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Thales FMGS Pilot's Manual

Thales FMGS Pilot's Manual

For a318, a319, a320, a321
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Table of Contents

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Summary of Contents for Thales FMGS

  • Page 1 New FM Pilot’s Guide New FM Pilot’s Guide REV 1 REV 1 A318 / A319 / A320 / A321 A318 / A319 / A320 / A321 Aerospace Division...

  • Page 3: Table Of Contents

    PART I – GENERAL DESCRIPTION ........2 PART II - FLIGHT PHASE PROCEDURES......3 PART III - MULTI PHASE PROCEDURES ......8 PART IV - DEGRADED OPERATIONS ......14 PART V - APPENDICES ..........15 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 4 FOREWORD CONTENTS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 5: Disclaimer

    User's sole risks. Thales Avionics disclaims any liability whatsoever for any appropriation or use of this Pilot's Guide directly or indirectly in relation with or for the purpose of any criminal, terrorist or whatever malevolent actions on the part of individuals or groups which may have access to this Pilot's Guide or part thereof by any means.

  • Page 6: Contact

    PLEASE CONTACT: techpubs.frontoffice@fr.thalesgroup.com Technical Publications Department 18, Avenue du Maréchal Juin - B.P. 49 92362 Meudon-la-Forêt Cedex France Tel : + 33-1-39-45-50-00 Fax : + 33-1-39-45-58-71 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 7: Authors' Note

    FOREWORD DISCLAIMER 3 AUTHORS' NOTE The THALES NEW FM as installed on A318/319/320/321 aircraft is part of the Flight Management & Guidance System (FMGS), which provides Flight Management (FM) and Flight Guidance (FG) functions. This guide was written by pilots for pilots. It provides information on utilization of the Flight Management (FM) functions of the FMGS.
  • Page 8 FOREWORD DISCLAIMER PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 9: Structure Of Guide

    VERTICAL F-PLN management SEC F-PLN FUEL monitoring NAVIGATION management & monitoring ENGINE-OUT OPERATION DATA LINK PRINT FUNCTION PART IV – FMGS DEGRADED OPERATIONS OVERVIEW FMGC RESETS AND FAILURES MCDU ANOMALIES OTHER DEGRADED OPERATIONS PART V – APPENDICES MESSAGES MCDU NAMING AND FORMAT...

  • Page 10: Guide Organization

    MCDU. Parts are divided into chapters and subjects. Tab dividers showing Part titles and numbers are provided for prompt identification. Part I - GENERAL DESCRIPTION is an overview of the FMGS and its philosophy, FMGC operation, MCDU functions and operations (for Abbreviations see PART V - Appendices).

  • Page 11: Guide Updating

    The head of each page presents Part name and Chapter name. Page identification consists of the standard page numbering within the chapter. The issue reference is placed in the lower right/left corner. Information concerning AIRBUS type applicability appears in the lower left/right corner AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 12 FOREWORD STRUCTURE OF GUIDE A normal blank page within a page block is identified with the phrase: INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 13: Figures

    ND or ECAM. GPS PRIMARY ......Check Scroll means using the MCDU slew key to adjust a value. Ex: Vertical slew keys Scroll Select means choosing the appropriate value or option. FCU SPEED ....Select/Pull AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 14: Supplementary Information

    Details not essential for operational use are omitted. Additional information which may be of interest is provided in italic text. Terminology Technical terms appearing through the guide are listed in the Abbreviations in Appendices. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 15: Record Of Revisions

    FOREWORD REVISIONS 1 2. RECORD OF REVISIONS Revision Description Date Initials Reference inserted J43126AA 00 First release. DEC 2004 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 16 FOREWORD REVISIONS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 17 J43126AA 00 LIST OF EFFECTIVE PAGES J43126AA 00 LIST OF EFFECTIVE PAGES J43126AA 00 LIST OF EFFECTIVE PAGES J43126AA 00 LIST OF EFFECTIVE PAGES J43126AA 00 LIST OF EFFECTIVE PAGES J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 18: List Of Effective

    J43126AA 00 FMGS OPERATION J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 MCDU J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 19: Part Ii - Flight Phase Procedures

    J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 PREFLIGHT J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 20 J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 CLIMB J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 21 J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 CRUISE J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 22 J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 APPROACH J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 23 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 DONE PHASE J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 24: Part Iii - Multi Phase Procedures

    J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 25 J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 LATERAL F-PLN management J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 26 VERTICAL F-PLN management J43126AA 00 VERTICAL F-PLN management J43126AA 00 SEC F-PLN J43126AA 00 SEC F-PLN J43126AA 00 SEC F-PLN J43126AA 00 SEC F-PLN J43126AA 00 SEC F-PLN J43126AA 00 SEC F-PLN J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 27 J43126AA 00 NAVIGATION management & monitoring J43126AA 00 NAVIGATION management & monitoring J43126AA 00 NAVIGATION management & monitoring J43126AA 00 NAVIGATION management & monitoring J43126AA 00 NAVIGATION management & monitoring J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 28 DATA LINK J43126AA 00 DATA LINK J43126AA 00 DATA LINK J43126AA 00 DATA LINK J43126AA 00 DATA LINK J43126AA 00 DATA LINK J43126AA 00 DATA LINK J43126AA 00 DATA LINK J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 29 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 PRINT FUNCTION J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 30: Part Iv - Degraded Operations

    J43126AA 00 FMGC RESETS AND FAILURES J43126AA 00 FMGC RESETS AND FAILURES J43126AA 00 FMGC RESETS AND FAILURES J43126AA 00 FMGC RESETS AND FAILURES J43126AA 00 FMGC RESETS AND FAILURES J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 31: Part V - Appendices

    MCDU NAMING and DATA FORMAT J43126AA 00 MCDU NAMING and DATA FORMAT J43126AA 00 MCDU NAMING and DATA FORMAT J43126AA 00 MCDU NAMING and DATA FORMAT J43126AA 00 MCDU NAMING and DATA FORMAT J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 32 J43126AA 00 ND SYMBOLS J43126AA 00 ND SYMBOLS J43126AA 00 ND SYMBOLS J43126AA 00 ND SYMBOLS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 33 REVISION ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 ABBREVIATIONS J43126AA 00 PAGE REVISION MCDU FOLDOUT J43126AA 00 MCDU FOLDOUT J43126AA 00 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 34 FOREWORD LIST OF EFFECTIVE PAGES PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 35 Part I FMS GENERAL DESCRIPTION AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 36 PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 37 2.1. FLIGHT DECK CONFIGURATION ..........3 2.2. SYSTEM INTERFACES............4 2.3. PILOT INTERFACES ..............5 2.4. FLIGHT PHASES..............9 Chapter 3 - FMGS OPERATION 3.1. FMS MODES OF OPERATION: Dual/Single/Independent..3 3.2. TEMPORARY FLIGHT PLAN ...........6 3.3. NAVIGATION/FLIGHT MANAGEMENT ........7 3.4. SOFTWARE AND DATABASE ..........18 Chapter 4 –...
  • Page 38 FMGS GENERAL PRESENTATION CONTENTS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 39 FMS GENERAL DESCRIPTION INTRODUCTION 1 Part I: Chapter 1 – INTRODUCTION The THALES Flight Management & Guidance System (FMGS), as installed on Airbus Single-Aisle Family (A318/319/320/321), provides Flight Management (FM) and Flight Guidance (FG) functions. The main FM functions are: −...
  • Page 40 FMS GENERAL DESCRIPTION INTRODUCTION PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 41 SYSTEM OVERVIEW 1 Part I: Chapter 2 – SYSTEM OVERVIEW Contents 2.1. FLIGHT DECK CONFIGURATION ......... 3 2.2. SYSTEM INTERFACES ..........4 2.3. PILOT INTERFACES ............ 5 2.4. FLIGHT PHASES ............9 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 42: Chapter 2 - System Overview

    FMS GENERAL DESCRIPTION SYSTEM OVERVIEW PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 43: Flight Deck Configuration

    FMS GENERAL DESCRIPTION SYSTEM OVERVIEW 3 2.1. FLIGHT DECK CONFIGURATION The location of the cockpit components of the FMGS is shown below. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 44: System Interfaces

    FMS GENERAL DESCRIPTION SYSTEM OVERVIEW 2.2. SYSTEM INTERFACES The FMGCs receive and transmit signals from and to other aircraft systems. Figure here under shows the interconnections between these systems and the FMGCs. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 45: Pilot Interfaces

    FMS GENERAL DESCRIPTION SYSTEM OVERVIEW 5 2.3. PILOT INTERFACES The figure shows the pilot interfaces and their interconnection. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 46 FMS GENERAL DESCRIPTION SYSTEM OVERVIEW The main interfaces for crew inputs to FMGS are FCU, MCDUs and Thrust Levers (T/L). Outputs of FMGS are monitored on the EFIS (PFD and ND). The FCU is the short-term (tactical) interface, and has the following functions: −...
  • Page 47 − Selection of other thrust rating limits (T/L to MCT or CL), − Setting the limit for A/THR authority, by T/L position, − Controlling manual thrust when A/THR is not active, and reverse thrust. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 48 The EFIS Displays: The PFDs and NDs are the visual interface which enables each pilot to continuously monitor status and operation of the FMGS. EFIS Control Panel allows the pilot to select the ND mode, range and navigation features. The Flight Mode Annunciator (FMA) on the PFD indicates: −...

  • Page 49: Flight Phases

    The switching conditions and procedures related to each phase are detailed in Parts II and III of this Guide. The active phase is shown in the title field of the PROG and PERF pages of the MCDU. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 50 FMS GENERAL DESCRIPTION SYSTEM OVERVIEW J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 51 FMS GENERAL DESCRIPTION FMGS OPERATION 1 Part I: Chapter 3 – FMGS OPERATION Contents 3.1. FMS MODES OF OPERATION........3 General ............... 3 DUAL Mode ..............4 SINGLE Mode ............... 5 INDEPENDENT Mode ............. 5 3.2. TEMPORARY FLIGHT PLAN ......... 6 3.3.
  • Page 52 FMS GENERAL DESCRIPTION FMGS OPERATION PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 53: Chapter 3 - Fmgs Operation

    FMS GENERAL DESCRIPTION FMGS OPERATION 3 The Flight Management and Guidance System (FMGS) provides guidance from takeoff, through climb, cruise and descent to approach and landing. It provides the following capabilities: − Pre-flight: definition of the required route and prediction of the optimum profile and speeds.

  • Page 54: Dual Mode

    During operation in DUAL mode, one FMGC is selected as the "master" and the other as the "slave". This ensures that prime navigation functions are synchronized and that guidance commands to A/P, FD, A/THR, are provided by the same source. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 55: Single Mode

    FMS GENERAL DESCRIPTION FMGS OPERATION 5 FMGC1 is the Master except when: − AP2 is engaged singly (normal situation when the RHS pilot is PF). When both APs are engaged for ILS approach, FMGC1 becomes the "master". − FD2 is ON, FD1 is OFF and both APs disengaged.

  • Page 56: Temporary Flight Plan

    The FMS computes track, profile and predictions of the Temporary Flight Plan, according to the entered revisions. This specific Thales feature enables the pilot to visualize revisions on the ND, and thus avoid incorrect entries. Because of this feature, it is not necessary to insert the Temporary Flight Plan after each revision in turn, which would waste time.

  • Page 57: Navigation/Flight Management

    FMS GENERAL DESCRIPTION FMGS OPERATION 7 3.3. NAVIGATION/FLIGHT MANAGEMENT Navigation FMGC position The prime function of the FMGC is to compute an accurate position and ground speed based on the navigation data available. FMGC1 uses IRS1/IRS2/IRS3, GPS1, VOR1/DME1/LOC1/MLS1, FMGC2 uses IRS1/IRS2/IRS3, GPS2, VOR2/DME2/LOC2/MLS2,...
  • Page 58 FMGCs use the triple mix IRS MIX IRS 4337.5N/00123.7E best position to determine, through the IRS1 IRS2 IRS3 filter, the mixed best FMGC position. NAV 1.5 NAV 1.0 NAV 2.2 <FREEZE NAVAIDS> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 59: Radio Navaids

    FMS GENERAL DESCRIPTION FMGS OPERATION 9 EPE (Estimated Position Error) The FMGC position is estimated with 95% probability to be within a probability circle of uncertainty. The ESTIMATED circle radius is shown on the PROGRESS page. By comparison of REQUIRED value with ESTIMATED value, the system determines a HIGH/LOW accuracy level .

  • Page 60: Navigation Information

    DES, V/S or FPA), the FMGC recomputes the predictions based on the selected parameters until the end of current FMS flight phase. Caution Performance computation is based on the performance model stored in the FMS, including the one-engine out performance. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 61: Guidance Modes

    FMS GENERAL DESCRIPTION FMGS OPERATION 11 Guidance modes Guidance modes of the FMGC are of two types: − Managed modes provide guidance computed by the FMGC to follow the flight plan track, profile and/or speed schedule, as programmed in the MCDU. To engage a Managed mode, pilot action is to push the appropriate selector knob on the FCU.

  • Page 62: Speed

    − On MCDU (PERF page), SELECTED mode is confirmed with the target value (which is the reference for FMS computation in the current flight phase). The auto-thrust mode indicated on the FMA does not distinguish between managed and selected Speed/Mach. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 63 FMS GENERAL DESCRIPTION FMGS OPERATION 13 Speed (Cont'd) MANAGED SELECTED J=J=J= ACT MODE UTC DEST EFOB ACT MODE UTC DEST EFOB SELECTED 1544 MANAGED 1541 PRED TO FL070 PRED TO FL070 MANAGED DIST MANAGED DIST 250/.79 250/.79 1420 MCDU SELECTED 250/.40...

  • Page 64: Lateral Guidance

    − On ND flight plan track is displayed by a dashed green line, and actual track by a continuous green line, − On FCU the Heading/Track Window displays the Target Heading (Track). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 65 FMS GENERAL DESCRIPTION FMGS OPERATION 15 Lateral guidance (Cont'd) MANAGED SELECTED J=J=J= P R M = THV001 {} SPD/ALT FISTO 1953 305/ FL294 (T/C) 1955 .79/ FL360 UN874 TRK399° FOUCO 2005 300/ " MCDU UN874 ADABI 2011 " " UN874...

  • Page 66: Vertical Guidance

    PROG page displays the exact value. FMA indications in 2 column from left: − ALT is displayed for an intermediate level-off during climb or descent. − ALT CRZ indicates that altitude matches with the FMS cruise level. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 67 FMS GENERAL DESCRIPTION FMGS OPERATION 17 Vertical guidance (Cont'd) MANAGED SELECTED OP CLB J=J=J=J=J= CLIMB OOMMM= J=J=J=J=J= OOMMM= J=J=J=J=J= DESCENT DESCENT THV001 DESCENT THV001 REC MAX REC MAX ----- ----- FL398 ----- ----- FL398 <REPORT VDEV=+ <REPORT VDEV=- 440 UPDATE AT...

  • Page 68: Software And Database

    FM via the cross-load function available on the A/C STATUS- Software STATUS / XLOAD page. Each database is identified with a reference number that can be checked on the MCDU pages - SOFTWARE/STATUS menu. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 69 GENERAL DISPLAY RULES........14 Non-valid and Missing Data .......... 14 Font size ..............14 Color code ..............15 Data Labels ............... 16 Special symbols or displays .......... 17 Data Entry ..............18 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 70: Chapter 4 - Mcdu

    FMS GENERAL DESCRIPTION MCDU PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 71: Description

    LINE SELECT LINE SELECT KEYS KEYS ATSU KEY MULTI PURPOSE KEY PAGE KEYS ON/OFF AIRPORT KEY BRIGHTNESS ADJUSTMENT KEYS SLEW KEYS FRONT ANNUNCIATOR ALPHA NUMERIC CLEAR KEY KEYS SPACE KEY OVERFLY KEY AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 72: General

    FMS GENERAL DESCRIPTION MCDU GENERAL Information processed by the FMGS is presented on the various pages, which can be displayed on the MCDU screen. The pages are accessed either: − Directly by pressing the PAGE keys, − By pressing the LINE SELECT keys, −...

  • Page 73: Display Screen

    The line select keys are used: − To enter data written in the scratchpad, − To access sub-menu, shown by symbol < or >, − To activate a specific function identified by a prompt *, AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 74 FLT NBR ________ parameters of the planned flight, and LONG ----.-- -----.-- initializing the FM position at the COST INDEX departure point position. WIND> CRZ FL/TEMP TROPO ----- /---° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 75: Data Key

    Data pages can be accessed. <A/C STATUS PRINT FUNCTION> FUNCTION> DATA INDEX 2/2 {} PILOTS <WAYPOINTS WAYPOINTS> PILOTS <NAVAIDS NAVAIDS> PILOTS <RUNWAYS RUNWAYS> PILOTS <ROUTES ROUTES> ACTIVE F-PLN <WINDS SEC F-PLN <WINDS AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 76: F-Pln Key

    The FUEL PRED page displays RTE RSV/% CRZTEMP/TROPO 0.1/ 5.0 -50°/36090 fuel and time predictions based FINAL/TIME on the active flight plan and the 1.0/0030 EXTRA/TIME current gross weight (GW) and 1.4/0040 fuel on board (FOB). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 77: Sec F-Pln Key

    The vertical slew keys are also used to increase or decrease latitude and longitude. Vertical arrows next to these data fields indicate that this data can be modified by using the ↑ and ↓ keys. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 78: Atc Comm Key

    (only before take-off) and back to destination. After take-off, origin is omitted. As on F-PLN A or B page, line 6 displays destination airport with estimated time of arrival, distance to go and EFOB. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 79: Alphanumeric Keys

    The slash key ( / ) is used to separate data when multiple entries are written onto the scratchpad. For example, airspeed and Mach (280/.78), wind direction / velocity / altitude (150/50/200). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 80: Space Key

    If the cleared data field is a leg in the flight plan, the leg is deleted from the flight plan and, in most cases, a discontinuity is created. − Pressing the CLR key will erase CLR from the scratchpad. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 81: On/Off And Brightness Adjustment Keys

    − Important messages are those displayed in amber. − MCDU MENU (white) is illuminated when a system linked to the MCDU other than the FM requests the display (such as ACARS or CFDS). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 82: General Display Rules

    If there are active or selected data displayed with non-active or non- selected data, the active or selected data are displayed in large font while the other are in small font. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 83: Color Code

    Slash (/), when used to separate data fields, are the same color and font as of the data to the right of the /, whether the field contains alphanumeric characters, dashes, boxes. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 84: Data Labels

    (No alternate flight plan). £$ THV001 {} C320° SPD/ALT 3000 ---- ---/ ----- ------END OF F-PLN------ ------NO ALTN F-PLN----- 1930 / FL120 BRG000° FISTO 2256 .79/ FL314 DEST DIST EFOB EGLL27R 0003 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 85: Special Symbols Or Displays

    FMS generated WPT. +, - Associated with ALT constraint. A plus (+) is displayed for an AT or ABOVE ALTITUDE constraint and a minus (-) for an AT or BELOW ALTITUDE constraint. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 86: Data Entry

    Simultaneous data entry in the two MCDUs is not a limitation but should be avoided. Data formats are described in the next chapters and listed in the appendices at the end of the Pilot's Guide. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 87 Part II FLIGHT PHASES PROCEDURES AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 88 PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 89 SWITCHING CONDITIONS ............3 5.2. REACHING CRUISE FLIGHT LEVEL ........4 5.3. NORMAL CRUISE ..............6 5.4. Use of PERF CRZ page ............13 5.5. Use of PROG CRUISE page..........15 5.6. PREPARATION FOR DESCENT AND APPROACH ....17 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 90 RETURN for another approach..........8 8.4. DIVERSION to ALTN Airport ..........10 Chapter 9 – DONE 9.1. SWITCHING CONDITIONS ............3 9.2. FLIGHT DECK INDICATIONS..........3 9.3. SUPPLEMENTARY INFORMATION .........5 9.4. Conditions for Switching to PREFLIGHT PHASE ....8 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 91 FLIGHT PHASES FLIGHT PLAN SCENARIO 1 Part II: Chapter 1 – FLIGHT PLAN SCENARIO Contents 1.1. ROUTE ............... 3 1.2. FLIGHT PLAN DATA............ 4 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 92 FLIGHT PHASES FLIGHT PLAN SCENARIO PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 93 (EGLL/LHR), with alternate airport AMSTERDAM (EHAM/AMS) is used in this guide as a support to describe the different flight phases. REDFA UL620 BPK 6F REDFA EHAM ALESO BIG 3B DIMAL UT426 ABUDA UT191 BAMES UN874 FOUCO FISTO FISTO 5A LFBO AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 94 CONF 2 TOW CG: 26% / TRIM 0.6UP V1 141 VR 141 V2 143 FLEX TEMP :F55 THR RED ALT :1990 FT ACC ALT :3490 FT ENG OUT ACC ALT :1990 FT J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 95 TEMP 15/10 QNH 1015 DEVRO 310/50/M48 FL360 BAMES 320/60/M47 FL360 EHAM: ARRIVAL REDFA DESC WIND 200/15 ILS 18R 320/40 FL300 TEMP 16/12 QNH 1014 300/30 FL200 290/20 FL100 ALTN WIND/TEMP 300/35/M35 FL250 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 96 FLIGHT PHASES FLIGHT PLAN SCENARIO PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 97 FLIGHT PHASES PREFLIGHT 1 Part II: Chapter 2 – PREFLIGHT Contents 2.1. FMGS INITIALIZATION ..........3 FMGC power up/Access ..........4 Check A/C Status page ..........5 Complete INIT A page ........... 6 Enter Route ..............6 Enter Alternate / Alternate Route ........8 Enter Flight Number............
  • Page 98 Take-off with preset HDG: ..........39 MCDU Page selection ...........40 2.4. PROCEDURES DURING TAXI........41 Take-off from intersection or displaced threshold .....41 Change of RWY ............42 CHANGE OF SID ............44 Change RWY/SID with SEC F-PLN........46 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 99: Fmgs Initialization

    For layout of MCDU keyboard (see fold-out at end of the Guide). This chapter describes the normal crew procedures to initialize the FMGS in the preflight phase. In this phase flight data are entered or confirmed via MCDU pages in the following sequence: −...

  • Page 100: Fmgc Power Up/Access

    To access A/C STATUS page: DATA key .......Press A320-211 A/C STATUS [4L]....Press CFM56-5-B4 ACTIVE NAV DATA BASE The A/C STATUS page is displayed. 21JAN-18FEB THV1040101 SECOND NAV DATA BASE {24DEC-21JAN CHG CODE IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 101: Check A/C Status Page

    If some pilot stored data are used in CHG CODE CONFIRM *DELETE ALL the ACTIVE or SEC F-PLN, "PILOT IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> ELEMENT RETAINED" s-pad msg (white) is displayed when DELETE ALL is pressed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 102 ALIGN IRS} FLT NBR LONG $£ ________ ALIGN IRS} 4338.1N 00122.1E LONG $£ COST INDEX 4338.1N 00122.1E WIND> COST INDEX CRZ FL/TEMP TROPO WIND> _____ /___° 36090 CRZ FL/TEMP TROPO _____ /___° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 103 _________ ____/____ amber prompt are described in ALTN/CO RTE INIT ----/---------- REQUEST* Part III: Multiphase Data Link. FLT NBR ________ LONG ----.- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 104: Enter Alternate / Alternate Route

    LONG $£ To change an automatically or 4338.1N 00122.1E COST INDEX manually entered alternate, WIND> overwrite ALTN/CO RTE field in the CRZ FL/TEMP TROPO _____ /___° 36090 same manner as described above. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 105: Enter Flight Number

    ATC INIT flight plan. CO RTE FROM/TO TLSLHR01 LFBO/EGLL ALTN/CO RTE EHAM/LHRAMS01 FLT NBR THV001 ALIGN IRS} LONG $£ 4338.1N 00122.1E COST INDEX WIND> CRZ FL/TEMP TROPO _____ /___° 36090 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 106 When position is correct: INIT CO RTE FROM/TO ALIGN IRS [3R]....Press TLSLHR01 LFBO/EGLL ALTN/CO RTE EHAM/LHRAMS01 FLT NBR THV001 LONG £$ 4338.1N 00122.1E COST INDEX WIND> CRZ FL/TEMP TROPO _____ /___° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 107 <FREEZE NAVAIDS> POSITION MONITOR FMGC1 4338.1N/00122.1E 3IRS/GPS FMGC2 4338.1N/00122.1E 3IRS/GPS GPIRS 4338.1N/00122.1E MIX IRS 4338.1N/00122.1E IRS1 IRS2 IRS3 NAV 0.0 NAV 0.0 NAV 0.0 <FREEZE NAVAIDS> GPS PRIMARY RESET IRS TO NAV AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 108: Enter Cost Index

    THV001 EHAM/LHRAMS01 LONG $£ FLT NBR 4338.1N 00122.1E THV001 COST INDEX LONG $£ WIND> 4338.1N 00122.1E CRZ FL/TEMP TROPO COST INDEX FL360 /-50° 36090 WIND> 35000 CRZ FL/TEMP TROPO FL360 /-50° 35000 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 109: Enter Climb Wind

    Part III: Multiphase – Data Link. FROM THV001 {} FIST5A TIME SPD/ALT LFBO14R ---- ---/ H144° BRG144° ---- ---/ ----- C144° TRK144° D144H} ---- ---/ ----- C356° AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 110: Enter History Wind (When Applicable)

    FLIGHT PHASES PREFLIGHT Enter History Wind (when applicable) The FMGS memorizes the last winds of the previous flight. The HISTORY WIND prompt allows these winds to be inserted for the next flight. In this case: HISTORY WIND [1R]..Press Verify the data.

  • Page 111: Enter Cruise Wind

    CRUISE WIND AT DEVRO WIND TRU WIND/ALT the propagated value. REQUEST 310°/050 AT FL360 PREV PHASE> NEXT WIND PHASE> REQUEST* UPDATE UPDATE PREV {CANCEL INSERT* PHASE> £$ NEXT PHASE> UPDATE UPDATE {CANCEL INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 112: Enter Descent Wind

    [ ]°/[ ] FL310 300°/030/FL200 Insertion of CRZ/DES/ALTN winds WIND 290°/020/FL100 REQUEST* during preflight improves the PREV accuracy of the computed FMGS F- [ ]°/[ ]/[ PHASE> PLN. Otherwise these insertions may UPDATE UPDATE be done in flight. {CANCEL INSERT*...

  • Page 113: Complete F-Pln Page

    Use vertical slew keys when necessary. {AFRI5A {AFRI5H The MCDU display switches to SIDs {AMOL5A pages and changes TITLE FIELD in yellow with TMPY F-PLN at the bottom left. {AMOL5H TMPY EOSID <F-PLN NONE £ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 114: Monitor Nd In Plan Mode

    On ND, the RTE is displayed as a {FINO5H dashed yellow line. FIST5A {FIST5H Due to multiple TMPY F-PLN concept on {GAI5A Thales FM2, it is not required to insert TMPY EOSID TMPY F-PLN until it has been completed <F-PLN NONE £$ and checked.

  • Page 115: Enter En-Route Airways

    AIRWAYS page from FISTO is ------END OF F-PLN------ TMPY TMPY displayed. {ERASE INSERT* £$ LAT REV FROM FISTO 44°27.7N/001°13.6E NEXT WPT <HOLD ENABLE NEW DEST <ALTN AIRWAYS> TMPY <F-PLN AIRWAYS FROM FISTO TMPY <F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 116 DIMAL. ---- ---/ ----- FIST5A BRG144° FISTO ---- ---/ ----- UN874 TRK339° FOUCO ---- ---/ ----- UN874 ADABI ---- ---/ ----- UN874 30NM BOKNO ---- ---/ ----- ONCE THEN {UNDO/ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 117: Enter A Wpt

    ALESO TMPY THV001 {} UT191 TIME SPD/ALT ABUDA ---- ---/ ----- UT426 DIMAL ---- ---/ ----- TRK316° ALESO ---- ---/ ----- ---F-PLN DISCONTINUITY-- EGLL ---- ---/ ONCE THEN TMPY {UNDO/ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 118: Use Airport Key

    TMPY EOSID <F-PLN NONE £$ TMPY THV001 {} C356° TIME SPD/ALT ---- ---/ ----- FIST5A FISTO ---- ---/ ----- ---F-PLN DISCONTINUITY-- EGLL ---- ---/ ------END OF F-PLN------ TMPY TMPY {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 119: Enter Arrival

    THV001 {} BIG3B TIME SPD/ALT intermediate step and select VIA ---- 220/ FL70 if not already selected. C335 BIG07@ ---- ---/ 2500 TMPY F-PLN [6L] ..Press C273° TRK295° CI27R ---- ---/ 2500 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 120: Enter / Revise Alternate Route

    Entry of alternate route may be completed either during Pre-flight phase, or during Cruise phase before descent, at crew’s discretion (see Ch.5 for procedure). The benefit to insert during preflight is to give more accuracy to the FMGS fuel prediction. TMPY F-PLN insert When the entire route is inserted, TMPY F-PLN....Insert...
  • Page 121 £$ See Part III: Multiphase – SEC F- PLN. INIT CO RTE FROM/TO ALTN/CO RTE INIT ----/---------- REQUEST* FLT NBR LONG ----.-- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 122 RADIO NAV SLOPE appropriate. VOR1/FREQ FREQ/VOR2 F144 &TOU/117.70 117.70/TOU ADF1/FREQ FREQ/ADF2 .]/[ (See Part III: Ch 7.2 - RAD NAV ILS /FREQ CHAN/ MLS page). TBS/110.70 [ ]/[ SLOPE F144 ADF1/FREQ FREQ/ADF2 .]/[ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 123 1.0/0030 62.4 EXTRA/TIME 1.4/0038 If a F-PLN & CRZ FL have been entered, the FMGS will now compute time & fuel predictions, including turn radius, lateral and vertical profile. Trajectory is displayed on ND, time and fuel predictions are displayed on F-PLN pages.

  • Page 124: Check & Complete Prog Page

    BRG/DIST TO may be entered with DEST (see Check F-PLN section), or ident of take-off RWY in case of immediate return. If GPS installed: GPS PRIMARY ....Check In any case: ACCUR ......Check See Part III: Ch 7.3 – Position monitoring. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 125: Complete Perf Page

    Enter V1, VR, V2 in their respective fields. Ex:V1 141, VR 141, V2 143. TAKE OFF V1 & VR are displayed on PFD FLP RETR F=150 speed tape, V2 is sent to FMGS for SLT RETR TO SHIFT SRS mode. S=192 [M][ CLEAN...

  • Page 126: Reference Speeds

    The Take-off Shift is used for climb profile computation. If GPS is not available, this take-off shift is taken into account for position update at take-off (See Part I: Ch 3 – Take-off). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 127: Climb Speed

    DEST APPR FLP RETR FINAL F=171 ILS27R TEMP SLT RETR [ ]° S=187 MAG WIND CLEAN [ ]°/[ ] O=210 TRANS ALT LOG CONF 6000 CONF3* VAPP FULL PREV NEXT <PHASE PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 128: Check F-Pln

    WPT on first line of F-PLN page is shown at centre of ND. To change an incorrect AIRWAY or WPT, delete by CLR key. Check and clear any F-PLN DISCONTINUITY as appropriate. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 129 BRG /DIST 352° /476.3 EGLL PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 0.80NM HIGH 0.08NM This field may be then completed by the Departure RWY, to display BRG/DIST in case of immediate return. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 130: Supplementary Procedures

    0000. LFBO14R 0000 141/ An ETT may be entered to enable the H144° BRG144° 0000 153/ FMGS to provide time predictions at C144° TRK144° the destination and at each WPT in D144H} 0002 " / *3130 C356° the F-PLN.

  • Page 131: Change Idle/Perf Factors

    When cleared, IDLE/PERF field becomes green. A320-211 CFM56-5-B4 ACTIVE NAV DATA BASE 21JAN-18FEB THV1040101 SECOND NAV DATA BASE {24DEC-21JAN PILOT STORED 02RTES 00RWYS CHG CODE 00WPTS 00NAVS DELETE ALL} IDLE/PERF SOFTWARE +0.0/+2.0 STATUS/XLOAD> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 132: Data Not Stored In Nav Database

    FMS memory. <ROUTES ROUTES> ACTIVE F-PLN <WINDS Access to Pilot's stored data is from SEC F-PLN DATA INDEX 2/2. <WINDS Insertion of these data is described in Part III: Ch 7.1 Navigation Data. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 133 FMS (WPT, AWY, Navaids) should be A320-211 verified. CFM56-5-B4 ACTIVE NAV DATA BASE Refer to SOPs for applicable procedure. 21JAN-18FEB THV1040101 SECOND NAV DATA BASE {24DEC-21JAN CHG CODE IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 134 1505 250/ FL85 (SPD) (LIM) 1505 *250/ FL100 FIST5A TRK357° FISTO 1514 .79/ FL357 (T/C) 1515 .79/ FL360 UN874 81NM FOUCO 1525 " / " DEST TIME DIST EFOB EGLL27R 1622 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 135: Fcu Selection For Take-Off

    (blue) on heading scale. The F-PLN route becomes dashed green, and blue HDG index is displayed. See Part II: Ch 3 - Take-off. To cancel preset HDG and re- arm NAV, push HDG knob. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 136: Mcdu Page Selection

    ---.-/--.- -50°/35000 FINAL/TIME ---.-/---- EXTRA/TIME ---.-/---- BEFORE ENGINE START FUEL PRED EFOB EGLL 1622 EHAM 1705 65.8 /25.0 7.80/FF+FQ RTE RSV/% CRZTEMP/TROPO 0.2/ 5.0 -50°/35000 FINAL/TIME 1.0/0030 EXTRA/TIME 1.4/0038 AFTER ENGINE START J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 137: Procedures During Taxi

    S=192 If no change, clear message. CLEAN FLAPS/THS O=216 2/UP0.6 TRANS ALT DRT TO-FLX TO 5000 THR RED/ACC ENG OUT ACC 1990/3490 1990 UPLINK NEXT <TO DATA PHASE> CHECK TAKE OFF DATA AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 138 250/ *2820 (SPD) C356° (LIM) 1505 *250/ FL100 1504 " / FL82 TMPY TMPY (SPD) {ERASE INSERT* (LIM) 1505 *250/ FL100 £$ DEST DIST EFOB EGLL27R 1522 CHECK TAKE OFF DATA £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 139 TO SHIFT S=192 [M][ CLEAN FLAPS/THS CONFIRM TO DATA [6R] ..O=216 2/UP0.6 ........Press TRANS ALT DRT TO-FLX TO 5000 THR RED/ACC ENG OUT ACC 1990/1990 1990 UPLINK NEXT <TO DATA PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 140 Scroll up by vertical slew key if TD/108.35 <RETURN required. New SID..... Select/Press Ex: LACO5A. DEPARTURE FROM LFBO TRANS FIST5A NONE SIDS AVAILABLE TRANS {GAI5H {LACO5A {LACO5H {MEN5A EOSID <RETURN NONE £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 141 LACO5A TIME SPD/ALT LFBO14L 1500 141/ H144° BRG144° 1500 153/ C144° TRK146° D144H} 1501 250/ *2820 C356° 1503 " / FL82 (SPD) (LIM) 1504 *250/ FL100 DEST DIST EFOB EGLL27R 1619 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 142 TAKE OFF FLP RETR F=150 SLT RETR TO SHIFT S=192 [M][ CLEAN FLAPS/THS O=216 2/UP0.6 TRANS ALT DRT TO-FLX TO 5000 THR RED/ACC ENG OUT ACC 1990/3490 1990 UPLINK NEXT <TO DATA PHASE> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 143 T/O with a climb speed preselected ......... 7 TAKE-OFF using localizer of OPPOSITE RWY ..... 8 TAKE-OFF with no V2 entry ..........9 3.4. OTHER INFORMATION ..........9 Position update ............9 MAP SHIFT ..............9 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 144 FLIGHT PHASES TAKE-OFF PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 145 FLIGHT PHASES TAKE-OFF 3 3.1. SWITCHING CONDITIONS The FMGS transitions automatically from the PREFLIGHT phase to the TAKE-OFF phase when the following conditions are met: − Thrust levers set to the FLEX or TOGA detent, and, − Left and right N1 > 85% for CFM engines, or, −...
  • Page 146 FCU is at or below the ACC ALT, ALT (blue) will be displayed instead of CLB. ND......... Check The aircraft symbol must be centered on the runway threshold on the ND. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 147 See part II: Climb ALT in magenta is displayed if the level-off altitude is managed by the FMS due to an inserted ALT constraint while the FCU is set at a higher altitude. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 148 RWY T RK FMA. 1FD2 A/THR When appropriate: FCU ......HDG Pull HDG green is displayed on the FMA. 1FD2 A/THR At ACC ALT SRS mode is replaced by OP CLB mode. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 149 ACT MODE UTC DEST EFOB SPEED SEL:XXX is displayed on FMA SELECTED 1100 (line 3, columns 1 & 2). MANAGED *250/.79 PRESEL 220/.66 PREV NEXT 1FD2 <PHASE PHASE> A/THR SPEED SEL:220 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 150: After Take-Off

    LOC information is reversal. ND selected in LS ROSE mode may be preferred. After take-off, NAV mode is 1FD2 automatically engaged. A/THR Select HDG mode and adjust to fly the LOC course. 1FD2 A/THR J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 151: Take-Off With No V2 Entry

    Aircraft with GPS No position update occurs when the thrust levers are set to the FLEX or TOGA detent. MAP SHIFT See Part III: Ch 7.3 - Position monitoring AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 152 FLIGHT PHASES TAKE-OFF PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 153 USE OF PERF CLB PAGE..........22 4.6. USE OF PROG CLIMB PAGE........26 4.7. SCRATCHPAD MESSAGES ......... 28 SPEED ERROR AT XXX ..........28 SPEED LIMIT EXCEEDED ..........28 CHECK GW ..............29 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 154 FLIGHT PHASES CLIMB PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 155: Switching Conditions

    FLIGHT PHASES CLIMB 3 4.1. SWITCHING CONDITIONS The FMGS switches automatically from TAKE-OFF to CLIMB phase: When A/C reaches acceleration altitude (ACC), or, By engagement of another vertical mode. Acceleration altitude (ACC) is shown on TAKE OFF FLP RETR TAKE OFF PERF page [5L]...
  • Page 156 325° /4.7 LFBO14R 325° /4.7 LFBO14R PREDICTIVE PREDICTIVE <GPS GPS PRIMARY <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM 1.00NM HIGH 0.08NM PROG CLB page PROG TAKE OFF page J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 157: Normal Climb

    FLIGHT PHASES CLIMB 5 4.2. NORMAL CLIMB If lateral and vertical managed modes are engaged the FMGS provides guidance to maintain track and profile of ACTIVE F-PLN. On PFD at transition altitude (TRANS ALT), BARO REF flashes, reminding pilot to set STD.

  • Page 158: Speed Control

    ACTIVE F-PLN are taken into account by the FMGS. It is the recommended climb speed mode. If SELECTED speed is engaged, FMGS will maintain speed as selected by pilot on FCU. If a specific speed is required OPM= FCU SPD ....

  • Page 159: To Resume Managed Speed

    EFOB VERT REV AT SPDLIM associated to an airport and EGLL27R 1 $£ stored in the NAV data base CLB SPD LIM (Normally defaulted to 250 KT 250/FL100 up to FL100). <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 160: Lateral Guidance

    (Value depends of A/C orientation to F-PLN track) FCU HDG-TRK ....Push − HDG-TRK window is dashed + J=J=J= dot, − FMA displays NAV green, − A/C returns to track. SPEED 1FD2 A/THR 1FD2 A/THR J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 161 INTCPT is computed. To resume NAV mode: − Manually sequence the ACTIVE F-PLN, − Use DIR TO / DIR TO RADIAL IN functions. See Part III: Ch 3 – Lateral F-PLN management AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 162: Vertical Guidance

    ---° /----.- TO PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM FMGS transitions to CRZ phase only when reaching the CRZ ALT as entered on PROG page. FMA then displays ALT CRZ. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 163: Resuming Climb After Intermediate Level-Off

    III: Multiphase – Vertical functions PTMMM= CLIMB THV001 REC MAX FL370 FL360 FL385 <REPORT UPDATE AT BRG /DIST 123° /1.7 LFBO14R PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM NEW CRZ ALT-37000 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 164: Gps Selection

    GPS selection (A/C equipped with GPS) Reselect GPS as per SOPs if GPS has been deselected for departure (e.g. in case of non WGS84 coordinates). See Part III: Ch 7.3 - Position monitoring J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 165 £$ WIND data WINDS may be inserted or updated at any time manually or by Data Link (if available). The WIND DATA function is described in Part III: Multiphase – Vertical functions. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 166 SPD/ALT the entered constraint. 1945 FL60 (SPD) BRG356° (LIM) 2022 *270/ FL100 TRK339° 2022 " / FL127 (T/C) 2030 270/ FL360 FIST5A FISTO 2030 .79/ " DEST DIST EFOB EGLL27R 2141 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 167 Speed Limit [2R] and ALT constraint at SPD/ALT 1945 FL60 TOU [3R]. (SPD) BRG344° (LIM) 1948 *250/ FL100 TRK339° 1949 305/*FL110 (T/C) 1955 .79/ FL360 FIST5A FISTO 1956 " / " DEST DIST EFOB EGLL27R 2107 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 168 " DEST DIST EFOB EGLL27R 2338 £$ VERT REV AT EFOB=7.0 EXTRA=0.6 CLB SPD LIM UTC CSTR 250/FL100 SPD CSTR ALT CSTR FL110 ALT ERROR -410 ACCESS <WIND DATA STEP ALTS> <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 169 2141 *250/ FL100 TRK339° 2141 305/*FL110 (T/C) 2149 .79/ FL360 FIST5A FISTO 2149 " / " DEST DIST EFOB EGLL27R 2300 £$ Caution Use CLB mode for constraints management as per SOPs. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 170: Supplementary Procedures

    ACT MODE UTC DEST EFOB EXPEDITE 2343 climb mode. PRED TO FL270 MANAGED DIST 305/.79 2227 EXPEDITE 2226 ACTIVATE NEXT {APPR PHASE PHASE> To resume normal climb proceed as described in 4.2. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 171 THV001 REC MAX FL360 FL360 FL386 PSMMM= <REPORT UPDATE AT BRG /DIST 173° /23.6 LFBO14R PREDECTIVE <GPS GPS PRIMARY THR C LB REQUIRED ACCUR ESTIMATED 1FD2 1.00NM HIGH 0.08NM A/THR MACH SEL:.80 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 172 − RAD NAV page (SPD) − PROGRESS page (LIM) 2322 *250/ FL100 TRK000° − PERF page (DECEL) 2329 250/ LFBO 2329 137/ ------END OF F-PLN------ TMPY TMPY {ERASE INSERT* £$ To ARRIVAL pages J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 173 ---F-PLN DISCONTINUITY-- HDG mode, assure F-PLN ---F-PLN DISCONTINUITY-- sequencing, or use DIR TO (T/C) 0008 .79/ FL360 function. 104NM (T/D) 0021 .79/ FL360 See Part III: Multiphase DEST DIST EFOB LFBO14R 0038 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 174 "USING COST INDEX-XXX" ACTIVATE NEXT s-pad msg (white) is displayed, or, {APPR PHASE PHASE> − If TIME CSTR prevails, clear is not allowed and "TIME CSTR EXISTS" s-pad msg (white) is triggered. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 175 1580 TRANS ALT LDG CONF PRESEL 6000 CONF3* MANAGED *[ ] <PH ASE VAPP .79/292 DES CABIN RATE FULL -350FT/MN PREV NEXT PREV NEXT <PHASE PHASE> <PHASE PHASE> PREV NEXT <PHASE PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 176 ACTIVATE APPR PHASE prompt. Reversion to ACTIVATE APPR PHASE prompt also occurs: If actual CLIMB phase transitions to another phase, or in case of FMGC reset, or after a long-term power loss. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 177 FMGCs switch back to current phase. CLIMB THV001 REC MAX FL360 FL360 FL385 Resume normal climb. <REPORT UPDATE AT BRG /DIST 123° /1.7 LFBO14R PREDECTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 178 BRG/DIST with VOR/DME indications. Refer to Part III: Multiphase CLIMB THV001 REC MAX FL360 FL360 FL385 <REPORT UPDATE AT BRG /DIST 123° /1.7 LFBO14R PREDECTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 179 REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM Monitor GPS PRIMARY LOST A/C WITHOUT GPS CLIMB THV001 REC MAX FL360 FL360 FL384 <REPORT UPDATE AT BRG /DIST ---° /----.- TO REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.28NM AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 180: Scratchpad Messages

    270 KT although a SPD LIM 250 KT (LIM) 2207 *270/ FL100 exists below FL100. TRK339° 2207 *270/ FL108 (T/C) 2215 270/ FL360 FIST5A FISTO 2215 .79/ " DEST DIST EFOB EGLL27R 2326 SPD LIM EXCEEDED £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 181: Check Gw

    FUEL PRED page. If actual GW appears to be correct, refer to OPS procedures. FUEL PRED EFOB EGLL 0105 EHAM 0148 64.9 /25.0 6.91/FF+FQ RTE RSV/% CRZTEMP/TROPO 0.1/ 5.0 -50°/35000 FINAL/TIME 1.0/0030 EXTRA/TIME 1.2/0033 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 182 FLIGHT PHASES CLIMB PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 183 Re-pressurization segment........... 22 Enter destination data ..........23 SECONDARY F-PLN ............. 26 Prepare a second Arrival or/and RWY......27 Prepare a circling approach .......... 29 TOO STEEP PATH AHEAD s-pad message ....... 30 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 184 FLIGHT PHASES CRUISE PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 185: Switching Conditions

    FLIGHT PHASES CRUISE 3 5.1. SWITCHING CONDITIONS The FMGS switches automatically from CLIMB to CRUISE phase when A/C reaches the cruise altitude entered on PROG page. FMA ALT CRZ is displayed, MCDU: − PERF page title becomes CRZ green, − PROG page title becomes CRUISE green.

  • Page 186: Reaching Cruise Flight Level

    CRUISE 5.2. REACHING CRUISE FLIGHT LEVEL FMA ........Check ALT CRZ is displayed. If ALT is displayed FMGS is still in CLIMB phase. If the assigned altitude is lower than the CRZ ALT entered in PROG page, the FMGS will not switch to CRUISE phase.
  • Page 187 UTC DES T EFOB SELECTED 1909 FCU SPD/MACH knob..FCU SPD/MACH knob....Push Push (T/D) MANAGED DIST 0000 SELECTED 1847 DES CABIN RATE -350FT/MN ACTIVATE NEXT PHASE PHASE> SET MANAGED SPEED AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 188: Normal Cruise

    − LAT REV is a lateral F-PLN revision made by using MCDU left LSKs. − VERT REV is a vertical F-PLN revision made by using MCDU right LSKs. Refer to Part III: Multiphase for pilot actions not specific to the cruise phase. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 189: Speed Control

    If MANAGED speed is engaged, cruise speed is optimized, constraints and entered speed data in ACTIVE F-PLN are taken into account by the FMGS. If SELECTED speed is engaged, FMGS will maintain speed as selected by pilot on FCU. To change speed K T U= FCU SPD/MACH ..

  • Page 190: Lateral Functions

    Data Link (if available). CLB SPD LIM UTC CSTR 250/FL100 SPD CSTR ALT CSTR These functions are described in Part III: Ch 4 – Vertical F-PLN ACCESS <WIND DATA STEP ALTS> management. <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 191: Change Cruise Level

    CRUISE THV001 NAV. REC MAX FL360 FL361 FL390 If a higher ALT is selected, FMGS <REPORT switches for CRUISE to CLIMB phase UPDATE AT for the time of level change; then BRG /DIST switches again to CRUISE. ---° /----.- TO PREDICTIVE <GPS...

  • Page 192: Flight Monitoring

    .79/ FL360 UN874 TRK016° BOKNO 2046 " / " UN874 DEVRO 2050 " / " UN874 22NM VANAD 2053 " / " DEST DIST EFOB EGLL27R 2137 £$ PNF: F-PLN page A J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 193 For monitoring of position and accuracy see Part III: Ch 7.3 CRUISE THV001 REC MAX FL360 FL360 FL388 <REPORT UPDATE AT BRG /DIST 241° /69.3 LFBD PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 2.0NM HIGH 0.08NM AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 194: Wind Data

    FLIGHT PHASES CRUISE WIND data WINDS may be inserted or updated at any time manually or by Data Link (if available). The WIND DATA function is described in Part III: Ch 4.2. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 195: Use Of Perf Crz Page

    UTC: Estimated time at destination. 0000 SELECTED EFOB: Estimated Fuel On Board at 1535 destination based on ACTIVE F-PLN. DES CABIN RATE -350FT/MN ACTIVATE NEXT CI [2L] {APPR PHASE PHASE> As for CLB page. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 196 ACTIVATE APPR PHASE prompt [6L] ACTIVATE NEXT {APPR PHASE PHASE> As for CLB page. Enables to switch FMGS directly to APPROACH phase: e.g. for diversion. If activated by error, re-enter CRZ A in PROG page. ACT MODE UTC DEST EFOB...

  • Page 197: Use Of Prog Cruise Page

    FL360 FL388 It cannot be cleared, but may be <REPORT modified by a new entry. UPDATE AT Entering a higher ALT switches FMGS to BRG /DIST CLIMB phase. 355° /366.5 EGLL27R To enter a lower ALT distance to DEST PREDICTIVE <GPS...
  • Page 198 See Part II – Descent DIR DEST TO DEST= 170NM REQUIRED ACCUR ESTIMATED 1.0NM HIGH 0.28NM Line 6: ACCURACY This field enables to monitor navigation accuracy. See Part III: Ch 7.3 – Position Monitoring. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 199: Preparation For Descent And Approach

    The MCDU preparation for descent and approach is described here in the following sequence: − F-PLN page A − FUEL PRED page − RAD NAV page − PROG page − PERF page − SEC F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 200: F-Pln Page

    APPROACH VIAS {BIG3A APPR STAR ILS27R BIG3B <RETURN ARRIVAL TO EGLL APPR VIAS £ APPR STAR ILS27R BIG3B APPR TRANS {NO VIA <VIAS NONE STARS AVAILABLE TRANS {WLD3D {NO STAR <RETURN <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 201: Enter/Revise Alternate Route

    137/ *2500 C273° C127R 2048 " / *2500 C273° TRK273° 3-3.0° F127R 2050 " / 1400 C273° 4-3.0° EGLL27R 2052 137/ C273° 1580 ---- ---/ ----- DEST DIST EFOB EGLL27R 2052 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 202: Fuel Pred Page

    ILS/MLS is manually tuned, at less than ADF2 BFO} 100NM track distance from T/D, or, in DES or APPR phase, "CHECK APPR SELECT ION" s-pad msg is triggered on MCDUs and PFD. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 203: Prog Page

    .79/ FL360 UT426 not been inserted on PERF APPR page DIMAL 2300 " / FL308 (CRZ or DES phase only). ALESO 2301 293/ FL286 DEST DIST EFOB EGLL27R 2320 ENTER DEST DATA £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 204: Re-Pressurization Segment

    − Cabin rate of computed descent profile exceeds the maximum cabin rate. Slope of the re-pressurization segment is 4 x cabin rate. CABIN Altitude (Zc) Re-pressurization segment DEST Altitude (Zt) Time (T) J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 205: Enter Destination Data

    SLT RETR 6000 CONF3* [ ]° S=186 VAPP MAG WIND CLEAN FULL [ ]°/[ ] O=210 PREV NEXT TRANS ALT LDG CONF <PHASE PHASE> 6000 CONF3* VAPP FULL PREV NEXT <PHASE PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 206 These speeds are computed by the FMGC and not modifiable. Fields are dashed if not computed. FINAL [1R]: This field is a reminder of the approach selected. It is dashed if no approach has been selected. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 207 PERF GO AROUND page is displayed. F=148 SLT RETR S=186 THR RED/ACC [5L] ....CLEAN ......Check/Modify O=210 ENG OUT ACC [5R] ....THR RED/ACC ENG OUT ACC ......Check/Modify 1580/1580 1580 PREV Logic is identical to take-off <PHASE AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 208: Secondary F-Pln

    See below & Part III: Ch 5 – SEC SEC F-PLN PRINT* F-PLN INIT CO RTE FROM/TO ALTN/CO RTE INIT ----/---------- REQUEST* FLT NBR LONG ----.-- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 209 <VIAS NONE IBB/109.50 APPROACH VIAS STARS AVAILABLE TRANS ILS27L 3658M CRS273 APPR STAR {WLD3D ILL/109.5 ILS27L NONE NONE <RETURN APPR VIAS NO STAR £ {OCK {RICH1 <RETURN NO VIA <RETURN NOT ALLOWED AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 210 STEP ALTS> NEXT PHASE> APPR FLP RETR FINAL 1015 F=148 ILS27L TEMP SLT RETR 15° S=186 MAG WIND CLEAN 250°/15 O=210 TRANS ALT LDG CONF 6000 CONF3* VAPP FULL PREV NEXT <PHASE PHASE> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 211 0122 *250/ FL100 {09R 3658M CRS093 STARS AVAILABLE TRANS TRK000° IBB/109.5 {WLD3D (DECEL) 0128 250/ 1720 <RETURN $£ NO STAR 0128 137/ " 5-3.0° EGLL09L 0130 137/ DEST DIST EFOB <RETURN EGLL09L 0130 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 212: Too Steep Path Ahead S-Pad Message

    5 NM to threshold with a –3° final path. Complete SEC PERF page: Proceed as described in paragraph above. TOO STEEP PATH AHEAD s-pad message See Part II: Ch 6 – Descent J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 213 Use of PERF DES page..........26 6.7. Use of PROG DESCENT page........27 6.8. CROSS REFERENCES ..........28 TOO STEEP PATH AHEAD ..........28 MORE DRAG............... 28 Check APP selection ............ 28 Energy circle .............. 28 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 214 FLIGHT PHASES DESCENT PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 215: Switching Conditions

    FLIGHT PHASES DESCENT 3 6.1. SWITCHING CONDITIONS The FMGS switches automatically from CRUISE to DESCENT phase when: − Reaching TOP of DESCENT (T/D) as computed in ACTIVE F-PLN, or, − A lower ALT is selected on FCU at less than 200 NM to DEST (Early Descent), −...

  • Page 216: Normal Descent

    Descent is initiated, THR IDLE − Thrust decreases to I DLE if no 1FD2 A/THR re-pressurization segment is computed, − FMGS switch t o descent phase, ACT MODE UTC DEST EFOB MANAGED 2230 − Speed t arget is indicated on PERF DES page.

  • Page 217: Selection Of Mcdu Pages

    THV001 {} SPD/ALT 1442 / FL356 BRG331° TIGER 1459 293/*FL154 (SPD) TRK319° (LIM) 1501 *250/ FL100 BIG3B D139L 1501 *250/ FL105 BIG3B 12NM 1504 *220/ 4780 DEST UTC DIST EFOB EGLL27R 1512 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 218: Speed Control

    Speed is optimized; constraints and entered J=J=J= speed data in ACTIVE F-PLN are taken into account by the FMGS. It is the recommended descent speed mode. Target speed is shown by a double magenta line, but to avoid excessive thrust variations, an...

  • Page 219: If A Specific Speed Is Required

    PERF Page shows − SELECTED [1L] with THR I associated value [4L], 1FD2 FMA displays THR IDLE A/THR − or MACH/SPEED if FMGS needs to adjust thrust to maintain profile. ACT MODE UTC DEST EFOB SELECTED 2248 PRED TO FL150...

  • Page 220: Lateral Guidance

    F-PLN constraints are ignored. FCU V/S ....... Adjust FCU ALT......Pull To select OP DES mode. THR I OP DES 1FD2 A/THR To resume NAV mode Proceed as described in climb phase. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 221: Vertical Guidance

    [2R]. Selected vertical modes (OP DES – V/S) The vertical profile is not maintained by the FMGS. In OP DES mode, descent is IDLE thrust maintaining target speed. In V/S mode, thrust is adjusted to maintain target speed; if idle thrust is not enough to assure V/S requested, target speed is not maintained.

  • Page 222: If Hdg-Trk Is Selected

    ) on ND and by predictions on PERF page [2R/3R]. These data are available in both managed and selected. =PfMMM= ACT MODE UTC DEST EFOB MANAGED 1432 PRED TO FL310 MANAGED DIST .79/293 1412 EXPEDITE 1411 ACTIVATE NEXT {APPR PHASE PHASE> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 223: Typical Vertical Profile

    See PART II: Cruise - DES CABIN RATE Cost Index value has a direct influence on T/D position as shown below: INCREASING CI AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 224: Variations

    {APPR PHASE PHASE> − Vertical deviation symbol moves up, − ND: The "broken" blue arrow( shows the intercept point where the FMGS profile will be rejoined, − PROG page indicates VDEV [2R] from computed profile. MACH 1FD2 A/THR...

  • Page 225: Late Descent

    UTC DEST EFOB This message is cleared by the CLR key MANAGED 1903 only if speed is SELECTED, or when (T/D) FMGS transitions to DESCENT phase. MANAGED DIST 1841 Deviation from computed profile is indicated on PROG page VDEV [2R].

  • Page 226: Expedite Descent Function

    ACT MODE UTC DEST EFOB EXPEDITE 1937 PRED TO FL150 MANAGED DIST 305/.79 1918 EXPEDITE 1934 ACTIVATE NEXT {APPR PHASE PHASE> To resume normal descent FCU ALT......Push Or select another appropriate vertical mode. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 227 TRK319° (LIM) 2232 *250/ FL100 BIG3B D139L 2232 *250/ FL105 BIG3B 12NM 2235 *220/ 4780 DEST UTC DIST EFOB EGLL27R 2243 £$ Caution Use DES mode for constraints management as per SOPs. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 228 D139L 0902 *250/ FL106 DES SPD LIM BIG3B 12NM 250/FL100 0905 *220/ *4970 SPD CSTR ALT CSTR DEST DIST EFOB FL150 EGLL27R 0914 ALT ERROR £$ ACCESS <WIND DATA STEP ALTS> <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 229 A/THR target altitude are displayed in magenta. MTMMM= Caution If HDG mode is selected, POM= MTMMM= J==fU DES mode disengages, - FMGS reverts to V/S, - Constraints are ignored. SPEED 1FD2 A/THR AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 230: F-Pln Sequencing

    WPT. The F-PLN will no longer be in sequence with the actual position. Ex: “20 miles before BIG, turn R hdg 350” BIG is by-passed but is still shown as the TO WPT. > 5 Nm J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 231 To sequence the F-PLN, 3 methods can be used: − By clearing each WPT individually, − By collapsing a group of WPTs, − By using the DIR TO or DIR TO RADIAL IN functions. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 232: Clearing Wpts Already Passed Individually

    1553 137/ *2660 C273° 3-3.0° " / FI27R 1554 1400 DEST DIST EFOB EGLL27R 1556 £$ The TO WPT is now correct and the F-PLN is again in sequence with actual position. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 233: Collapsing A Group Of Wpts

    BIG3B BRG318° (DECEL) 1517 250/ 2660 BIG3B TRK318° CI27R 1519 137/ *2660 EGLL C273° 3-3.0° FI27R " / FI27R 1521 1400 C273° 4-3.0° EGLL27R & 1523 137/ TMPY TMPY {ERASE INSRT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 234: Use Of Dir To Radial In Function

    FI27R to CI27R (093°) which is th F-PLN WPTS {BIG DIRECT TO final approach course WITH {BIG07 ABEAM PTS } RADIAL IN {CI27R 093° } RADIAL OUT FI27R [ ]° DIR TO DIR TO {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 235 − "ADJUST DESIRED HDG/TRK" s- EGLL27R&0912 137/ C273° pad msg (amber) appears as a 1580 ---- ---/---- reminder to set the correct DEST DIST EFOB EGLL27R 0912 intercept HDG. ADJUST DESIRED HDG/TRK£$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 236 See Part III: Multiphase - DIR TO function. Note: Use of DIR TO function, without RADIAL IN, to clear unwanted WPTs, causes immediate engagement of NAV mode. It should therefore only be used if there is no heading restriction. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 237: Sec F-Pln Activation

    In the example below, SEC F-PLN is no longer in sequence with ACTIVE from DIVERSION POINT. See Part III: Multiphase SEC F-PLN SEC F-PLN ACTIVE F-PLN DIVERSION POINT PREVIOUS ACTIVE F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 238: Use Of Perf Des Page

    When clear, [2R] field defaults to FCU selected ALT. ACTIVATE APPR PHASE prompt [6L]: Same rule applies as described for CLB & CRZ pages. Enables to switch FMGS directly to APPROACH phase in case and anticipate deceleration for approach. See also Part II: Approach NEXT PHASE prompt [6R]: Enables access to APPR &...

  • Page 239: Use Of Prog Descent Page

    ----- FL393 transitioning to DESCENT phase, − Entering a value in CRZ field switches <REPORT VDEV=- UPDATE AT the FMGS in CRUISE phase, BRG /DIST − REC MAX. 310° /49.3 EGLL27R PREDICTIVE See Part II – CH 5 Cruise <GPS...

  • Page 240: Cross References

    100NM track distance from T/D, or, in DES or APPR phase, "CHECK APPR SELECTION" message is triggered on both MCDU and PFD. Energy circle See to Part II: Ch 7 – Approach. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 241 Circling ..............21 NAV ACCUR DOWNGRAD ..........24 Final approach speed ..........25 7.5. SUPPLEMENTARY PROCEDURES ....... 26 Change RWY .............. 26 Using SEC F-PLN ............26 By revision in ACTIVE F-PLN......... 28 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 242 FLIGHT PHASES APPROACH PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 243: Switching Conditions

    FLIGHT PHASES APPROACH 3 7.1. SWITCHING CONDITIONS The FMGS is designed to switch automatically from DESCENT to APPROACH phase, on passing the DECEL pseudo-waypoint. It may also be switched manually to APPROACH phase by using ACTIVATE APPROACH function from any PERF pages except TO and APPR.
  • Page 244 15° S=186 MANAGED DIST MAG WIND CLEAN .44/250 1351 250°/15 O=209 TRANS ALT LOG CONF 6000 CONF3* VAPP EXPEDITE 1427 FULL ACTIVATE NEXT NEXT {APPR PHASE PHASE> PHASE> PERF DES PERF APPR J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 245: Before Approach Activation

    293° /16.7 EGLL27R − REQD DIST TO LAND, REQD DIST TO LAND= 12NM DIR DIST TO DEST= 161NM − DIR DIST TO DEST. REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.28NM A/C without GPS AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 246: Nav Accuracy Check

    HIGH. If accuracy is evaluated LOW, refer to SOPs, consider Raw data, EGPWS deactivation and selected modes should be used. Predictive GPS Refer to Part III: Multiphase – Position monitoring. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 247: F-Pln Sequencing

    137/ *2500 − Missed approach routing & altitudes, C273° 3-3.0° FI27R 1930 " / 1400 − Distance to landing, along F-PLN DEST DIST EFOB track, EGLL27R 1932 £$ − TO WPT is correct. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 248: Approach Activation

    DECEL pseudo-waypoint is displayed by a symbol (magenta). If Speed and/or Lateral mode is selected: symbol is not normally displayed; if DECEL 2 option is selected (OPC file), it is displayed in white. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 249: Manual Activation

    − If actual phase transitions to TRANS ALT LOG CONF 6000 CONF3* another phase, or VAPP FULL − In case of FMGC reset, or NEXT PHASE> − After a prolonged power loss. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 250: Speed Control

    TRANS FL LOG CONF FL60 CONF3* VAPP FULL NEXT PHASE> If speed is selected: − FCU SPD window is open with selected speed, − Target speed is blue, − VAPP is not displayed. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 251: Approach Management

    PROG <REPORT VDEV= page, magenta circle is no UPDATE AT longer displayed on PFD. BRG /DIST 333° /7.7 EGLL27R PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 0.3NM HIGH 0.08NM AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 252: Trajectory Deviation Symbol

    APP NAV 1FD2 displayed when APPR mode is A/THR armed or engaged. Otherwise vertical deviation (magenta circle) is displayed SPEED APP NAV FINAL 1FD2 with logics described above. A/THR SPEED FINAL 1FD2 A/THR J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 253: Ils Or Mls

    − ILS APP is displayed at top of screen, − Final descent is shown by arrow, − Final track, distance to threshold are displayed, − Actual wind is shown and may be correlated with VAPP variation (ground speed mini function). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 254 Changes to data on PERF APPR page (wind, config, or Vapp) are not accepted by the FMGC, when speed is managed. Caution APPR mode disengages if DIR TO is selected. Modes revert to NAV – V/S. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 255: Npa (Non Precision Approach)

    FLP RETR FINAL 5000 CONF3* 1018 F=171 VOR14R VAPP TEMP SLT RETR FULL 18° S=191 NEXT MAG WIND CLEAN PHASE> 140°/10 O=215 TRANS FL LOG CONF FL60 CONF3* VAPP FULL NEXT PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 256 HDG/TRK and vertical guidance through V/S-FPA mode, − Managed guidance modes: lateral and vertical guidance are controlled by FMGS through FINAL APP mode, − Managed lateral / Selected vertical guidance modes: lateral guidance is controlled by FMS via NAV mode, vertical guidance is controlled by pilot via V/S-FPA mode.
  • Page 257 140°/10 O=215 TRANS ALT LOG CONF 5000 CONF3* VERT REV AT FD14R VAPP EFOB=7.1 EXTRA=5.9 FULL NEXT DES SPD LIM PHASE> 250/FL100 SPD CSTR ALT CSTR ACCESS <WIND DATA STEP ALTS> <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 258 C145 LATERAL MANAGED MD105{ ---- ---/ *900 VERTICAL SELECTED C018° 11NM INTCPT ---- ---/ ----- DEST DIST EFOB LFBO14R 2111 £$ PROG page VDEV is displayed in [2R]. LATERAL SELECTED VERTICAL SELECTED J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 259 PROG page VDEV is displayed in [2R]. APPROACH THV001 REC MAX ----- ----- FL397 <REPORT VDEV=+ UPDATE AT BRG /DIST 145° /7.3 LFBO14R LATERAL SELECTED REQUIRED ACCUR ESTIMATED VERTICAL SELECTED 0.50NM HIGH 0.28NM AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 260 (XTK) are displayed, − Actual wind is shown and may be correlated to VAPP variation, − Energy circle is available when HDG/TRK is selected and may be information if accuracy is high. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 261: Circling

    {DELETE SEC *ACTIVATE SEC SEC F-PLN PRINT FROM THV001 {} SPD/ALT PPOS 1751 FL58 ---F-PLN DISCONTINUITY-- 1756 129/ 1580 5-3.0° EGLL09L &1758 129/ ------END OF F-PLN------ DEST DIST EFOB EGLL09L 1758 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 262 ---- ----- A/C position may be visualized relative to RWY (if accuracy is high). MCDU: Established on final managed speed is available, VAPP is based on landing data as shown on PERF page. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 263 RWY has not been entered, and thus ND does not provide position awareness relative to RWY. There is no input data for Ground Speed Mini protection on landing RWY, selected SPD must be used. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 264: Nav Accur Downgrad

    REQD DIST TO LAND= 12NM DIR DIST TO DEST= 16NM situation may require reversion to REQUIRED ACCUR ESTIMATED selected modes and use of raw data. 0.5NM 0.60NM NAV ACCUR DOWNGRAD Final approach J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 265: Final Approach Speed

    TEMP SLT RETR 15° S=176 wind inserted in [3L] and varies MAG WIND CLEAN according to Ground Speed Mini 230°/15 O=196 TRANS ALT LDG CONF protection. 6000 CONF3* VAPP FULL NEXT PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 266 WPT in line 2. TRK289° (DECEL) 2340 250/ 2380 See F-PLN sequencing in Part II: Descent CI27L 2341 137/ *2380 C273° 3-3.0° FI27L 2343 " / 1400 DEST DIST EFOB EGLL27L 2329 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 267 Select as required. 2336 4780 C335 BRG334° BIG07 & 2340 250/ *2620 TRK289° (DECEL) 2340 250/ 2380 CI27L 2342 137/ *2380 C273° 3-3.0° FI27L 2344 " / 1400 DEST DIST EFOB EGLL27L 2345 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 268 STAR ILS27L BIG3B APPR TRANS <VIAS NONE STARS AVAILABLE TRANS {WLD3D NO VIA ....Select/Press {NO STAR TMPY <F-PLN APPROACH VIAS APPR STAR ILS27L NONE APPR VIAS {OCK {RICH1 {NO VIA <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 269 If A/C is not on correct HDG: HDG/TRK ..Select/Adjust Otherwise "SELECT HDG/TRK FIRST" s-pad msg (white) is triggered. If APP modes already armed or engaged, they revert to HDG – V/S. APP mode......Select Select as required. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 270 FLIGHT PHASES APPROACH PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 271 At ACC ALT ..............7 8.3. RETURN for another approach ........8 8.4. DIVERSION to ALTN Airport........10 ENABLE ALTN function..........10 Using SEC F-PLN ............13 Diversion not prepared ..........13 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 272 FLIGHT PHASES GO-AROUND PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 273: Switching Conditions

    FLIGHT PHASES GO-AROUND 3 8.1. SWITCHING CONDITIONS The FMGS is designed to switch automatically from APPROACH to GO- AROUND phase when all the following conditions are met: − A/C in flight, − Slats extended, − Thrust levers set to TOGA detent.

  • Page 274: Standard Go-Around

    In SRS mode, vertical guidance is not managed. The initial altitude constraint of the missed approach procedure must be set on FCU after passing FAF on the approach. If a constraint exists: "CSTR DEL UP TO XXXX" s-pad msg (white) is triggered. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 275 C320° 3000 ---- ---/ ----- THR RED/ACC ENG OUT ACC 1580/1580 1580 ---F-PLN DISCONTINUITY-- ACTIVATE NEXT DEST DIST EFOB {APPR PHASE PHASE> EGLL27R ---- 26 ----- CSTR DEL UP TO EGLL27R £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 276: Lateral Guidance

    ENG OUT ACC 1580/1580 1580 − A/THR becomes active in THR CLB ACTIVATE NEXT mode, {APPR PHASE PHASE> − FMA displays THR CLB. TOGA 1FD2 LVR CLB A/THR THR C LB 1FD2 A/THR J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 277: At Acc Alt

    FCU, − If speed is managed, speed increases to Green Dot, shown (magenta) at top of PFD speed scale, − Select configuration as per SOPs. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 278: Return For Another Approach

    TEMP SLT RETR THR RED/ACC ENG OUT ACC 15° S=186 1580/1580 1580 MAG WIND CLEAN CONFIRM NEXT 240°/12 O=208 *APPR PHASE PHASE> TRANS ALT LDG CONF 6000 CONF3* VAPP FULL NEXT PHASE> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 279 FROM THV001 {} SPD/ALT EGLL27R&---- / ----- C273° BRG274° 1580 ---- ---/ ----- C320° TRK320° 3000 ---- ---/ ----- ---- ---/ ----- ---F-PLN DISCONTINUITY-- DEST DIST EFOB EGLL27R ---- 34 ----- £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 280: Diversion To Altn Airport

    SPD/ALT EHAM18R ---- ---/ EHA184 390 } ---- ---/ ----- C325° INTCP ---- ---/ ----- C184° EH624 ---- ---/ 2000 ---END OF ALTN F-PLN---- DEST DIST EFOB EGLL27R ---- 26 ----- £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 281 ND shows ALTN route (dashed ---F-PLN DISCONTINUITY-- yellow) departing from its origin, EGLL ---- / ----- EGLL. TRK042° ---- ---/ ----- ---- ---/ ----- UL620 26NM DIDGO ---- ---/ ----- TMPY TMPY {ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 282 BRG /DIST {APPR PHASE PHASE> 93° /3.0 EGLL27R PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM Sequence the ACTIVE F-PLN according to ATC clearance using for example the DIR-TO function. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 283: Using Sec F-Pln

    THV001 {} Enter WPT, revise as desired. SPD/ALT 1580 ---- / ----- C320° BRG320° 3000 ---- ---/ ----- TRK017° ---- ---/ ----- ---F-PLN DISCONTINUITY-- EGCC ---- ---/ TMPY TMPY {ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 284 GPS PRIMARY REQUIRED ACCUR ESTIMATED 2.0NM HIGH 0.08NM F-PLN page: Enter / modify route as desired. Caution If actual DEST is entered in NEW DEST, A/C will remain in GO AROUND phase. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 285 PILOTS ROUTES: ............4 9.3. SUPPLEMENTARY INFORMATION ....... 5 Use of FMS during Base Training........5 Touch-and-go landings ..........5 Full-stop landing............6 SIMSOFT ..............7 9.4. Conditions for Switching to PREFLIGHT PHASE..8 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 286 FLIGHT PHASES DONE PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 287: Switching Conditions

    GPS PRIMARY <GPS REQUIRED ACCUR ESTIMATED REQUIRED ACCUR ESTIMATED 1.00NM HIGH 0.08NM 0.00NM 17.0NM A320-200 CFM56-5-B4 ACTIVE NAV DATA BASE 21JAN-18FEB JEP3040101 SECOND NAV DATA BASE {24DEC-21JAN CHG CODE IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 288: Mcdu Display

    FUNCTION> PILOTS ROUTES: IRS MONITOR Pilot stored routes are either deleted DRIFT AT EGLL27R or retained, depending on option <IRS1 DRIFT 0.5NM/H selected in AMI file. <IRS2 DRIFT 1.5NM/H <IRS3 DRIFT 2.5NM/H J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 289: Supplementary Information

    1557 3000 BRG359° BASE14 1659 132/ 3000 TRK230° CI14R 1702 " / " C144° 5-3.0° FI14R 1704 " / 1760 C144° 4-3.0° LFBO14R 1705 132/ DEST DIST EFOB LFBO14R 1705 14.5 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 290 SEC F-PLN PRINT* LONG 4338.1N 00122.1E COST INDEX WIND> CRZ FL/TEMP TROPO FL020 / 11° 36090 If SEC INIT B page and SEC PERF pages are not completed, managed modes are not available. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 291: Simsoft

    SEC F-PLN may be also available in case of lost in flight after a touch and go. SIMSOFT The FMS contains special features for use in the simulators. These features enable FMS Simulator synchronization during repositioning. Refer to Simulator User manuals. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 292: Conditions For Switching To Preflight Phase

    − PERF key pressed, − an ACTIVE F-PLN initialized by ACTIVATE SECONDARY function, − an ACTIVE F-PLN initialized by an AOC uplink. DONE phase is not switched if WPTs are inserted in F-PLN page. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 293 Part III MULTI PHASE PROCEDURES AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 294 PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 295 5.3. ND display ..............7 5.4. Use of SEC F-PLN ............8 Chapter 6 - FUEL monitoring 6.1. Overview ..............3 6.2. FUEL PRED page ............3 6.3. F-PLN page B ..............7 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 296 9.4. WIND DATA ..............29 9.5. FLIGHT REPORTS messages.........40 9.6. DATA LINK SCRATCHPAD MESSAGES ......45 Chapter 10 - PRINT FUNCTION 10.1. OVERVIEW ..............3 10.2. MCDU ACCESS AND DESCRIPTION .........4 10.3. REPORT PRINT-OUT ............9 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 297 Part III: Chapter 1 – MCDU MENU PAGE Contents 1.1. GENERAL ..............3 1.2. MCDU DISPLAY ............4 Selection of a subsystem ..........4 FMGC (REQ) ..............6 FMGC (TIME OUT)............6 FMGC (OWN) ............... 6 FMGC (OPP)..............6 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 298 MULTIPHASE MCDU MENU PAGE PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 299 This page is normally used to access to subsystems other than FMGC. In normal operation access to FMGC pages is made via the FM page keys. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 300: Mcdu Display

    RETURN> WAIT FOR SYSTEM RESPONSE A320-211 CFM56-5-B4 ACTIVE NAV DATA BASE 21JAN-18FEB THV1040101 SECOND NAV DATA BASE {24DEC-21JAN PILOT STORED 03RTES 00RWYS CHG CODE 00WPTS 00NAVS DELETE ALL} IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 301 1.0NM HIGH 0.28NM If communication fails, The display reverts to the MCDU MENU MCDU MENU page "SYSTEM NOT AVAILABLE" s-pad <FMGC msg (white) is triggered. <ACARS <AIDS <CFDS RETURN> SYSTEM NOT AVAILABLE AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 302: Fmgc (Req)

    "(REQ)" <AIDS indicator is inserted after the <CFDS (REQ) subsystem name. RETURN> SELECT DESIRED SYSTEM FMGC (TIME OUT) FMGC (OWN) FMGC (OPP) These labels are described in Part IV: FMS degraded operations. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 303 MULTIPHASE F-PLN pages 1 Part III: Chapter 2 - F-PLN pages Contents 2.1. Overview ..............3 General ............... 3 LAT REV ..............6 VERT REV ..............8 2.2. TMPY F-PLN ............. 10 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 304 MULTIPHASE F-PLN pages PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 305 Purpose of F-PLN page B is to display the flight plan with wind, distance and estimated fuel on board. For alternate flight plan and non-active missed approach, no EFOB is available, winds and F-PLN distances are displayed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 306 BRG015° BOKNO 1536 " / " UN874 TRK007° DEVRO 1540 " / " UN874 VANAD 1543 " / " UN874 45NM VADOM 1549 " / " DEST DIST EFOB EGLL27R 1625 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 307 If data is insufficient for predictions to run, the destination data is dashed. WPTS abbreviations, F-PLN markers, Lateral defining legs on F-PLN page are listed in Part V: Appendices – Ch.2 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 308 When a LAT REV at a F-PLN LAT REV FROM DISCON DISCONTINUITY is selected, NEXT WPT ARRIVAL> [3R] and NEW DEST [4R] are only available. NEXT WPT NEXT DEW Lateral functions are described in Ch 3. <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 309 LAT REV FROM EGLL27R VERT REV AT EGLL27R 51°28.7N/000°26.0W EFOB=4.4 EXTRA= ARRIVALS> DES SPD LIM UTC CSTR 250/FL100 NEXT WPT G/S INTCPT <ALTN ENABLE {ALTN ACCESS <WIND DATA STEP ALTS> <RETURN <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 310 − UTC CSTR [2R] enable to enter time constraint at DEST airport, − Access to WIND DATA function via [5L], − Access to STEP ALTS page via [5R]. Vertical functions are described in Ch 4. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 311 LAT REV FROM EGLL27R VERT REV AT EGLL27R 51°28.7N/000°26.0W EFOB=3.9 EXTRA= ARRIVALS> DES SPD LIM UTC CSTR 250/FL100 NEXT WPT G/S INTCPT <ALTN ENABLE {ALTN ACCESS <WIND DATA STEP ALTS> <RETURN <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 312 2.2. TMPY F-PLN When any revision is made to the ACTIVE F-PLN, a Temporary Flight Plan (TMPY) is created while FMGS continues to provide guidance on ACTIVE F-PLN references. TMPY F-PLN is displayed in yellow on MCDU and by a dashed yellow line on ND.
  • Page 313 INSERT* £$ FROM TMPY THV001 {} SPD/ALT 1522 / FL356 BRG333° TIGER 1533 293/*FL154 TRK328° TUNBY 1534 " / FL117 ---F-PLN DISCONTINUITY-- (SPD) (LIM) 1535 *250/ FL100 TMPY TMPY {ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 314 BIG3 SPD/ALT 2201 250/ 5140 (DECEL) 2202 250/ 4620 TRK334° BIG80 2203 137/ " C273° ILL75 2206 " / *2660 C273° 3-3.0° ILL4 2207 " / 1390 TMPY TMPY {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 315 C335 BIG07@ 2210 137/ *2500 C273° CI27R 2213 " / *2500 DIR TO DIR TO {ERASE INSERT* DIR TO IN PROCESS £$ Examples of TMPY F-PLN are given through out this manual AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 316 MULTIPHASE F-PLN pages PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 317 Lateral Guidance ............34 Notes................ 34 DIR TO RADIAL IN / RADIAL OUT functions ....35 DIR TO RADIAL IN ............35 DIR TO RADIAL OUT ........... 37 Lateral guidance ............39 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 318 Without ALTN in NAVdb ..........62 With ALTN in NAVdb ............65 ENABLE ALTN function ..........69 With ALTN RTE entered in ACTIVE F-PLN ......70 Without ALTN RTE entered in ACTIVE F-PLN ....72 ALTN F-PLN cruise altitude..........72 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 319: Lateral Revisions

    {UNDO/ERASE INSERT* £$ TMPY THV001 {} SPD/ALT 1540 .79/ FL360 1445 " / " ---F-PLN DISCONTINUITY-- BOKNO 1454 .79/ " UN874 27NM DEVRO 1557 " / " ONCE THEN {UNDO/ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 320 " / " UT191 52NM ABUDA 1604 " / " DEST DIST EFOB EGLL27R 1625 £$ Another method could be clearing all unwanted WPTs individually and last by clearing the F-PLN DISCONTINUITY. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 321: Change To Wpt

    TMPY {ERASE INSERT* SELECT HDG/TRK FIRST £$ FROM THV001 {} SPD/ALT PPOS 1522 / FL360 ---F-PLN DISCONTINUITY-- 1540 .79/ FL360 ---F-PLN DISCONTINUITY-- ADABI 1548 .79/ " DEST DIST EFOB EGLL27R 1625 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 322: Delete Wpt(S)

    / FL360 BRG356° ADABI 1534 .79/ FL360 TRK017° 123 VADOM 1550 " / " UN874 27NM BAMES 1604 " / " UN874 17NM PODEM 1606 " / " TMPY TMPY {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 323 BRG356° ADABI 1532 .79/ FL360 UN874 TRK016° 150 BAMES 1536 " / " UT191 PODEM 1540 " / " UT191 52NM ABUDA 1543 " / " DEST DIST EFOB EGLL27R 1625 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 324: Overfly A Wpt (Ovfy)

    " / " TRK330° (T/D) 1604 .79/ FL360 UT426 DIMAL 1606 " / FL308 ALESO 1607 293/ FL286 DEST DIST EFOB EGLL27R 1625 £$ OVFLY symbol at the TO WPT is shown white. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 325: Next Wpt

    1540 " / " UT191 52NM ABUDA 1543 " / " If the entered WPT is not part of the DEST DIST EFOB EGLL27R 1625 ACTIVE F-PLN, a discontinuity is £$ created. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 326: Airways

    "AWY/WPT MISMATCH" s-pad msg (white) is triggered. ND should be used with appropriate mode/range to check entered AIRWAYS FROM FOUCO revisions. <RETURN AWY/WPT MISMATCH UT158 AIRWAYS FROM FOUCO UT209 <RETURN AWY/WPT MISMATCH J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 327 " UT158 TRK015° 1529 " / " UN859 VANAD 1533 " / " 45NM VADOM 1543 " / " ONCE THEN TMPY {UNDO/ERASE INSERT* £$ If correct. TMPY INSERT [6R] ..Press AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 328: New Dest

    1552 *250/ FL100 TMPY TMPY {ERASE INSERT* £$ FROM TMPY THV001 {} SPD/ALT ---F-PLN DISCOBTINUITY-- (SPD) (LIM) 1552 *250/ FL100 (DECEL) 1600 250/ LFBD 1600 137/ ------END OF F-PLN------ TMPY TMPY {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 329: F-Pln Sequencing

    / FL358 BRG356° ADABI 1532 .79/ FL360 UN874 TRK016° BOKNO 1536 " / " UN874 DEVRO 1540 " / " UN874 22NM VANAD 1543 " / " DEST DIST EFOB EGLL27R 1625 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 330 INTCPT waypoint is computed; otherwise "SELECT HDG TRK FIRST" s-pad msg would be triggered. TO WPT displayed on ND (top right) and on F-PLN page (white color) should be monitored. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 331: Stringing Rules

    Search downstream Example 1 in F-PLN-route SID RWY SID En-route TRANS En-route TRANS First point of En-route Search downstream in F-PLN-route Example 2 F-PLN DISCONTINUITY SID RWY En-route TRANS SID En-route TRANS AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 332 " / " UN874 62NM UN874 FOUCO 1525 " / " ADABI 1531 " / " TMPY TMPY UN874 30NM {ERASE INSERT* BOKNO 1535 .79/ FL322 FOUCO ONCE THEN TMPY {UNDO/ERASE INSERT* J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 333: Change Selected Sid (With Or Without Rwy Change)

    WPT of the new SID and start of en-route segment (Example 4). Example 4 First point of En-route in F-PLN-route Revise point Before change SID En-route TRANS En-route TRANS F-PLN DISCONTINUITY After change SID En-route TRANS TRANS En-route AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 334: Route

    (Ex.2-2) is not in F-PLN, the last entered WPT is strung with the WPT following the revised WPT by a F-PLN discontinuity. Entered WPT Example 2-1 Revise WPT F-PLN DISCONTINUITY Entered WPT Revised segment Example 2-2 F-PLN DISCONTINUITY Revise WPT J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 335: Manual Legs

    UN874 BRG023° BOKNO 1536 .79/ FL360 UN874 TRK007° DEVRO 1540 " / " UN874 VANAD 1543 " / " UN874 45NM VADOM 1549 " / " DEST DIST EFOB EGLL27R 1625 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 336: At Arrival

    If RWY is selected with no STAR approach is defined as a leg starting 5 NM on RWY axis. Picture below shows scheme for waypoint matching. Last point of En-route Search upstream in F-PLN-route Search upstream Search downstream Approach TRANS (VIA) En-route STAR STAR APPROACH En-routeTRANS J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 337: Changes During Arrival

    Ex: A change for RWY 27L during arrival at EGLL If changes are made before starting STAR: All WPTs are strung. No action is required. FI27L CI27L BIG07 RWY 27L D139L TIGER DIMAL BIG3B ALESO AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 338 TMPY THV001 {} SPD/ALT TIGER 1615 293/*FL150 (SPD) (LIM) 1616 *250/ FL100 BIG3B TRK319° D139L 1616 *250/ FL100 BIG3A 1617 *220/ *4850 (DECEL) 1618 220/ 2500 ONCE THEN TMPY {UNDO/ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 339 ALESO; En-route ends is now BIG. Selection of the new arrival is re-strung from BIG; a discontinuity exists between BIG and ALESO, start of arrival procedure. FI27L CI27L BIG07 RWY 27L D139L TIGER BIG3B F-PLN DISCONTINUITY ALESO AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 340 " / 1400 ONCE THEN TMPY {UNDO/ERASE INSERT* £$ In any case, to string the F-PLN, write and enter the desired WPT after the TO WPT, which collapse the unwanted WPT(s) or segment. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 341: Incorrect Lateral Trajectory

    Managed speed may be re-selected when the correct target speed is shown on PRF CRZ page (delay may be approx. 10 seconds). Refer to Operator's manual and/or Airbus OEB for more details. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 342: Dir To Function

    " UN874 TMPY F-PLN, “DIR TO IN PROCESS” BAMES 1553 " / " UT191 17NM s-pad msg (white) is triggered. PODEM 1555 " / " DIR TO DIR TO {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 343 2. Dir To Intercept To: proceed direct to intercept a Radial TO a reference fix (RADIAL IN function), 3. Dir To Intercept From: proceed direct to intercept a Radial FROM a reference fix (RADIAL OUT function). (RADIAL IN) (RADIAL OUT) AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 344: Abeam Pts / Direct To Functions

    ACTIVE F-PLN. Abeam WPTs are named ABxxxxx, xxxxx representing the first five characters of the relative WPTs. Ex: ABADAIB, ABBOKNO, ABDEVRO Check DIR TO track (dashed yellow) is correct on ND. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 345 ABDEVRO 1553 " / " UN874 27NM UN874 21NM BAMES 1555 " / " VANAD 1557 " / " DIR TO DIR TO DEST DIST EFOB {ERASE INSERT* EGLL27R 1625 £$ £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 346 DIR TO WAYPOINT DIST VANAD 1543 F-PLN WPTS {BOKNO DIRECT TO WITH {DEVRO ABEAM PTS } RADIAL IN VANAD 200° } RADIAL OUT {VADOM [ ]° DIR TO DIR TO {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 347 BAMES 1546 " / " UT191 17NM UT191 17NM PODEM 1549 " / " PODEM 1549 " / " DIR TO DIR TO DEST DIST EFOB {ERASE INSERT* EGLL27R 1625 £$ £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 348: If Wpt Is Not In Active F-Pln

    DIR TO WAYPOINT DIST 1540 F-PLN WPTS {BOKNO DIRECT TO } WITH {DEVRO ABEAM PTS RADIAL IN {VANAD [ ]° RADIAL OUT {VADOM [ ]° DIR TO DIR TO {ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 349 " / " ABBOKNO 1535 " / " 1539 " / " --F-PLN DISCONTINUITY--- DEVRO 1542 .79/ " --F-PLN DISCONTINUITY--- DIR TO DIR TO DEST DIST EFOB {ERASE INSERT* EGLL27R 1625 £$ £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 350: Lateral Guidance

    STEP ALT point as defined in original F-PLN remains at ABEAM WPT. WIND data for original WPTs are tranferred to ABM WPTs if it is less than 100 Nm from original WPTs; otherwise, no wind data is assumed. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 351: Dir To Radial In / Radial Out Functions

    DIR TO WAYPOINT DIST 1540 F-PLN WPTS {BOKNO DIRECT TO } WITH {DEVRO ABEAM PTS } RADIAL IN {VANAD 185° RADIAL OUT {VADOM [ ]° DIR TO DIR TO {ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 352 − TO WPT is the selected DIR TO WPT. In the example, since AMB is not in ACTIVE F-PLN, it is followed by a F-PLN DISCONTINUITY. See below for Lateral Guidance and INTCPT computation. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 353: Dir To Radial Out

    £$ DIR TO WAYPOINT DIST 1540 F-PLN WPTS {BOKNO DIRECT TO } WITH {DEVRO ABEAM PTS RADIAL IN {VANAD [ ]° RADIAL OUT {VADOM 045° DIR TO DIR TO {ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 354 − Distance to INTCPT point is shown on ND beside actual position, in place of cross-track error. When established on the OUT-BND leg, predictions are continuously adjusted assuming a GC between actual A/C position and next WPT. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 355: Lateral Guidance

    1533 .79/ FL360 UN874 TRK007° DEVRO 1437 " / " UN874 VANAD 1540 " / " UN874 45NM VADOM 1546 " / " DEST DIST EFOB EGLL27R 1625 NO NAV INTERCEPT £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 356 Distance to radial for NAV A/THR capture varies from different criteria (e.g. Ground Speed, angle of interception). To leave MANUAL leg in case of RADIAL OUT refer to F-PLN sequencing in this chapter. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 357: Hold Function

    TURN, TIME DIST parameters. HOLD AT TIGER LAST EXIT field provides FUEL and INB CRS [ ]° COMPUTED} time predictions. TURN DATABASE} TIME/DIST These fields are described below. 1.0/---- LAST EXIT FUEL ---- ---.- <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 358: Title Page

    HOLD AT. 1.0/3.5 If DATABASE hold does not exist in the LAST EXIT NAVdb arrow is not displayed. FUEL 2231 This prompt is not available when a HOLD <RETURN is selected at PPOS. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 359: Holding Parameters: Inb Crs, Turn, Time/Dist

    In the example a COMPUTED HOLD at BIG has been selected (TMPY F-PLN has been created), INB CRS is modified, which causes change hold in a HOLD AT BIG. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 360: Last Exit

    + BIG to EGLL 27R EHAM 1213 GW / CG 63.5 /25.0 5.50/FF+FQ RTE RSV/% CRZTEMP/TROPO 0.1/ 5.0 ----°/35000 FINAL TIME 1.0/0030 EXTRA TIME 1.1/0031 See also Part III: Ch 6 Fuel monitoring J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 361: Nd Display

    For range scale 160 or 320 NM, or when holding pattern is not the active or next leg, HOLD is shown by a white arrow that originates at the associated fix and indicates the direction of the turn. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 362: Hold Entries

    ND displays both the joining track and the entire holding pattern. Examples are shown below. When leg entry is "limit" between Teardrop and Parallel entry, FMGC may compute and display the two entries. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 363: Hold To An Altitude (Ha)

    (INB CRS, TURN, TIME/DIST 1.0/3.5 TIME/DIST), the hold changes for a HOLD AT, hold with manual LAST EXIT FUEL termination (HM) and the automatic ---- ---.- exit is no longer available. <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 364: Hold To A Fix (Hf)

    If the pilot modifies any of the parameters of the holding pattern (INB CRS, TURN, TIME/DIST), the hold becomes a hold with manual termination and the automatic exit is no longer available. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 365: Hold With Manual Termination (Hm)

    [ ]° COMPUTED} TURN ND ........Check DATABASE TIME/DIST 1.5/---- LAST EXIT FUEL ---- ---.- <RETURN COMPUTED HOLD PPOS INB CRS 353° COMPUTED TURN DATABASE TIME/DIST 1.5/5.7 LAST EXIT FUEL 0149 TMPY <F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 366: Hold At A Waypoint

    WPT. − If discontinuities exist before and after the revise WPT, INB CRS cannot be computed. In this case arrow prompt is not available beside COMPUTED J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 367 TMPY {ERASE INSERT* £$ THV001 {} BIG3B SPD/ALT D139L 1615 *250/ 5720 BIG3B 1618 *220/ HOLD HOLD R C303° ---- ---/ ----- (DECEL) 1619 220/ 2500 DEST DIST EFOB EGLL27R 1625 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 368: Predictions And Guidance (Hm)

    Note: HOLD size is based on A/C predicted speed at HOLD entry fix; thus in case of overspeed the HOLD size can be above the expected size. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 369: When In Hold

    " / " UN874 27NM DEVRO 1548 " / " DEST DIST EFOB EGLL27R 1629 £$ HOLD AT ADABI INB CRS 356° COMPUTED} TURN DATABASE TIME/DIST 1.5/5.7 LAST EXIT FUEL 2024 <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 370: Immediate Exit Prompt

    − If SPD is managed, target speed returns to the applicable speed of the current flight phase, − If DES mode is engaged rate of descent is adjusted according to vertical profile computation. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 371: Time To Exit

    (extra fuel is zero). HOLD R EXIT* C355° ADABI 1603 .79/ FL360 UN874 TRK016° BOKNO 1607 " / " UN874 27NM DEVRO 1611 " / " DEST DIST EFOB EGLL27R 1656 TIME TO EXIT £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 372: Hold Deletion

    BIG3B SPD/ALT D139L 1615 *250/ FL106 BIG3B 1618 *220/ *4980 TRK336° (DECEL) 1619 220/ 2500 C335 BIG07@ 1620 137/ *2500 C273° CI27R 1623 " / *2500 DEST DIST EFOB EGLL27R 1626 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 373: Offset Function

    £$ The offset ends by default at the last consecutive "offsetable" waypoint. LAT REV FROM PPOS 48°33.0N/001°16.2E OFFSET range is 1 to 50 NM. <OFFSET <HOLD <RETURN OFFSET FROM PPOS OFFSET <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 374: Offset Insert

    " / " DEST DIST EFOB EGLL27R 2113 £$ On ND: new active track is shown by a continuous green line, original track by a dashed green line. OFST xx is indicated. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 375 EGLL27R 2113 £$ A HOLD is not offsetable, then if a HOLD is inserted on an OFFSET path, offset is terminated at this point. Predictions do not take into account OFFSET transitions. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 376: Offset Deletion

    / FL360 BRG015° BOKNO 1536 .79/ FL360 UN874 TRK007° DEVRO 1540 " / " UN874 VANAD 1543 " / " UN874 45NM VADOM 1549 " / " DEST DIST EFOB EGLL27R 2113 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 377: Scratchpad Messages (Automatic Deletion)

    This scratchpad messages (amber) is triggered when an OFFSET is selected and the SEC F-PLN is activated, deleting the selected OFFSET or, a revision is made in TMPY F-PLN, which causes deletion of the selected OFFSET. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 378: Alternate Function

    TRK (great circle), EXTRA fuel (zero {NO ALTN wind) and DIST for the entered ALTN F-PLN route. <RETURN − [line 4] shows NO ALTN with EXTRA fuel. Example shows EHAM (green) entered as ALTN for EGLL. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 379 TRK330° Enter or revise ALTN route as DIMAL 1116 " / FL308 appropriate on F-PLN page. ALESO 1117 293/ FL286 BIG3B 42NM TIGER 1129 " /*FL154 DEST DIST EFOB EGLL27R 1136 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 380 ALTN CO RTE EHAM TRK EXTRA DIST Select & insert TMPY F-PLN. OTHER ALTN EHAM 075° Entered ALTN is now active. EXTRA Enter ALTN route on F-PLN page. {NO ALTN TMPY <F-PLN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 381: With Altn In Navdb

    − EGSS, EGCC (with CO RTE LHRMAN1), EHAM (with CO RTE LHRAMS1), EBBR, EGPK are also listed. Color logic is same as Departure & Arrival pages: − Active – green, − Selected (TMPY) – yellow, − Available (not selected) – blue. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 382 <RETURN ALTERNATES FOR EGLL DEST DIST EFOB £ ALTN CO RTE EGLL27R 1806 EGSS £$ TRK EXTRA DIST {EGKK 152° EGSS 046° LHRMAN1 EXTRA EGCC 329° LHRAMS1 {EHAM 075° TMPY <F-PLN £ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 383 146° FMS computes TRK, EXTRA fuel, for EXTRA defaulted DIST on [line 3] as described {NO ALTN TMPY above. <F-PLN Check fuel reserve. TMPY F-PLN select [6L] and insert [6R], as above. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 384 TRK EXTRA DIST − Associated EXTRA fuel is shown in {EBBR 100° [line 4]. {EGPK 328° -0.5 OTHER ALTN TMPY F-PLN select [6L] and insert EXTRA [6R] as above. NO ALTN TMPY <F-PLN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 385: Enable Altn Function

    DIMAL. LAT REV FROM DIMAL 50°29.6N/001°22.0E LAT REV page at selected WPT is displayed, showing ENABLE ALTN NEXT WPT prompt at [4L]. <HOLD ENABLE NEW DEST {ALTN AIRWAYS> <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 386: With Altn Rte Entered In Active F-Pln

    Since CLN exists in the ALTN F-PLN, REDFA 1832 *293/*22710 WPTs between the DISCONTINUITY and REDFA 40NM CLN (EGLL, BPK) are “collapsed” (i.e. SULUT 1837 " / " ONCE THEN automatically deleted). {UNDO/ERASE INSERT* £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 387 EHAM18R 1144 ENTER DEST DATA £$ If TMPY F-PLN shows desired route to ALTN, insert it in the ACTIVE F-PLN: INSERT prompt [6R] ..Press The ALTN F-PLN is now the ACTIVE F-PLN. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 388: Without Altn Rte Entered In Active F-Pln

    FL220 if DEST to ALTN distance is below 200 NM, or FL310 if above. This value is modifiable, if FCU altitude is set above the default FL, "NEW CRZ ALT" s-pad msg is triggered. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 389 CRUISE WIND page ............ 29 DESCENT WIND page ..........30 Alternate wind [1R]............. 31 4.3. STEP ALTS ............... 32 To enter STEP CLB or DES ........... 32 To delete a STEP CLB or DES........35 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 390 MULTIPHASE VERTICAL F-PLN management PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 391: Vertical Constraints

    * symbol (magenta); if predicted as missed, predicted speed overwrites the SPD LIM value, preceded by a * symbol (amber). On ND, SPD LIM point is shown by a solid magenta circle. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 392: To Enter Or Modify Clb Or Des Spd Lim

    (SPD)(LIM) values are entered in C356° BRG339° ACTIVE F-PLN. 1132 280/ FL123 (SPD) TRK357° (LIM) 1133 *280/ FL150 (T/C) 1138 .79/ FL360 FIST5A 10NM FISTO 1140 " / " DEST DIST EFOB EGLL27R 1251 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 393: To Delete Clb Or Des Spd Lim

    Vertical constraints may be modified or cleared directly on F-PLN pages via right LSKs. This method is not recommended, since a possible simultaneous leg- switching could cause inadvertent revision of the adjacent WPT. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 394: Spd Cstr [3L]

    − ALT is within 150 ft of SPEED LIMIT ALTITUDE. Message is cleared when speed no longer exceeds the SPEED LIMIT + 5 KT. See also Part II: Ch 4 Climb for example. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 395: To Enter Or Modify A Spd Cstr At A Wpt

    (SPD) BRG339° (LIM) 1145 *220/ FL100 on EFIS control panel. C356° TRK325° 1145 *220/ FL123 (T/C) 1153 .79/ FL360 FIST5A 10NM FISTO 1154 " / " DEST DIST EFOB EGLL27R 1306 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 396 If speed is managed, SPD at all BIG3B TIGER 1337 " /*FL154 WPTs after the revise point are (SPD) superseded by the new speed (LIM) 1339 *250/FL100 DEST DIST EFOB constraint if more restrictive. EGLL27R 1350 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 397: Spd Cstr In Crz

    A SPD CSTR at a WPT in CRZ segment, entered when A/C is in CLB phase, causes this display. VERT REV AT ADABI EFOB=5.5 EXTRA=1.1 CLB SPD LIM UTC CSTR 250/FL100 SPD CSTR ALT CSTR FL350 ACCESS <WIND DATA STEP ALTS> {CLB DES} AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 398: To Delete A Spd Cstr

    / FL287 BRG340° (T/C) 1500 .79/ FL360 UN874 TRK339° FOUCO 1507 " / " UN874 ADABI 1513 " / " UN874 30NM BOKNO 1517 " / " DEST DIST EFOB EGLL27R 1607 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 399: Utc Cstr [2R]

    1 min/1000 NM. UTC CSTR remains “missed” until Time Tolerance decreases to 15 sec for distances up to 2000 NM, adjusted at same rate as above for longer distances. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 400: To Enter Utc Cstr At A Wpt

    * symbol UN874 TRK012° PODEM 1559 " / FL360 (amber). UN874 ABUDA 1606 " / FL360 10NM (T/D) 1608 .82/ FL360 TMPY INSERT [6R] ..Press DEST DIST EFOB EGLL27R 1629 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 401: To Enter Estimated Time Of Take-Off (Ett)

    An ETT cannot be cleared from the VERT REV page at origin, but can be modified. An ETT may be computed by FMGC as a result of a UTC CSTR entry en-route or at DEST (see below). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 402: To Enter Desired Time Of Arrival At Dest

    FMGC computes a revised CI to comply C356° 1510 250/ FL85 with desired arrival time as closely as (SPD) possible, as described above. (LIM) 1510 *250/FL100 DEST DIST EFOB EGLL27R 1630 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 403: To Delete Or Modify Utc Cstr

    Using CLR function directly from F-PLN page (right LSKs) would cause deletion of all vertical constarints at the revise point. UTC CSTR in SEC F-PLN Refer to Part III: Ch 5 SEC F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 404: Alt Cstr [4R]

    An ALT CSTR is considered matched if ALT ERROR is less than or equal to 250 ft; otherwise it is considered missed. It remains missed until the ALT ERROR decreases to 200 ft. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 405: To Enter Or Modify Alt Cstr At A Wpt

    TMPY F-PLN shows predicted ALT at D144H} 0002 " / *3130 C356° revise point preceded by * symbol 0005 250/ *FL80 (amber). (SPD) (LIM) 0005 *250/FL100 DEST DIST EFOB EGLL27R 0125 TMPY INSERT [6R] ..Press £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 406 SPD CSTR ALT CSTR SPD CSTR ALT CSTR FL080 +FL120 ALT ERROR -3500 ACCESS ACCESS <WIND DATA STEP ALTS> <WIND DATA STEP ALTS> <RETURN <RETURN IGNORED THR CLB OP CLB 1FD2 A/THR J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 407: Clb Or Des

    MULTIPHASE VERTICAL F-PLN management 19 Vertical Guidance: ALT CSTRs are taken into account by the FMGS for target altitude. Refer to Part II: Climb - Ch 4.3 Constraints management for details. {CLB OR DES} When the FMGC cannot determine THV001 {}...

  • Page 408: Alt Window Cstrs

    ND shows upper and lower limits (magenta), if CSTR p/b pushed on EFIS control panel. These constraints may be modified only by replacing with a CSTR AT, AT OR ABOVE or AT OR BELOW. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 409: To Delete Alt Cstrs

    − Use CLR function for deletion. In this case it will delete all vertical constraints. As already explained this method is not recommended due to possible error insertion in case of simultaneous leg switching. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 410: Alt Cstrs In Approach Procedure

    VERT REV AT EGLL27R approach points before (and not EFOB=3.9 EXTRA= including) the RWY. DES SPD LIM UTC CSTR 250/FL100 G/S INTCPT ACCESS <WIND DATA STEP ALTS> <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 411: Wind Data

    See Part III: Ch 9 Data Link When accessed via VERT REV pages at a WPT, the display is CLIMB / CRUISE / DESCENT WIND page according to the phase at which the WPT is belonging. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 412 CRUISE WIND AT ADABI TRU WIND/ALT 300°/040 AT FL360 WIND REQUEST* NEXT PHASE> <RETURN £$ DESCENT WIND TRU WIND/ALT ALTN WIND 320°/040/FL300 300°/035 300°/030/FL200 WIND 290°/020/FL100 REQUEST* PREV [ ]°/[ ]/[ PHASE> <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 413 SEC CRZ WIND AT WOBUN TRU WIND/ALT [ ]°/[ ]/[ AT FL180 WIND REQUEST* PREV PHASE> NEXT PHASE> <RETURN SEC DESCENT WIND TRU WIND/ALT [ ]°/[ ]/[ FL310 WIND REQUEST* PREV PHASE> <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 414 £$ DESCENT WIND SEC DESCENT WIND TRU WIND/ALT ALTN WIND TRU WIND/ALT [ ]°/[ ]/[ [ ]°/[ ] [ ]°/[ ]/[ FL310 WIND WIND REQUEST REQUEST PREV PREV PHASE> PHASE> <RETURN <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 415 (providing the destination has been modified in this latter case). Climb winds are not automatically deleted if the origin airport is changed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 416 REQUEST base cycle change, or after a DEP 110°/025/FL350 airport change. They are only deleted NEXT 110°/025/FL360 PHASE> when overwritten during the descent of UPDATE UPDATE the next flight leg. {CANCEL INSERT* J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 417 UPDATE UPDATE {CANCEL INSERT* data. When this prompt is pressed, £$ the page reverts to the respective F- PLN A page oriented with the FROM Ex. 4 waypoint. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 418 F- 247°/015/GRND PLN A page oriented with the FROM waypoint. Descent winds (including alternate <RETURN wind) are automatically deleted if the destination airport is changed. Ex. 4 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 419 FL220 if distance to ALTN is 247°/015/GRND less than 200NM, otherwise FL310. <RETURN This field is blanked if an alternate destination is not defined. The alternate wind is automatically deleted if the alternate airport is changed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 420 F-PLN (e.g. 360/ADABI/20). In this case a PLACE/DIST TMPY <F-PLN waypoint is automatically inserted in F-PLN. Entry above MAX ALT causes "STEP ABOVE MAX FL" s-pad msg (white). Minimum ALT change allowed is 500 ft. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 421 CRZ phase is extended. It is shown on STEP ALTS page with “IGNORED” indicator. This also applies if start point found to be before T/C, or end pointt after T/D. TMPY <F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 422 The step climb or step descent is not initiated automatically; FL change must be initiated by pilot via FCU. If FL change is not initiated, "STEP DELETED" s-pad msg (white) is triggered. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 423 .79/ FL360 0022 .77/ FL360 TMPY TMPY TRK330° {ERASE INSERT* (T/D) 0133 .79/ FL360 UT426 $£ DIMAL 0136 " / FL308 ALESO 0137 293 / FL286 DEST UTC DIST EFOB EGLL27R 0156 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 424 MULTIPHASE VERTICAL F-PLN management PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 425 ND display ..............7 5.4. Use of SEC F-PLN ............8 SEC F-PLN sequencing........... 8 To create a SEC F-PLN........... 9 By COPY ACTIVE............9 From INIT..............9 To revise SEC F-PLN.............11 SEC F-PLN activation............12 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 426 MULTI PHASE SEC F-PLN PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 427 SEC F-PLN may be stored in PILOTS ROUTES. See Part III: Ch 7.1 Navigation data. For use of SEC F-PLN in specific flight phases, refer to PART II: Ch 2 Preflight, Ch 5 Cruise, Ch 7 Approach. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 428 THV001 {} FIST5A SPD/ALT LFBO14R 0000 141/ H144° BRG144° 0000 153/ C144° TRK144° D144H} 0002 " / *3130 C356° 0005 250/ FL85 (SPD) (LIM) 0005 *250/ FL100 DEST DIST EFOB EGLL27R 0125 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 429 TRANS ALT DRT TO-FLX TO O=216 []/[ 5000 TRANS ALT DRT TO-FLX TO THR RED/ACC ENG OUT ACC 5000 1990/3490 1990 THR RED/ACC ENG OUT ACC NEXT 1990/1990 1990 PHASE> NEXT PHASE> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 430 Vertical slew keys are used to scroll and view F-PLN pages content. Airport key is available with the same logic than F-PLN pages. All data in SEC F-PLN pages are shown white. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 431 A/C symbol is shown according to area displayed. SEC INDEX {COPY ACTIVE <SEC F-PLN {DELETE SEC *ACTIVATE SEC SEC F-PLN PRINT* ND in NAV/ARC mode ND in PLAN ND in PLAN mode mode AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 432 " / " DEST DIST EFOB DEST TIME DIST EFOB EGLL27R 1702 EGLL27R 0118 £$ £$ As explained above, if SEC is not sequenced as ACTIVE, PERF prompt [2R] is not displayed. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 433 This deletes all data contained {DELETE SEC in SEC F-PLN. *ACTIVATE SEC SEC INDEX SEC F-PLN PRINT* INIT [1R] ....Press {COPY ACTIVE INIT> SEC INIT page A is displayed. <SEC F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 434 ---F-PLN DISCONTINUITY-- (SPD) in SEC INIT page B. (LIM) 1656 *250/ FL100 (T/C) 1721 338/ FL150 47NM (T/D) 1727 326/ FL150 DEST DIST EFOB EGCC 1740 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 435 PERF prompt. In this case, SEC must be prepared by using INIT prompt as described above. To simplify SEC INIT process, it may be useful to store at first the ACTIVE F-PLN in PILOTS ROUTES; then use this CO RTE to init SEC. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 436 FROM TIME SPD/ALT 1712 / FL358 BRG357° ADABI 1748 .79/ FL360 TRK016° 1756 " / " 1801 " / " 55NM BAMES 1809 " / " DEST DIST EFOB EGLL27R 1843 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 437 ADABI 2041 .79/ FL360 TRK026° 2049 " / " 2054 " / " 55NM BAMES 2101 " / " DEST DIST EFOB FMA ......... Check EGLL27R 2135 £$ Verify modes as required. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 438 / FL360 FIST5A BRG160° FISTO 1504 .79/ FL360 UN874 TRK339° FOUCO 1515 " / " UN874 DABI 1522 " " UN874 30NM BOKNO 1526 " / " DEST DIST EFOB EGLL27R 1616 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 439 At SEC F-PLN activation, GW and/or CG entered in SEC INIT page B are transferred in ACTIVE F-PLN. In case of wrong entry this may generate "CHECK GW" s-pad msg (amber) and erroneous guidance (SPD THRUST target). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 440 MULTI PHASE SEC F-PLN PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 441 Part III: Chapter 6 – FUEL Monitoring Contents 6.1. Overview ..............3 6.2. FUEL PRED page ............3 Presentation ..............3 Fuel to Divert and EXTRA/TIME........5 6.3. F-PLN page B ............. 7 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 442 MULTI PHASE FUEL monitoring PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 443 ACTIVE F-PLN and reserves as shown in the FUEL PRED page. When a negative extra fuel is displayed, the extra time is dashed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 444 Line 3R shows FOB computed EHAM 1829 using FF sensor only. 63.7 /25.0 5.68/FQ To restore a deselected sensor: RTE RSV/% CRZTEMP/TROPO 0.1/5.0 ----°/35000 either use CLR function, or FINAL/TIME re-enter / FF+FQ. 1.0/0030 EXTRA/TIME 1.3/0036 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 445 HOLD time available displayed on HOLD page is based on EXTRA shown on FUEL PRED page. If EXTRA is not correct, HOLD TIME is also erroneous. In this case an adjustment should be made to FINAL fuel. See following example. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 446 1630 63.7 /25.0 5.68/FF+FQ RTE RSV/% CRZTEMP/TROPO 0.1/5.0 ----°/35000 FINAL/TIME 1.0/0030 EXTRA/TIME FUEL PRED 3.0/0122 EFOB EGLL 1625 EGKK 1630 63.7 /25.0 5.68/FF+FQ RTE RSV/% CRZTEMP/TROPO 0.1/5.0 ----°/35000 FINAL/TIME 1.7/0049 EXTRA/TIME 2.3/0101 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 447 FROM THV001 {} EFOB T WIND 299°/039 BRG356° 68NM ADABI 300°/040 UN874 TRK016° BOKNO " °/ " UN874 DEVRO 310°/050 UN874 22NM VANAD " °/ " DEST DIST EFOB EGLL27R 1625 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 448 MULTI PHASE FUEL monitoring PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 449 Manual selection of an ILS by a frequency...... 30 Manual selection of an ILS by an ident......32 Manual selection of a MLS by a channel ......34 Manual selection of a MLS by an ident ......36 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 450 ESTIMATED Position Error (EPE) [6R] ......45 ACCURACY [6C] ............45 Navigation accuracy cross-check ........47 PREDICTIVE GPS function..........49 DESELECT SATELLITE function ........50 MANUAL POSITION UPDATE function......51 POSITION DISCREPANCY..........53 FMS1/FMS2 POS DIFF ..........53 CHECK IRS (1)(2)(3)/FM POSITION .......53 MAP-SHIFT ..............53 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 451: Navigation Data

    − 01 is reference number in the current cycle, Operator NAV data base contains only selected data requested by operator in a defined geographical area including Airports, RWYs, SIDs/STARs, approach procedures, AWYs as specified. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 452: Data Index 2/2 Page (All Nav Data)

    <WINDS SEC F-PLN <WINDS ALL NAV data DATA INDEX 2/2 {} PILOTS <WAYPOINTS WAYPOINTS> PILOTS <NAVAIDS NAVAIDS> PILOTS <RUNWAYS RUNWAYS> PILOTS <ROUTES ROUTES> ACTIVE F-PLN <WINDS SEC F-PLN <WINDS PILOTS STORED data J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 453: Waypoint [1L]

    If the IDENT is not r ecognized NEW WAYPOINT by the system, the NEW IDENT WAYPOINT page is displayed. LAT/LONG ____.__/_____.__ See Pilot da PLACE /BRG /DIST _______/___° /___._ PLACE-BRG /PLACE-BRG _____-___° /_____-___° RETURN> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 454: Navaid [2L]

    LAT/LONG for ILS, I LS DME or ILS TAC is LAT/LONG of localizer. LAT/LONG for MLS, MLS DME is LAT/LONG of azimuth antenna. REQ or CHAN [4L]. Frequency for ILS, CHAN for MLS. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 455 SLOPE [4R]: If NAVAID is MLS. ____.__/_____.__ If the entered identifier is not found in NAVdb or pilot stored navaid list, NEW RETURN> NAVAID page is displayed with the IDENT field filled. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 456: Runway [3L]

    If both ILS and MLS facilities are available for the RWY, ILS ident has precedence over MLS. ntry of an unknown ARPT in [1L] causes NEW RUNWAY page to be displayed with the ident inserted. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 457: Route [4L]

    UN874 BAMES fit on one page display, vertical UT191 ABUDA DIMAL arrows are displayed bottom righ ALESO BIG3B ABUDA BIG07 ILS27R Use vertical slew keys to scroll and see all the content. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 458 (top right) is 4430.8N/00115.6E PLACE /BRG /DIST updated, /000° /50.0 − NEW WAYPOINT prompt [5R] is available for creatio n of WAYPOINT> another waypoint, − DELETE ALL p rompt [6R] DELETE ALL} (see below). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 459 WAYPOINT> DELETE ALL} PILOT ELEMENT RETAINED To cancel CONFIRM DELETE ALL, select another MCDU page or press a LSK other than [6R]; DELETE ALL prompt is displayed again in [6R]. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 460 _______/___° /___._ PLACE-BRG /PLACE-BRG Stored waypoints are automatically _____-___° /_____-___° deleted when FMGC switches to RETURN> DONE phase if CO RTE retention is selected NO in AMI file. Otherwise they are retained. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 461: Pilots Navaids [2R]

    If twenty NAVAIDS have already been stored and NEW NAVAID prompt is pressed, "LIST OF 20 IN USE" s-pad msg (white) is triggered. Logic for deletion of stored navaids, all or individually, and associated scratchpad messages is identical that for stored waypoints. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 462 ___° NEW NAVAID FREQ IDENT RWY IDENT 108.50 _______ CLASS CATEGORY RETURN> LAT/LONG COURSE 4500.0N/00000.0E 000° FREQ 108.50 RETURN> NEW RUNWAY ABCD36 IDENT ILS IDENT ABCD36 LAT/LONG ____.__/_____.__ LENGTH ____ ____ RETURN> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 463: Pilots Runways [3R]

    If ten RUNWAYS have already been stored and NEW RUNWAY prompt is pressed, "LIST OF 10 IN USE" s-pad msg (white) is triggered. Logic for deletion of stored runways, all or individually and associated scratchpad messages is identical to stored waypoints. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 464: Pilots Routes

    FIST5AFISTO FIST5ATOU FOUCO UN874 BAMES PD02 FIST5AFISTO UT191 ABUDA DIMAL FOUCO UN874 BAMES ALESO BIG3B ABUDA UT191 ABUDA DIMAL BIG07 ILS27R ALESO BIG3B ABUDA BIG07 ILS27R {DELETE ALL ROUTE> {DELETE ALL ROUTE> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 465: Ac Status Page

    See also Part I: Preflight Ch 2.1 01RTES 01RWYS CHG CODE 02WPTS 02NAVS CONFIRM DEL* IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> A320-200 CFM56-5-B4 ACTIVE NAV DATA BASE 21JAN-18FEB THV1040101 SECOND NAV DATA BASE {24DEC-21JAN CHG CODE IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 466: Duplicate Names Page

    £$ DUPLICATE NAMES page is described DUPLICATE NAMES below. 38NM LAT/LONG FREQ *AMB 45N/000E 120NM *AMB 47N/001E 341.0 121NM *AMB 47N/001E 113.70 5001NM *AMB 01S/078W 360.0 6113NM *AMB 33S/070W 116.10 <RETURN £ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 467 / FL358 revision. BRG357° ADABI 1532 .79/ FL360 In the example, AMB VORDME freq. TRK026° 1540 " / " 113.70 is selected. ---F-PLN DISCONTINUITY-- BOKNO 1544 .79/ " TMPY TMPY {ERASE INSERT* £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 468 If the DUPLICATE NAMES page is displayed on the ONSIDE MCDU and an attempt is made to delete a pilot defined element displayed on that DUPLICATE NAMES page, "PILOT ELEMENT RETAINED" s-pad msg (white) is displayed and element is not deleted. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 469: Rad Nav Page

    − Title lines are displayed but entry is not possible. STBY RADIO NAV VOR1/FREQ FREQ/VOR2 ILS /FREQ CHAN/ MLS SLOPE ADF1/FREQ FREQ/ADF2 Fields [3R] MLS & [4R] ADF2 are operator options. If not activated field(s) is (are) blank. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 470: General Rules

    Auto-tuned data and data resulting from manual entry are displayed in small font (blue). Until cleared, manually tuned navaid has priority over auto-tuned navaid. RADNAV page is automatically cleared when FMS phase switches to DONE. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 471: Radio Nav Page Description

    LON is auto-tuned by the FMGC 113.6 because it is the closest VOR DME. RADIO NAV VOR1/FREQ FREQ/VOR2 LON/113.60 115.10/BIG ILS /FREQ CHAN/ MLS IRR/110.30 [ ]/[ SLOPE F273 ADF1/FREQ FREQ/ADF2 .]/[ 113.6 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 472 [ ]/[ SLOPE ident field; "NOT IN DATA ADF1/FREQ FREQ/ADF2 BASE" s-pad msg (white) is .]/[ VOR1 triggered. ND shows 113.7O M frequency only. NOT IN DATA BASE J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 473: Crs [2L] - [2R]

    SLOPE Ex. 1: OAN (TACAN). Ex. 2: 110.7. ADF1/FREQ FREQ/ADF2 .]/[ RADIO NAV VOR1/FREQ FREQ/VOR2 ]/110.70 117.70/TOU ILS /FREQ CHAN/ MLS TBS/110.70 [ ]/[ SLOPE VOR1 F144 11O.7O M ADF1/FREQ FREQ/ADF2 .]/[ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 474: Ils/Freq [3L]

    When a course is displayed (entered ILS /FREQ CHAN/ MLS manually or automatically), it can be ]/110.60 [ ]/[ modified. Only manually entered courses SLOPE ____ can be cleared. ADF1/FREQ FREQ/ADF2 .]/[ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 475: Mls [3R] - [4R]

    MLS is tuned the MLS is deselected, [3R] and [4R] fields revert to brackets. When a course is displayed (manually or automatically tuned), it can be modified. Only manually entered courses can be cleared. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 476: Adf [5L] - [5R]

    [ ]/[ SLOPE enabling BFO operation. If a CLR is performed on that field, BFO ADF1/FREQ FREQ/ADF2 277.0/CHT operation is cancelled and arrow re- appears. ADF2 BFO} Re-tuning ADF automatically cancels BFO operation. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 477: To Cancel Manually Tuned Navaids

    VOR1/FREQ FREQ/VOR2 LON/113.60 113.60/LON ILS /FREQ CHAN/ MLS [ ]/[ SLOPE ADF1/FREQ FREQ/ADF2 277.0/CHT RADIO NAV VOR1/FREQ FREQ/VOR2 ADF2 BFO LON/113.60 113.60/LON ILS /FREQ CHAN/ MLS [ ]/[ SLOPE ADF1/FREQ FREQ/ADF2 .]/[ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 478: Supplementary Information

    MLS approach has been SLOPE ____ selected, only the frequency is displayed ADF1/FREQ FREQ/ADF2 and brackets are displayed in [3L], no .]/[ course is auto-tuned, [4L] displays amber boxes, no message is displayed. RWY/LS MISMATCH J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 479 If no LS (ILS or MLS) has been selected at the departure runway, only the frequency is displayed and brackets are displayed in [3L], no course is auto-tuned, [4L] displays amber boxes, no message is displayed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 480 ILL/109.50 [ ]/[ SLOPE LOC bearing of the entered ILS is auto- F273 ADF1/FREQ FREQ/ADF2 tuned and displayed in [4L], with logic .]/[ "F" or "B". RWY/LS MISMATCH J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 481 If no LS (ILS or MLS) has been selected at the departure runway, no message is displayed, the LOC bearing of the entered ILS is auto-tuned and displayed in [4L], with logic "F" or "B". AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 482 3R, course and slope are not auto-tuned, [4R] displays amber boxes for the course, dashes for the slope, no message is displayed J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 483 If no LS (ILS or MLS) has been selected at the origin runway, only the channel is displayed and brackets are displayed in 3R, no course is auto-tuned, 4R displays amber boxes for the course, dashes for the slope. No message is displayed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 484 SLOPE -3.0 displayed. The nominal azimuth of the ADF1/FREQ FREQ/ADF2 entered MLS is auto-tuned and displayed .]/[ in [4R]; dashes are displayed for the slope. RWY/LS MISMATCH J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 485 If no LS (ILS or MLS) has been selected at the origin runway, no message is displayed. The nominal azimuth of the entered MLS is auto- tuned and displayed in [4R]; dashes are displayed for slope. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 486: Position Monitoring

    Title changes to POSITION FROZEN AT XXXX, showing time at which display is frozen. UNFREEZE prompt enables return to continuous updating of position data. If another page is selected, FREEZE function is automatically cancelled. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 487: Irs Monitor Page

    1.5NM/H <IRS3 − The landing RWY was as selected in DRIFT 2.5NM/H ACTIVE F-PLN. If not, DRIFT rate computation is not correct. See also Part II: Flight phases Ch 9 - Done AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 488 IRS1 FROZEN AT 1535 POSITION 45°09.8N/000°49.5E TTRK NEXT IRS> prompt allows access 337.2 to other IRS data pages. THDG MHDG 334.1 335.7 WIND GPIRS ACCUR 300°/040 100M GPIRS POSITION 45°09.8N/000°49.5E {UNFREEZE NEXT IRS> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 489: Gps Monitor Page

    114.80 on ND and DDRMI. VOR/DME <MEN 115.30 [2 & 3L] show navaids used AUTO for radio position <IRR 110.30 DESELECT computation. {GPS [4L] shows an ILS or MLS, if <RETURN tuned. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 490: Deselect Navaid Function

    VOR/DME AUTO DESELECT <CNA 114.65 VOR/DME Navaid deselections are cleared <CNA 114.65 VOR/DME when FMGC phase switches to <MEN 113.75 AUTO DONE, or if second NAVdb is <IRR 110.30 activated. DESELECT {GPS <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 491: Deselect Gps Function

    REQUIRED ACCUR ESTIMATED 2.0NM HIGH 0.08NM CRUISE THV001 REC MAX FL360 FL360 FL389 <REPORT UPDATE AT BRG /DIST 354° /382.2 EGLL27R PREDICTIVE <GPS REQUIRED ACCUR ESTIMATED 2.0NM HIGH 0.28NM GPS PRIMARY LOST AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 492: Position Accuracy

    HIGH 0.28NM GPS PRIMARY LOST CRUISE THV001 REC MAX FL360 FL360 FL389 <REPORT UPDATE AT BRG /DIST 354° /382.2 EGLL27R PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 2.0NM HIGH 0.08NM GPS PRIMARY J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 493: Required Navigation Performance (Rnp) [6L]

    (e.g. GPS, radio navaids, IRS). CCURACY [6C] This field shows t he accuracy based on EPE and RNP: − If EPE is below RNP, ACCURACY is HIGH, − If EPE is above RNP, ACCURACY is LOW. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 494 If ACCUR becomes LOW, "GPS PRIMARY LOST" s-pad msg (amber) is displayed. This situation should occur in exceptional cases or after a wrong MANUAL UPDATE. EPE is defaulted at 0.2 NM at IRS alignment. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 495: Navigation Accuracy Cross-Check

    REQUIRED ACCUR ESTIMATED 2.0NM HIGH 0.08NM This method may be used for non auto-tuned navaids, which, in this case, must be forced manually in RADNAV page. See also Part II: Ch.7.2 – Approach. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 496 If a pilot defined waypoint (WPT, NAVAID, ARPT or RWY) has been entered, and then deleted through DELETE ALL prompt on A/C STATUS page or on PILOT WAYPOINT page, the display reverts to brackets with BRG/DIST dashed. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 497: Predictive Gps Function

    ETA for a WPT in existing ACTIVE F- -15 -10 -5 ETA+5 +10 +15 PLN is not automatically entered, and DESELECTED SATELLITES must be inserted manually. ETA [3R]......Enter Ex: 1710. Predicted GPS status is then computed and displayed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 498: Deselect Satellite Function

    To deselect all GPS inputs to position -15 -10 -5 ETA+5 +10 +15 computation, use DESELECT GPS function See SELECTED NAVAIDS p PRIMARY -15 -10 -5 ETA+5 +10 +15 in this chapter. DESELECTED SATELLITES J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 499: Manual Position Update Function

    − IDENT is shown at [3R], or if defined by LAT/LONG, PB/PB, PBD, replaced by "ENTRY". If entered ident is not in NAVdb or pilot-defined file, NEW WAYPOINT or NEW NAVAID page is displayed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 500 NM if performed on ground. <REPORT UPDATE AT BRG /DIST 000° /0.0 PREDICTIVE <GPS REQUIRED ACCUR ESTIMATED 2.0NM 4.0NM POSITION MONITOR FMGC1 4549.0N/00101.5E 3IRS/DME/DME FMGC2 4549.0N/00101.5E 3IRS/DME/DME RADIO 4549.0N/00101.5E MIX IRS 4549.9N/00102.3E IRS1 IRS2 IRS3 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 501: Position Discrepancy

    − Identify erroneous navaid and check coordinates, Navaid data may be checked via DATA INDEX 2/2 as described in Ch 7.1. − Deselect erroneous navaid via SELECTED NAVAIDS page as described above. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 502 HIGH 0.08NM In any case MANUAL UPDATE should be considered carefully and only if certainty of position used for updating. In approach FMGC position is updated by LOC (or MLS) when existing. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 503 Part III: Chapter 8 – ENGINE-OUT Contents 8.1. GENERAL DESCRIPTION..........3 8.2. PREFLIGHT / EOSID ..........4 8.3. TAKE-OFF..............6 8.4. CLIMB ................ 8 8.5. CRUISE ..............10 8.6. DESCENT/APPROACH ..........11 8.7. GO-AROUND ............12 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 504 MULTIPHASE PROCEDURES ENGINE-OUT PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 505: General Description

    − N2 > IDLE on both engines, and, CRZ FL ABOVE MAX FL − Both thrust levers have an angle greater than 5°. FMGS is in DONE or PREFLIGHT phase EO CLR prompt is pressed. Caution Pressing EO CLR prompt deactivates EO mode. EO mode cannot be restored.

  • Page 506: Preflight / Eosid

    It can only be DEPARTURES FROM LFBO modified if EO mode is activated after TRANS FIST5A NONE take-off before reaching the EOSID SIDS AVAILABLE TRANS diversion point. {AFRI5A {AFRI5H {AMOL5A {AMOL5H EOSID <RETURN NONE £ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 507 No EOSID exists for the SEC F-PLN. However, if the SEC F-PLN is activated and a departure runway with an associated EOSID is selected for this flight plan, it is automatically selected, overwriting any previous EOSID. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 508: Take-Off

    MULTIPHASE PROCEDURES ENGINE-OUT 8.3. TAKE-OFF During TAKE OFF, FMGS switches to EO mode as soon as engine-out is detected. If engine failure occurs before the EOSID diversion point: FROM THV001 {} In the example diversion point is TOU8. SPD/ALT 1000...
  • Page 509 BRG /DIST 303° /23.9 LFBO14R PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED 1.0NM HIGH 0.08NM CRZ FL ABOVE MAX FL Proceed according to SOPs for Acceleration / Flap retraction & Thrust reduction. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 510: Climb

    MULTIPHASE PROCEDURES ENGINE-OUT 8.4. CLIMB THR CLB OP CLB If an engine failure 1FD2 occurs when FMGS is in LVR MCT A/THR CLIMB phase, EO mode is activated and: − LVR MCT flashes on FMA, − Both MCDUs switch automatically to the PERF...
  • Page 511 5.75/FF+FQ DEST DIST EFOB RTE RSV/% CRZTEMP/TROPO EGLL27R ---- 534 ----- ---.-/ 5.0 -56° /35000 $£ FINAL TIME ---.-/0030 EXTRA TIME ---.-/---- Proceed according to OPS procedures for EO procedure during climb. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 512: Cruise

    MULTIPHASE PROCEDURES ENGINE-OUT 8.5. CRUISE If an engine failure occurs when FMGS is in CRUISE phase, EO ACT MODE UTC DEST mode is activated and: MANAGED 1629 CLR* − LVR MCT flashes on FMA, EO LRC − Both MCDUs switch...

  • Page 513: Descent/Approach

    MULTIPHASE ENGINE-OUT 11 8.6. DESCENT/APPROACH If an engine failure occurs SPEED OP DES when FMGS is in 1FD2 DESCENT or APPROACH LVR MCT A/THR phase, the EO mode is activated and: − LVR MCT flashes on FMA, − Both MCDUs switch to the...

  • Page 514: Go-Around

    MULTIPHASE PROCEDURES ENGINE-OUT 8.7. GO-AROUND If an engine failure occurs when FMGS is in GA TRK AP1+2 GO AROUND phase, the TOGA 1FD2 A/THR EO mode is activated MCDUs switch to the PERF GO AROUND page automatically. Proceed according to OPS procedures for Standard or Obstacle strategy.
  • Page 515 WIND REQUEST from AOC FUNCTION page ....33 WIND DATA UPLINK message........34 Wind Data: insertion/deletion ........34 WIND DATA UPLINK scratchpad messages ..... 39 Normal messages ............39 Additional messages ........... 39 Error messages ............39 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 516 Manual position report from PROG page......41 Manual position report from AOC FUNCTION page ....42 Automatic position report ..........43 Progress report ............43 Flight plan report............44 Performance data report..........45 9.6. DATA LINK SCRATCHPAD MESSAGES .......45 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 517: General Description

    AOC functions are available only if A/C Data Link communication is installed and operative. This is confirmed to pilot when (*) symbol adjacent to the AOC prompts is displayed. (Refer to OPS Manual for configuration of communication system). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 518 Before CLB phase WIND DATA UPLINK becomes active REQUEST Cruise winds Before the last waypoint of CRZ Descent winds phase sequences, or when DES or APPR phase becomes active Alternate wind If ALTN exists J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 519 - Cruise temperature - Tropopause altitude - Climb transition altitude - Cost index - Perf factor - Idle factor - ZFW CG - ZFW - Block fuel - Taxi fuel Reserve fuel AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 520: Flight Plan Init Request

    ----- /---° 36090 NOT IN DATA BASE INIT CO RTE FROM/TO TLSLHR01 ____/____ ALTN/CO RTE INIT ----/---------- REQUEST FLT NBR ________ LONG ----.-- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 521 The amber (*) symbol disappears from INIT A page (and other DATALINK FUNCTION pages) until the request is terminated. When (*) symbol re-appears, another INIT REQUEST can be sent. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 522 Data Link transmission of WIND> ALTN/CO RTE INIT CRZ FL/TEMP TROPO ---/---------- REQUEST* the request. ----- /---° 36090 FLT NBR THV001 LONG ----.-- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 523: Init Request From Aoc Function Page

    Amber (*) symbol disappears during Data Link transmission of the request. TO DATA REQ* WIND DATA REQ* PRINT <RETURN FUNCTION> AOC FUNCTION 1/2 {} UPLINK F-PLN INIT TO DATA REQ* WIND DATA REQ* PRINT <RETURN FUNCTION> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 524: F-Pln Data And Perf Data Uplink Messages

    FLT NBR THV001 This message is rejected without any LONG 4338.1N 00122.1E scratchpad message if no ACTIVE or SEC COST INDEX F-PLN exists. WIND> CRZ FL/TEMP TROPO FL360/-50° 36090 PERF DATA UPLINK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 525 FIST5A TIME SPD/ALT LFBO14R 1500 ---/ H144° BRG144° 1501 100/ C144° TRK144° D144H} 1502 250/ *3130 C356° 1505 " / FL85 (SPD) (LIM) 1505 *250/ FL100 DEST DIST EFOB EGLL27R 1655 $£ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 526: Data Insertion Via The Sec Init A Page

    LFBO/EGLL ALTN/CO RTE INIT Then amber (*) symbol reappears; EHAM REQUEST* FLT NBR another INIT REQUEST can be made. THV001 LONG ----.-- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 527: F-Pln Uplink Deletion

    AOC F-PLN INSERT prompt AOC F-PLN INSERT* disappears from both the SEC INDEX and the SEC INIT pages. SEC F-PLN PRINT* SEC INDEX {COPY ACTIVE INIT> <SEC F-PLN SEC F-PLN PRINT* AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 528 LFBO/EGLL disappears from both the SEC INDEX ALTN/CO RTE INIT and the SEC INIT pages. EHAM REQUEST* FLT NBR THV001 LONG ----.-- -----.-- COST INDEX WIND> CRZ FL/TEMP TROPO ----- /---° 36090 J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 529: F-Pln Uplink Scratchpad Messages

    If the uplink and downlink CO RTE number are different, the valid uplinked flight plan is processed, and the CHECK CO RTE scratchpad message is triggered. The message is not displayed if the uplink message is rejected. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 530: Error Messages

    (white) is displayed. If an uplink message is received after a 4 minute timeout occurs on the downlink request, it is processed as an answer to the request and not as an unsolicited message. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 531: To Data Request

    []/[ CONTAM£$ DRT TO-FLX TO TOW /TOCG SHIFT/ UPLINK TO DATA REQ page is --.-/--.- ----/ [ ] displayed as long as the FMGS TEMP/QNH TO LIMIT has not switched to the TAKE RECEIVED ---°/----- TO DATA ---- <TO DATA...
  • Page 532 CONTAM DRT TO-FLX TO entry (and vice versa). --------- ---- RECEIVED TO DATA <TO DATA REQUEST* All fields in this page are dashed until a RWY is defined or entered in [1R]. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 533 Seven types of contamination are available on a circular loop: WET, DRY, 1/4 WATER, 1/2 WATER, 1/4 SLUSH, 1/2 SLUSH and COMP SNOW. [6L] RECEIVED TO DATA prompt This white prompt allows access to UPLINK MAX TO DATA pages for display. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 534 TO by selecting a Flex Temperature, or DERATED TO by selecting a Derating Level. But there is no restriction for the selection of either mode on the second page. The field title is not modified upon pilot entry. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 535 AOC Take Off data are received or until an "AOC time out" occurs. If an UPLINK TO DATA REQ page is displayed when a transition to TAKE OFF phase occurs, the display reverts to the TAKE OFF page. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 536: To Data Request Via Aoc Function Page

    PRINT <RETURN FUNCTION> received or when uplink process has been terminated (eg. "AOC time-out"). AOC FUNCTION 1/2 {} UPLINK F-PLN INIT REQ* TO DATA WIND DATA REQ* PRINT <RETURN FUNCTION> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 537: Takeoff Data Uplink Message

    FLAPS/THS DRT TO prompt, and page title is: 140/010 2/UP0.6 CONTAM UPLINK DRT TO DATA. MAX TO> THR RED/ACC ENG OUT ACC 1990 UPLINK INSERT Fields are described below. <TO DATA UPLINK* AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 538 If MAG WIND FLAPS/THS 140/010 2/UP0.6 no valid baro setting is entered, label line CONTAM MAX TO> shows QNH. THR RED/ACC ENG OUT ACC 1990 UPLINK INSERT <TO DATA UPLINK* J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 539 This prompt provides access to DRT/FLX TO page from MAX TO page (and vice-versa). [5R] ENG OUT ACC altitude This field displays uplinked Engine-out Acceleration Altitude. If no data is available, blanks are displayed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 540: Take Off Data Insertion

    WIND REQUEST* − Other advisory data are displayed on these pages for advisory and NEXT have no impact on the system PHASE> UPDATE UPDATE when INSERT UPLINK* prompt is *CANCEL INSERT* depressed. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 541 Take Off data for all runways are deleted and are replaced with the new uplinked data. After reception of uplinked data, UPLINK TO DATA pages that contain no information display dashed fields. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 542: To Data Uplink Scratchpad Messages

    ACTIVE F-PLN or SEC F-PLN. Error message INVALID TAKEOFF UPLINK This message is displayed in case of take off uplink data rejection. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 543: Wind Data

    However, if the aircraft is on the ground prior to engine start and data have not yet been entered or inserted on any WIND page then wind data are directly inserted into that flight plan and cannot be reviewed. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 544: Wind Request

    WIND REQUEST The WIND REQUEST function is available on ground or in flight, provided FMGS is not in DESCENT or APPROACH phase. It may be initiated from any WIND page of the ACTIVE or SEC F-PLN or from AOC FUNCTION pages.
  • Page 545 NAVAIDS> PILOTS <RUNWAYS RUNWAYS> PILOTS DESCENT WIND <ROUTES ROUTES> TRU WIND/ALT ALTN WIND ACTIVE F-PLN 320°/40/FL300 300°/35 <WINDS FL250 SEC F-PLN 300°/30/FL200 <WINDS WIND 290/20/FL100 REQUEST* PREV [ ]°/[ ]/[ PHASE> <RETURN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 546 CRUISE WIND AT FOUCO DESCENT WIND TRU WIND/ALT TRU WIND/ALT ALTN WIND ---°/---/----- ---°/---/----- ---°/--- ---°/---/----- WIND WIND REQUEST ---°/---/----- REQUEST PREV PREV PHASE> ---°/---/----- PHASE> NEXT PHASE> ---°/---/----- <RETURN <RETURN £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 547 AOC FUNCTION 1/2 {} UPLINK F-PLN INIT REQ* TO DATA REQ* WIND DATA REQ* PRINT <RETURN FUNCTION> AOC FUNCTION 1/2 {} UPLINK F-PLN INIT REQ* TO DATA REQ* WIND DATA PRINT <RETURN FUNCTION> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 548: Wind Data Uplink Message

    TRU WIND/ALT 300°/45 AT FL360 WIND REQUEST* PREV PHASE> NEXT PHASE> <RETURN DESCENT WIND TRU WIND/ALT ALTN WIND 320°/40/FL300 300°/35 FL250 300°/30/FL200 WIND 290/20/FL100 REQUEST* PREV 275/25/FL50 PHASE> [ ]°/[ ]/[ <RETURN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 549 141/ H144° BRG144° 0000 153/ DATE UPDATE C144° TRK144° {CANCEL INSERT* D144H} 0002 " / *3130 C356° 0005 250/ FL85 (SPD) (LIM) 0005 *250/ FL100 DEST TIME DIST EFOB EGLL27R 0125 $£ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 550 NOT ALLOWED message. The wind data displayed on the F-PLN B page remains displayed when a downlink request has been transmitted and an uplink response is pending. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 551 Propagation of wind data to downpath WPTs occurs, based on new uplinked cruise wind data. Thus pilot can preview the overall wind model data (uplinked and propagated), for all cruise WPTs, before insertion or cancellation. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 552 DESCENT WIND page at transition to descent, approach, or go- around flight phase, these prompts are automatically cleared and display reverts to the current descent winds. − The WIND REQUEST prompt is not displayed in descent, approach, or go-around flight phases. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 553: Wind Data Uplink Scratchpad Messages

    WIND UPLINK EXISTS A flight plan modification (active or secondary) is attempted when uplink winds are not yet inserted. This message is automatically cleared when the wind uplink is inserted or erased. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 554: Position Report

    It may be sent manually via a prompt on the MCDU (provided AMI option is selected), or, sent in response to a ground request, or, automatically upon crossing a position-reporting fix designated by the ground (in POS uplink message). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 555: Manual Position Report From Prog Page

    EGLL27R 2255 (although AOC function is enabled) − A POS report downlink is currently pending or processing (auto or manual). Pressing [5R] without (*) displayed will trigger NOT ALLOWED scratchpad message (white). AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 556: Manual Position Report From Aoc Function Page

    <RETURN FUNCTION> Horizontal slew key ..Press Select Page 2/2 POSITION RPT prompt is available in AOC FUNCTION 2/2 { } [2R]. REPORT F-PLN RPT SEND* POSI TION RPT SEND* PRINT <RET FUNCTION> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 557: Automatic Position Report

    The PRG downlink cannot be sent manually through a dedicated prompt. However, the message may result from a pilot action (e.g. changing the destination or runway at destination). Only Progress reports relative to the ACTIVE F-PLN are transmitted. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 558: Flight Plan Report

    TO DATA REQ* F-PLN REPORT prompt is available in WIND DATA REQ* [1R]. PRINT <RETURN FUNCTION> AOC FUNCTION 2/2 { } REPORT F-PLN RPT SEND* POSI TION RPT SEND* PRINT <RET FUNCTION> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 559: Performance Data Report

    When displayed, MCDU reverts to the page displayed before the downlink initiation. This message is cleared when the user re-sends a downlink message, whether it is the same message or not. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 560 MULTIPHASE DATA LINK PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 561 Flight Plan Init Report ..........10 Take Off Data report ........... 11 Wind Data report ............12 Preflight Report ............13 Inflight Report............15 Postflight Report............17 Secondary Preflight Report........... 18 Secondary Inflight Report ..........20 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 562 MULTI PHASE PRINT FUNCTION PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 563: Overview

    REPORTS F-PLN INIT TO DATA WIND DATA PREFLIGHT INFLIGHT ( 1 ) POSTFLIGHT SEC F-PLN (1) POST-FLIGHT report remains printable until INIT page FROM/TO [1R] is completed. (2) If destination data modified. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 564: Access To Print Function

    (OPC option), auto-print function is not available; all AUTO fields are blank. <RETURN FUNCTION> Screens shown are examples. PRINT FUNCTION 1/2 {} MANUAL F-PLN INIT PRINT* TO DATA PRINT* WIND DATA PRINT* <RETURN FUNCTION> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 565 *YES PREFLIGHT PRINT INFLIGHT PRINT *YES POSTFLIGHT PRINT SEC F-PLN PRINT* <RETURN FUNCTION> PRINT FUNCTION 2/2 {} AUTO MANUAL *YES PREFLIGHT PRINT* INFLIGHT PRINT *YES POSTFLIGHT PRINT SEC F-PLN PRINT* <RETURN FUNCTION> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 566: Auto-Print

    − At engine Start for Preflight report, F-PLN INIT PRINT* − When switching to Take Off phase TO DATA PRINT* for In-flight report, − At engine Shutdown for the Post- WIND DATA PRINT* flight report. <RETURN FUNCTION> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 567: Sec F-Pln Print

    {COPY ACTIVE <SEC F-PLN PERF> Two types of print report are available: {DELETE SEC − Secondary Pre-flight Report in *ACTIVATE SEC PREFLIGHT phase, SEC F-PLN − Secondary In-flight Report during other PRINT* phases. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 568: Error Messages

    AVAILABLE" s-pad msg (white) is displayed; (*) prompt reappears. <RETURN FUNCTION> PRINT FUNCTION 1/2 {} AUTO MANUAL *YES F-PLN INIT PRINT* TO DATA PRINT* WIND DATA PRINT* <RETURN FUNCTION> PRINTER NOT AVAILABLE J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 569 MULTI PHASE PRINT FUNCTION 9 10.3. REPORT PRINT-OUT The following pages show samples of various reports. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 570: Flight Plan Init Report

    COST INDEX : NNN IDLE FACTOR: SN.N CRZ ALT : FLNNN ZFWCG : NN.N CRZ TEMP : SNN : NNN.N CLB TRANS : AAAAA BLOCK : NNN.N TROPOPAUSE : AAAAA TAXI : NN.N ================================================================ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 571: Take Off Data Report

    : NNN : NNN : NNN : NNN : NNN : NNN THR RED ALT : AAAAA BARO : ANN.NN or ACC ALT : AAAAA ANNNN EO ACC ALT : AAAAA ================================================================ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 572: Wind Data Report

    DESCENT WINDS ------------- T. WIND/ALT DDD'/MMM/FLNNN 042'/055/FL250 044'/049/FL190 050'/035/02500 060'/020/GRND DEST DATA --------- : 1013 or 29.92 TEMP : +10' MAG WIND : 058'/020 TRANS ALT : 4000 ALTERNATE WIND -------------- 040'/040/FL260 ================================================================ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 573: Preflight Report

    : NNN.N ALTN : NNN.N : NNN.N FINAL : NNN.N NN.N% EXTRA : NNN.N ------------------- BLOCK NN.N MISC PERF DATA --------------- TROPOPAUSE : AAAAA CLB TRANS : AAAAA CRZ TEM : SNN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 574 FMS 1 P/N STATUS FMS 2 P/N STATUS ---------------- ---------------- FMS SOFTWARE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx NAV DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM AIRLINE CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM OPTIONS CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx PERF DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx ================================================================ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 575: Inflight Report

    WWWWWWW HH:MM NNN/AAAAA NN.NN DDD'/MMM NNN SNN NNNX NNNN WWWWWWW HH:MM NNN/AAAAA NN.NN DDD'/MMM NNN SNN NNNX NNNN FUEL INFORMATION AT HH:MM ------------------------- WEIGHT RSV/RSV% FINAL EXTRA NNN.N NN.N% NNN.N NNN.N/N.N% NNN.N NNN.N AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 576 FMS 1 P/N STATUS FMS 2 P/N STATUS ---------------- ---------------- FMS SOFTWARE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx NAV DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM AIRLINE CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM OPTIONS CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx PERF DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx ================================================================ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 577: Postflight Report

    FMS 1 P/N STATUS FMS 2 P/N STATUS ---------------- ---------------- FMS SOFTWARE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx NAV DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM AIRLINE CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM OPTIONS CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx PERF DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx ================================================================ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 578: Secondary Preflight Report

    : NNN.N ALTN : NNN.N : NNN.N FINAL : NNN.N NN.N% EXTRA : NNN.N ------------------- BLOCK NN.N MISC PERF DATA --------------- TROPOPAUSE : AAAAA CLB TRANS : AAAAA CRZ TEM : SNN J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 579 FMS 1 P/N STATUS FMS 2 P/N STATUS ---------------- ---------------- FMS SOFTWARE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx NAV DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM AIRLINE CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM OPTIONS CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx PERF DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx ================================================================ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 580: Secondary Inflight Report

    FMS 1 P/N STATUS FMS 2 P/N STATUS ---------------- ---------------- FMS SOFTWARE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx NAV DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM AIRLINE CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx FM OPTIONS CONFIG xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx PERF DATABASE xxxxxxxxxxxxxxx xxxxxxxxxxxxxxx ================================================================ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 581 Part IV FMS DEGRADED OPERATIONS AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 582 PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 583 CHECK IRS3/FM POSITION ..........5 NAV ACCUR DOWNGRAD ..........6 IR ALIGNMENT IN ATT MODE ......... 7 4.3. Weights ................ 8 FMS1/FMS2 GW DIFF ............ 8 CHECK GW ..............8 INITIALIZE WEIGHTS............ 8 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 584 FMS DEGRADED OPERATIONS CONTENTS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 585: Chapter 1 - Overview

    If errors are detected the FMS attempts to correct the situation by automatic software resets. If the error cannot be corrected the system is considered failed. It may be latched or reset manually. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 586 SINGLE mode). Note: If FM is failed, FMGC is out of order. MCDU failure Failure may affect the MCDU only. In this case FMGC access is limited to the onside operative MCDU. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 587: Chapter 2 - Fmgc Resets And Failures

    AP & A/THR may MAP NOT AVAIL disconnect and managed modes revert to selected modes (HDG-V/S or TRK/FPA). Use the other AP as necessary. SET OFFSIDE RNG/MODE FMA: Indicates auto- systems degradation. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 588 REC MAX <FMGC (OPP) ----- ----- FL398 <ACARS <REPORT VDEV=- 350 UPDATE AT <AIDS BRG /DIST <CFDS 303° /23.9 EGLL27R REQUIRED ACCUR ESTIMATED RETURN> 1.0NM HIGH 0.28NM SELECT DESIRED SYSTEM INDEPENDENT OPERATION J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 589 Temporarily SELECT a different mode or range on the corresponding EFIS control panel, in order to recover ND display and delete MAP NOT AVAIL and/or SET OFFSIDE RNG/MODE messages. On the opposite side: No action is required. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 590: Automatic Double Reset Of One Fmgc

    AP & A/THR may disconnect and managed modes revert to selected MAP NOT AVAIL modes (HDG-V/S or TRK/FPA). Use the other AP as necessary. FMA: Indicates auto- SET OFFSIDE RNG/MODE systems degradation. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 591 <FMGC (OPP) ----- ----- FL398 <ACARS <REPORT VDEV=- UPDATE AT <AIDS BRG /DIST <CFDS 303° /23.9 EGLL27R PREDICTIVE <GPS GPS PRIMARY REQUIRED ACCUR ESTIMATED RETURN> 1.0NM HIGH 0.28NM SELECT DESIRED SYSTEM INDEPENDENT OPERATION AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 592 MAP NOT AVAIL SECOND NAV DATA BASE and/or SET OFFSIDE RNG/MODE {13NOV-11DEC PILOT STORED messages. 03RTES 00RWYS CHG CODE 00WPTS 00NAVS DELETE ALL} IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> OWN FMGC IN PROCESS J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 593 (white) is displayed on BIG80 1637 129/ " scratchpad. C273° ILL75 1640 " / *2660 DEST DIST EFOB On the opposite side: EGLL27L 1643 OWN FMGC IN PROCESS £$ No action is required AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 594 0.0NM 1.0NM HIGH 0.8NM Caution It is not recommended to perform a manual reset with C/B. Pulling the C/B during the minute following a Double Reset may lead to a “Degraded mode". J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 595: Automatic Triple Reset Of One Fmgc

    SET OFFSIDE RNG/MODE MCDU failed side: The MCDU reverts to the MCDU menu page with: FMGC (OPP) prompt in [1L] field, SELECT DESIRED SYSTEM message (white) on scratchpad. The amber FM FAIL annunciator illuminates. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 596 " C273° used, with OPP FMGC IN PROCESS ILL75 1640 " / *2660 message (amber) on scratchpad. DEST DIST EFOB EGLL27L 1643 Select MCDU pages as desired. OPP FMGC IN PROCESS £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 597 In this case, apply the following procedure: − Pull C/B for 5 seconds, − Wait 1 minute, − Pull again C/B for 5 seconds. − Pull C/B for 12 minutes. On the opposite side: No action is required AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 598: Automatic Single Reset Of Both Fmgcs

    FL398 <ACARS <REPORT VDEV=- 350 UPDATE AT <AIDS BRG /DIST <CFDS 303° /23.9 EGLL27R REQUIRED ACCUR ESTIMATED RETURN> 1.0NM HIGH 0.28NM SELECT DESIRED SYSTEM OWN FMGC IN PROCESS Screens shown are examples J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 599 .... Mode/Range re-select Temporarily SELECT a different mode or range on the corresponding EFIS control panel, in order to recover ND display and delete MAP NOT AVAIL and/or SET OFFSIDE RNG/MODE messages. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 600: Automatic Double Reset Of Both Fmgcs

    <CFDS <CFDS MCDU MENU MCDU MENU <FMGC (OWN) <FMGC (OWN) RETURN> RETURN> <ACARS <ACARS SELEC DESIRED SYSTEM SELEC DESIRED SYSTEM <AIDS <AIDS <CFDS <CFDS RETURN> RETURN> SELECT DESIRED SYSTEM SELECT DESIRED SYSTEM J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 601 − FUEL predictions are lost due to loss of GW, − On PROG page CRZ FL is reset to the FCU value, − On PERF page CI is lost, − Entered speeds are lost. GPS PRIMARY AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 602 − "USING COST INDEX XX" Identify and clear these messages. Perform a FMS re-initialization as described below. Note: Any data entered on one FMGC will be synchronized to the other through the dual mode system. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 603: Fms Re-Initilization

    <A/C STATUS PRINT FUNCTION> FUNCTION> A320-200 CFM56-5-B4 ACTIVE NAV DATA BASE 11DEC-08JAN THV1021301 SECOND NAV DATA BASE {13NOV-11DEC PILOT STORED 03RTES 00RWYS CHG CODE 00WPTS 00NAVS DELETE ALL} IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 604 DIR TO INSERT ....Press 1730 / FL199 The F-PLN page is displayed. BRG 319° 1735 250/ FL62 --F-PLN DISCONTNUITY-- -----END OF F-PLN----- ------NO ALTN F-PLN----- DEST DIST EFOB ---- ---- ---- --.- J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 605 (DECEL) 1841 250/ TMPY TMPY {ERASE INSERT* $£ FROM AEC001 {} SPD/ALT 1730 / FL199 BRG319° 1735 250/ FL62 ---F-PLN DISCONTINUITY-- (DECEL) 1740 250/ EGLL 1740 129/ DEST DIST EFOB EGLL 1740 £$ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 606 GW/CG [2L] ....Insert --.-/--.- 4.37/FF+FQ RTE RSV/% CRZTEMP/TROPO Insert the actual GW and CG. ---.-/ 5.0 ----°/36090 The FMGS is now able to compute FINAL/TIME ---.-/0030 Fuel predictions. EXTRA/TIME ---.-/---- 55.4/25 USING COST INDEX XX message (white) is displayed on scratchpad.
  • Page 607 NAV 1.0 NAV 1.5 NAV 0.4 REQUIRED ACCUR ESTIMATED 1.0NM HIGH 0.28NM <FREEZE NAVAIDS> Use raw data to confirm position. 9. F-PLN PAGE Redefine the flight plan for the remainder of the flight. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 608: Degraded Modes

    FM side. Display is same on both NDs, otherwise SET OFFSIDE RANGE/MODE is displayed on failed side ND. POSITION MONITOR FMGC1 ----.--/-----.-- FMGC2 5116.6N/00007.0E 3IRS/GPS GPIRS 5116.7N/00007.1E MIX IRS 5117.6N/00007.8E IRS1 IRS2 IRS3 NAV 0.8 NAV 1.0 NAV 1.4 <FREEZE NAVAIDS> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 609: Independent Mode

    NAV 0.9 NAV 1.2 NAV 1.6 NAV 0.8 NAV 1.0 NAV 1.4 <FREEZE NAVAIDS> <FREEZE NAVAIDS> − On RAD NAV page navaids tuned on the opposite MCDU are not displayed. Corresponding fields are blank. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 610 − If significant differences exist in the two FMGCs, identify the most accurate and use the associated AP. Caution Airbus does not recommend pulling one FMGC circuit breaker to force the system to operate in SINGLE mode. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 611 A/C must be flown in raw data. RMPs B/Up mode ..Select NAVAIDS ..Manually tuned STBY NAV Consider manual reset one by one of the two FMGCs. If recovered, all pilot-entered data will have been lost. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 612: Map Not Avail Remains Displayed On Nd

    If MAP NOT AVAIL remains displayed on ND with "SET OFFSIDE RNG/MODE" message (amber), EFIS PANEL ........Mode/Range re-select Temporarily SELECT a different mode or range on the corresponding EFIS control panel. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 613: Chapter 3 - Mcdu Anomalies

    − If the FMS is concerned, consider performing a manual FMS reset through the associated C/B. Refer to Airbus FCOM or Operator's Manual for C/B location and procedure. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 614: Fmgc (Timeout)

    <FMGC (SEL) This logic is also available for the <ACARS other subsystems listed on MCDU <AIDS MENU page. <CFDS RETURN> WAIT FOR SYSTEM RESPONSE MCDU MENU <FMGC (TIMEOUT) <ACARS <AIDS <CFDS RETURN> J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 615: Fms Erroneous Predictions

    − Check for erroneous SENSOR INPUT, such FUEL, SAT. If value are different on both sides: − Re-enter Cost Index, which will restart a FMS computation, or − Make a DIR-TO the TO WPT. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 616: Fms Messages

    SECOND NAV DATA BASE FMS1 P/N {04MAY-01JUN THV2040601 PILOT STORED FMS2 P/N 02RTES 00RWYS THV2040602 00WPTS 00NAVS DELETE ALL} IDLE/PERF SOFTWARE +0.0/+0.0 STATUS/XLOAD> <A/C STATUS FMS1/FMS2 A/C STS DIFF <PREV PAGE NEXT PAGE> INDEPENDENT OPERATION J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 617: Sensor Is Invalid

    See Part III – Multiphase procedures for more information. FUEL PRED EFOB EGLL 1658 EHAM 1740 GW / CG 63.7 /25.0 5.75/FF RTE RSV/% CRZTEMP/TROPO 0.1/ 5.0 ----°/35000 FINAL TIME 1.0/0030 EXTRA TIME 0.8/0023 SENSOR IS INVALID AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 618: Fms1/Fms2 Pos Diff

    MIX IRS 5117.6N/00007.8E IRS1 IRS2 IRS3 IRS1 IRS2 IRS3 NAV 0.8 NAV 1.0 NAV 1.4 NAV 0.9 NAV 1.2 NAV 1.6 <FREEZE NAVAIDS> <FREEZE NAVAIDS> FMS1/FMS2 POS DIFF FMS1/FMS2 POS DIFF 5.5L J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 619: Check Irs2/Fm Position

    No pilot action is required on the IRS, unless requested by ECAM. IRS MONITOR <IRS1 <IRS2 <IRS3 IRS2 POSITION 51°16.6N/000°07.0E TTRK 316.6 THDG MHDG 313.4 316.4 WIND GPIRS ACCUR 223°/015 100M GPIRS POSITION 51°16.6N/000°07.0E <FREEZE NEXT IRS> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 620: Nav Accur Downgrad

    NAV ACCURACY DOWNGRAD DESCENT THV001 REC MAX ----- ----- FL398 <REPORT VDEV=- 350 UPDATE AT BRG /DIST 302° /23.5 EGLL27R PREDICTIVE <GPS REQUIRED ACCUR ESTIMATED 1.0NM HIGH 0.92NM NAV ACCURACY UPGRAD NAV ACCURACY UPGRAD J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 621 SET HDG 230.0 Relevant IRS page shows entered IRS 2 POSITION heading, other data are dashed. --°--.--/---°--.-- TTRK ---.- THDG ---.- 230.0 WIND GPIRS ACCUR ---°/--- ----- GPIRS POSITION --°--.--/---°--.-- {FREEZE NEXT IRS> AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 622: Weights

    FUEL PRED page ...Select EGLL 1658 EHAM 1740 GW [3L] ......Enter GW / CG __._ /25.0 5.75/FF+FQ RTE RSV/% CRZTEMP/TROPO 0.1/ 5.0 ----°/35000 FINAL TIME 1.0/0030 EXTRA TIME 0.8/0023 INITIALIZE WEIGHTS J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 623 Part V APPENDICES AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 624 PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 625 Chapter 3 – FMS RESETS SUMMARY Chapter 4 – OPC and AMI files Chapter 5 – ND SYMBOLS 5.1. NAVIGATION LATERAL SYMBOLS .........3 5.2. VERTICAL AND PERFORMANCE SYMBOLS ......5 Chapter 6 - ABBREVIATIONS AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 626 APPENDICES CONTENT PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 627 TYPE II messages – Conditions for display......4 1.3. MESSAGE DELETION ..........5 1.4. PFD FM MESSAGES............. 6 1.5. ND FM MESSAGES ............6 Center of ND..............6 Bottom of ND ............... 7 1.6. MCDU SCRATCHPAD MESSAGES ......... 8 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 628 APPENDICES MESSAGES PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 629: General Display Conditions

    FMS is active system and an important message (amber ones) has been sent. Press the MCDU MENU key and the line select key adjacent to the FMGC prompt to return to the FMGS pages. AIRBUS A318/319/320/321 J43126AA 00...

  • Page 630: Type Ii Messages - Conditions For Display

    − A Type II message, generated while data or a Type I message is occupying the scratchpad, is displayed only when the scratchpad is cleared. If a Type II message is cleared from the scratchpad, then the next one in the queue is displayed. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 631: Message Deletion

    DONE flight phase. Other messages may be displayed during DONE phase if appropriate. Messages, which are displayed on both scratchpad and PFD/ND are cleared simultaneously when cleared from scratchpad, except for GPS PRIMARY LOST. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 632: Pfd Fm Messages

    This message is displaye d when: − The MODE CHANGE or RANGE CHANGE message has been displayed more than six seco − FMGC has failed or − The FMGC has delivered an invalid aircraft position. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 633: Bottom Of Nd

    The pilot can clear this message by pressing the CLR key on the MCDU. GPS PRIMARY LOST (amber, boxed white) (With associated scratchpad message): This message appears when GPS PRIMARY is not available, it cannot be cleared by pilot action. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 634: Mcdu Scratchpad Messages

    − Color: A (amber) / W (white), − Display on PFD/ND, − Y (yes): message is inhibited during takeoff, approach and go-around below 800 ft, − D: Specific Data Link message, − Message definition. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 635 II A D Uplinked F-PLN is valid and processed but the CHECK CO RTE uplink and downlink CO RTE number are different. The message is not displayed if the uplink message is rejected. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 636 The FM uses GPS time and a difference, CLOCK/GPS TIME DIFF greater than 3 mn, exists between the clock time and the GPS time. Automatically cleared if this difference decreases to 1 minute. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 637 FLT NBR UPLINK previous flight number was sent in the downlink message the flight number. II W Y D The state of communication for both ACARS FM DATALINK UNAVAIL buses is NOT READY. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 638 - Less than or equal to 3NM when GPS mode is not active. II W Target speeds computed by the FMGs differ by FMS1/FMS2 SPD TGT DIFF 5KT or more. Pilot entry in a data field exceeds the field FORMAT ERROR width or is of incorrect format or type.
  • Page 639 See Part III - Data Link. II W PFD Displayed on PFD and MCDU when descent MORE DRAG profile cannot be achieved at idle thrust and speed-brakes are needed. See Part II - Descent AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 640 FROM/TO pair, a place defined by place-bearing-distance (PBD) or place- bearing/place-bearing (PB/PB) or an airport, or a waypoint runway, or a navaid, or a navaid frequency (including pilot-defined elements) that is not in the current database. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 641 PROCEDURE RNP IS XX.XX the system value found in the NAV database for the corresponding leg. Also triggered if route or NAV data base RNP value becomes smaller than the entered value. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 642 - EO is no longer active. II W PFD SELECTED speed mode is active and selected SET HOLD SPEED & holding SPD differ by more 5KT with 30 seconds before entering Holding fix. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 643 SYSTEM NOT AVAILABLE installed). II W Y D The Take off data uplink message is validated TAKE OFF DATA UPLINK and accepted. Take off data are available for review in either flight plan. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 644 ZFW on INIT page B, or GW on FUEL PRED page. CI is defaulted to NNN A sub-system is selected while communication WAIT FOR SYSTEM is being attempted prior to display of sub- RESPONSE system menu. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 645 XXXX: NAME OF NAVAID or NUMBER of a XXXX IS DESELECTED SATELLITE Pilot attempts to deselect a navaid or a satellite, which is already de-selected. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 646 APPENDICES MESSAGES PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 647 Abeam reference point (AB) ........... 9 Pseudo-Waypoints ............10 2.2. Flight Plan Markers ..........12 2.3. MCDU prompts ............13 2.4. F-PLN page: lateral defining legs ......14 2.5. Pilot entries: Data format ........19 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 648 APPENDICES MCDU NAMING and DATA FORMAT PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 649: Waypoint Abbreviations

    − MCDU prompts, − DATA FORMAT. 2.1. Waypoint abbreviations NAV data base WPTs NAV data base files are encoded and released by Thales based on data from the operator's provider. NAV data base codification must be compliant with the ARINC 424 specification.

  • Page 650: Pilot-Defined Wpts

    NM, which the letter relates to. Pilot-defined WPTs Certain pilot-entered waypoints in the flight plan are automatically abbreviated. They are LAT/LONG, PLACE/BRG/DIST, PLACE-BRG/PLACE-BRG and PLACE/DIST pilot-defined waypoints, Radial Intercept, and abeam reference points. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 651: Lat/Long (Llxx Or Nxxexxx)

    .79/ FL360 TRK059° LL01 0739 " / " ---F-PLN DISCONTINUITY-- ADABI 0744 .79/ " TMPY TMPY {ERASE INSERT* $£ LAT REV FROM LL01 46°00.0N/001°00.0E NEXT WPT <HOLD ENABLE NEW DEST {ALTN TMPY <F-PLN AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 652 Any time coordinates may be reviewed via LAT REV function at the WPT. NEXT WPT <HOLD ENABLE NEW DEST {ALTN On this page, the example is given for a LL WPT at: TMPY <F-PLN 46°00.0N/001°00.0E J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 653: Place/Brg/Dist (Pbd)

    20, which is not already used for TRK353° PBD02 0923 " / " another pilot defined waypoint abbreviation in that list. ---F-PLN DISCONTINUITY-- ADABI 0927 .79/ " TMPY TMPY {ERASE INSERT* $£ AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 654: Place-Brg/Place-Brg (Pbx)

    20, which is not already used for ADABI 1222 " / " another pilot defined waypoint UN874 30NM abbreviation in that list. BOKNO 1226 " / " TMPY TMPY {ERASE INSERT* $£ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 655: Abeam Reference Point (Ab)

    VANAD 1234 " / " used as for any other waypoint DEST DIST EFOB EGLL27R 1319 identifier. However, this £$ waypoint does not become one of the twenty pilot defined waypoints. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 656: Pseudo-Waypoints

    T/C and T/D pseudo waypoints, where forecast winds are also provided. The SPD LIM, S/C, and S/D pseudo waypoints can be cleared by the CLR key via either the right or left LS key. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 657 (DECEL) Deceleration Starting point of point deceleration for approach. (1) Indicates that the pseudo waypoint may be entered or modified directly on the F-PLN page of the MCDU. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 658: Flight Plan Markers

    ‘Direct To’ with abeam points revision. A discontinuity cannot be cleared between the origin and destination when the origin and destination waypoints are the same, and there are no other lateral defining legs between them. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 659: Mcdu Prompts

    Part III: 3.3 pending 'Direct To' revision. {ERASE {CLB Assigns the entered constraint to the Part III: 4.1 climb segment. DES} Assigns the entered constraint to the Part III: 4.1 descent segment. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

  • Page 660: F-Pln Page: Lateral Defining Legs

    TRK144° D144H} 0002 " / *3130 It indicates access from LAT/VERT C356° revision. WPT represents any 0005 250/ FL85 (SPD) waypoint name. (LIM) 0005 *250/ FL100 DEST DIST EFOB EGLL27R 0122 £$ J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 661 XXX is the inbound course CXXX° to the holding pattern fix. WPT is the holding pattern fix, which may be a fixed waypoint or T-P. L/R is direction of turn. HOLD L AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 662 070° INTCPT intercept termination. H090° DD is the radius of the arc. DDARC WPT is the termination waypoint. XXX is the inbound course PROC to the procedure turn fix INTCPT CXXX° INTCPT J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 663 Turn Point Present Position PPOS Displayed as the FROM waypoint if the A/C is in a discontinuity and does not meet the criteria for activation on the next leg. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 664 (4) Access from either left LS key results in a LAT REV at WPT. (5) Access from left LS key results in a LAT REV at the termination waypoint of the following leg (AF, CF, FA or FM). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 665: Pilot Entries: Data Format

    − For other units, the range should be converted. − When the maximum value of a given range is not specified, it will be defined in OPC file. MCDU PAGE The MCDU pages on which the data may be inserted. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 666 CO RTE XXXXXXXXXX If not in the NAV INIT A ROUTE Up to 10 Data Base, "NOT NEW ROUTE alphanumeric IN DATA BASE" s- characters may be pad msg (white) is entered displayed J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 667 FF + FQ One or both may be FUEL PREDICTION SENSORS entered. Both: /FF + FQ or /FQ + FF Fuel flow: /FF Fuel quantity: /FQ FIG OF MERIT 0 – 3 NEW NAVAID AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 668 Leading zeros may be omitted FREQ. NNN.NN decimal 108.00 – 117.95 PROG RADIO NAV point may be omitted NEW NAVAID if no decimal part J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 669 INIT A Minutes BDDDMM.M DDD: 180° Tenths of DDD: degrees MM.M: 59.9 minutes MM.M: minutes B: Direction Leading zeros may be omitted but the direction (B) is necessary. Longitude is displayed as DDDMM.MB AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 670 LAT REV dash in the middle. PLACE is limited PROG 2 couples have to be to 5 characters NEW WPT entered with “/” DIR TO between the entries J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 671 AAAANND RUNWAY, NEW RUNWAY AAAA is same as NEW NAVAID ARPT NN is runway number (2 digits must be entered) D is L or R or C (Left / Right / Center) AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 672 SNNN or NNNS Same as Flight Same as F-PLN A Flight NNN is in Flight Level or ALT Level or Level, or SNNNNN or NNNNNS NNNNN is in ALT Leading zeros may be omitted J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 673 LAT REV Acceptable as PROG, waypoint Ident, DIR TO ARPT, NAVAID, STEP ALTS PREDICTIVE WAYPOINT, LAT/LONG, VERT REV PLACE.BRG/ SEC INIT A PLACE.BRG PLACE/BRG/DIST PLACE/DIST may be entered to define a waypoint AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 674 - Otherwise, "FORMAT ERROR" s-pad msg is triggered. Note (2): The SHIFT and TO LIMIT values must be consistent (e.g. the runway length remaining shall be less than or equal to the runway length – position shift). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 675 APPENDICES FMS RESETS 1 Part V: Chapter 3 – FMS RESETS SUMMARY Contents AUTO RESET OF ONE FMGC ............ 2 AUTO RESET of BOTH FMGCs..........3 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 676 - Pull C/B for 5 seconds, Not required following a Double Reset this may - Wait 1 minute, lead to a “Degraded mode". - Pull again C/B for 5 seconds. Or Pull C/B for 12 minutes. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 677 Otherwise the current page remains displayed OWN FMGC IN PROCESS message (white) is displayed on scratchpad Data may be re-entered from either MCDU. The second FMGC will synchronize automatically. Select as appropriate MANUAL RESETS Not required AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 678 APPENDICES FMS RESETS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 679: Chapter 4 - Opc And Ami Files

    APPENDICES OPC and AMI FILES 1 Part V: Chapter 4 – OPC and AMI FILES Contents 4.1. OPC FILE..............3 4.2. AMI FILE..............4 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 680 APPENDICES OPC and AMI FILES PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 681 GPS APPROACH default RNP value PRECISION APPROACH default RNP value NON PRECISION APPROACH default RNP value Software DATA Max GW 99,9 99,9 Max RTE RSV 10,0 10,0 tons MAX ZFW 80,0 80,0 MAX BLOCK 80,0 80,0 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 682 Altitude at which the final holding pattern is 1500, 5000, 10000, ft AGL 1500 supposed to be flown 15000, 20000 Final holding pattern is flown at primary or alternate P / A destination J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 683 (N = no default) Y / N Auto-print at Engine shut down default setting (N = no default) Y / N Auto-print at transition to Take Off default setting (N = no default) AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 684 APPENDICES OPC and AMI FILES PAGE INTENTIONALLY BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 685: Chapter 5 - Nd Symbols

    APPENDICES ND SYMBOLS 1 Part V: Chapter 5 – ND SYMBOLS Contents 5.1. NAVIGATION LATERAL SYMBOLS....... 3 5.2. VERTICAL AND PERFORMANCE SYMBOLS ....5 AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 686 APPENDICES ND SYMBOLS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 687: Navigation Lateral Symbols

    The en-route WPTs with label are shown DIBAG in green. TRK/DIST If CSTR is not selected on EFIS control panel, TRK and DIST from the map reference point to the next F-PLN WPT are displayed in magenta. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 688 For shorter range scales and if the procedure turn or the holding pattern is in the next or the active leg, the display shows the full circuit or pattern. J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 689: Vertical And Performance Symbols

    Although the symbol is always displayed, automatic deceleration only occurs if in managed speed, and NAV or approach mode is engaged. White (Option): displayed when the A/C is in HDG mode. AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 690 CIRCLE oriented to the current track line. symbol Represents the Required Distance to Land. Only displayed in the descent and approach phases, when a selected lateral mode is engaged (HDG or TRK). J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.

  • Page 691: Chapter 6 - Abbreviations

    Air Speed Indicator Air Traffic Control Auto Thrust System ATSU Air Traffic Service Unit Attitude AVNCS Avionics Airway BARO Barometric Beat Frequency Oscillator BITE Built-in Test Equipment Bearing Brake Bright Centigrade Circuit Breaker Checklist AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 692 DIR TO Direct To DISC Disconnect DIST Distance Display Management Computer Distance Measuring Equipment Data Management Unit Down Derated take-off DSDL Dedicated Serial Data Link DSPL Display Distance To Go Display Unit J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 693 Course from a FIX FCDC Flight Control Data Concentrator FCMC Fuel Control and Monitoring Computer FCOM Flight Crew Operating Manual FCPC Flight Control Primary Computer FCSC Flight Control Secondary Computer Flight Control Unit Flight Director AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 694 Greenwich Mean Time Ground Global Positioning System GPWS Ground Proximity Warning System GRND Ground Geographic Reference Point GRVTY Gravity Ground speed Gross Weight Hour, Hot Harness Connector Hydraulic Control Unit Heading HDG/S Heading Selected J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 695 Localizer Inertial Smoothing Lock Latitude/Longitude Left-Line Select key LLSK Lest Line Select Key Localizer LONG Longitude Airbus Long Range family (A3330/340) Long Range Cruise LRRA Low Range Radio Altimeter Line Replaceable Unit AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 696 MAP Reference Point MTBF Mean Time Between Failure MTOGW Maximum Take Off Gross Weight MTOW Maximum Takeoff Weight MZFW Maximum Zero Fuel Weight Normal, North Not Applicable Next Page Not Acknowledge Transmission Navigation J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 697 Pilot Non Flying Panel Position PPOS Present Position Pressure PRE FLT Preflight PRED Prediction PROC Procedure PROC T Procedure Turn PROF Profile PROG Progress PROTEC Protection P-SPEED Profile Speed Point Printer Push To Talk AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 698 Required Time of Arrival Route Route Rudder Travel Limit RTOW Regulatory Takeoff Weight Request To Send RVSM Reduced Vertical Separation Minimum Runway Slats Retraction Speed, South Step Climb Step Descent Airbus Single Aisle family (A318/319/320/321) J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 699 Time to intercept To Be Confirmed To Be Determined TCAS Traffic Collision Alert System or Threat-Analysis/Collision Avoidance System TEMP Temperature TFTS Terrestrial Flight Telephone System Target Thrust THR Thrust Trimmable Horizontal Stabilizer AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 700 Minimum Control Speed on Ground VMCL Minimum Control Speed at Landing VMIN Minimum Operating Speed Maximum Operating Speed Minimum Unstick Speed VHF Omnidirectional Range VOR-D VOR-DME VORTAC VOR-TACAN Rotation Speed VREF Landing Reference Speed Stall Speed J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 701 Waypoint Weight Weather Radar XCVR Transceiver Transfer XING Crossing XMTR Transmitter XPDR Transponder Crosstrack Error Yellow Altitude ZFCG Zero Fuel Center of Gravity Zero Fuel Weight ZFWCG Center of Gravity without Fuel AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.
  • Page 702 APPENDICES ABBREVIATIONS PAGE INTENTIONALLY LEFT BLANK J43126AA 00 AIRBUS A318/319/320/321 © THALES AVIONICS S.A.
  • Page 703 FLIGHT MANAGEMENT SYSTEM PILOT'S GUIDE UNFOLD AIRBUS A318/319/320/321 J43126AA 00 © THALES AVIONICS S.A.

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