIEW P 3 SEQ 001 REV 01 The Phoenix Airbus A3xx panel has several pop-up windows and can be represented in different views, as shown below: Full panel view is the default view. It shows all EFIS displays and all gauges on the main panel. To return to full view from Compact or Overhead view, press NUMPAD 8 key. Full panel view Compact (“VFR”) panel view MCDU window open Compact panel view provides good outside view while including the most important displays, instruments and controls. Compact view is accessed by pressing and holding NUMPAD 2 key. To keep this view active, press and hold NUMPAD 2, then press CTRL, then release both. MCDU window shows expanded view and allows operation of Multipurpose Control Display Unit. This window is opened or closed by clicking on MCDU screen image on main panel view, or by pressing Shift+2 key.

Phoenix Simulation Software A319/320/321 Systems Manual PANEL OVERVIEW P 4 SEQ 001 REV 01 Each of EFIS displays presents a wealth of information. To help reading these displays, each of them can be expanded by clicking on it. Expanded displays are pop-up windows and can be moved and resized to your taste, or even undocked and dragged to another monitor. An expanded display can be closed by clicking on its upper right part. Shortcut keys for displays are, Shift+4 for PFD, Shift+5 for ND, Shift+6 for Upper ECAM, and Shift+7 for Lower ECAM. Overhead panel contains controls for aircraft systems such as Electrical, Fuel, Pressurization etc. Overhead view is accessed by pressing and holding NUMPAD 5 key. To keep this view active, press and hold NUMPAD 5, then press CTRL, then release both. Central pedestal carries thrust levers, aps and spoilers con- trols, engine starting controls, etc. Central pedestal window is opened and closed by pressing Shift+2 key. Virtual cockpit view Expanded EFIS displays Overhead panel view Central pedestal window open Flight Simulator Virtual Cockpit view contains full set of gauges. Although, due to FS limitation, the custom-drawn (“vector”) gauges are inoperative in Virtual Cockpit, and thus the EFIS displays are replaced with different versions with some ele- ments missing. Also, mouse clicks do not work in this mode.

Phoenix Simulation Software A319/320/321 Systems Manual MAIN PANEL COMPONENTS P 5 SEQ 001 REV 01 The Airbus has a modern glass cockpit. Mechanical gauges are replaced by an Electronic Flight Instrument System (EFIS) which includes six CRT displays representing all information in most convenient form. The displays include Captain and FO Primary Flight Displays (PFD), Captain and FO Navigation Displays (ND), and two Electronic Centralized Aircraft Monitoring (ECAM) displays: Engine/Warning Display (E/WD) and System Display (SD). Mechanical backup instruments are also provided. Automatic ight is controlled from Flight Control Unit (FCU). Fully automatic ight along a programmed route is possible and is guided by Flight Management System (FMS). The FMS is programmed and operated using Multi-function Control and Display Units (MCDU). Chronometer button EFIS Control Panel Flight Control Unit (FCU) Primary Flight Display (PFD) Navigation Display (ND) Engine/Warning Display (E/WD) Gear panel GPWS indicatior Backup Instruments DDRMI System Display (SD) Clock MCDU ECAM Control Panel

Phoenix Simulation Software A319/320/321 Systems Manual EFIS displays GENERAL NOTES P 6 SEQ 001 REV 01 EFIS displays contain a wealth of information. At standard display resolutions, they can be hard to read. To solve this, any display can be expanded by clicking it with the mouse. This brings a pop-up window with enlarged display picture. Such windows are standard Flight Simulator pop-up windows. They can be resized, moved to any position and arranged to your taste. You can drag a window clicking at any place, except for the area in upper right corner - clicking there will close the window. A window can be undocked by right-clicking it and selecting “Undock” in pop-up menu. This allows the window to be moved outside main FS window and placed anywhere on desktop, or on second monitor. The same can be done with MCDU pop-up window. Thrust control The A320 aircraft thrust levers are different from those found on Boeing-type or other common aircraft. The thrust levers move through distinct detents, or gates, marked “MREV”, “IDLE”, “CL”, “FLX/MCT”, and “TO-GA”. Takeoff power is applied by moving the levers to TO-GA or FLX-MCT gate, which commands autothrust system to produce computed takeoff thrust corresponding to current conditions. At thrust reduction altitude, thrust levers are retarded to CL gate, which automatically engages autothrust system. From this point, the levers are normally left in CL detent through all the ight until just before touchdown. Autothrust system controls engine thrust corresponding to active thrust modes and thrust limits. The A320 thrust levers are not back-driven by autothrust system, and don’t move as the thrust is automatically adjusted. Unless needed, they are left in CL gate until synthesized voice announces “RETARD” 20 feet above landing runway. Due to this, thrust control is implemented differently than on other Flight Simulator panels. Instead of using joystick throttle or Flight Simulator keys, the panel uses custom keys (Numpad PLUS and Numpad MINUS by default) to move thrust levers between gates. You can also use pedestal view and move levers with the mouse. Thrust levers position can be checked by looking at thrust Flight Mode Annunciator on PFD, the thrust limit name on E/WD, or by checking the pedestal view. Manual thrust control is still possible, using joystick throttle or Flight Simulator keys. Make sure that the panel-simulated thrust levers are left at IDLE, or set at CL but the autothrust is disengaged. Please check Autothrust discussion in Autoight section of this manual for further information. Flight controls The PSS A320 panel attempts to simulate electronic y-by-wire ight control system of the real aircraft. The conventional ight yokes are replaced on Airbus aircraft with side-sticks, much like a computer joystick. Sidesticks send electronic signals to ight computers, which drive the control surfaces. Left-right stick deection controls bank rate, and computers will not allow to exceed bank limits of ±67° bank. Forward-aft stick deection controls aircraft G load. Neutral stick position commands load of 1 G, resulting in level ight or constant vertical speed, regardless of airspeed, altitude or weight. This is simulated in PSS panel by auto-trimming the aircraft, although this can be done only when the joystick is centered. The joystick inputs to Flight Simulator are disabled when the autopilot is engaged. This is done to prevent joystick noise from interferring with autopilot operation.

Phoenix Simulation Software A319/320/321 Systems Manual General PRIMARY FLIGHT DISPLAY P 7 SEQ 001 REV 01 The Primary Flight Display (PFD) is the outer display on Captain and FO panels. It provides information on: • Attitude and Guidance commands • Airspeed • Barometric and radio altitude and vertical speed • Heading and track • Flight Mode Annunciations • Vertical and lateral deviations The PFD is divided into several sections: Flight Mode Annunciations Attitude and Guidance Airspeed Altitude and Vertical Speed Heading and Track Flight Mode Annunciations Flight Mode Annunciator (FMA) are indications of current status of FMS operation. The FMA is divided into 5 columns which indicate: The Flight Mode Annunciations are discussed in detail in Autoight and FCU section. • Thrust modes • Active and armed Pitch modes • Active and armed Roll modes • Approach capabilities • Autopilot, Flight Director and Autothrust engagement status

Phoenix Simulation Software A319/320/321 Systems Manual PRIMARY FLIGHT DISPLAY P 8 SEQ 001 REV 01 Attitude data Roll Scale Roll/Sideslip Index Aircraft symbol Pitch Scale Attitude Limits Radar Altitude Aircraft symbol Fixed aircraft symbol indicates position of aircraft relative to the horizon. Roll Scale The scale is graduated at 0, 10, 20, 30 and 45 bank degrees. Roll/Sideslip Index Upper part of the index indicates current bank. The lower part moves below roll part and shows amount of side slip. Pitch Scale Graduated each 2.5 degrees, indicates current aircraft pitch. Attitude Limits Green ‘=’ symbols are displayed at ±67° on roll scale, at 15° nose down and at 30° nose up on pitch scale. They represent the pitch and bank limits of Normal law protections. Radar Altitude Radar altimeter readout is displayed when below 2500 feet AGL. At low altitudes, the white line which separates pitch scale and solid bottom part, moves up as aircraft gets closer to the ground, covering the pitch scale, and meets the horizon line at touchdown. Radar altimeter readout turns yellow when below DH, if it was set. Specic indications on ground Ground roll command bar Sidestick position Max sidestick deection Ground roll command bar Indicates ground roll guidance command in RWY mode, which keeps runway course Sidestick position Indicates the position of sidestick (joystick). Appears after second engine start and is removed at takeoff power application. Max sidestick deection Four corners dene maximum sidestick deection.

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