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GENERAL INFORMATION

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A318/A319/A320/A321FLIGHT CREW

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GENERAL INFORMATIONPRELIMINARY PAGES

TABLE OF CONTENTS

82U A318/A319/A320/A321 FLEET GEN-PLP-TOC P 1/2FCOM 06 MAR 14

Main FCOM Changes..............................................................................................................................................AFCOM Purpose........................................................................................................................................................BList of Effective Sections/Subsections (LESS) - Paper Only.................................................................................. CList of Effective Operations Engineering Bulletins (LEOEB)...................................................................................DList of Effective Documentary Units (LEDU) - Paper Only..................................................................................... EList of Effective Temporary Documentary Units (LETDU) - Paper Only................................................................. FAircraft Allocation Table (AAT) - Paper Only..........................................................................................................GList of Modifications (LOM) - Paper Only............................................................................................................... HFCOM Use and Organization................................................................................................................................... IFCOM Format and Style Information - Paper only..................................................................................................JFCOM Revisions......................................................................................................................................................KAbbreviations............................................................................................................................................................ L


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TABLE OF CONTENTS


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SUMMARY OF HIGHLIGHTS

82U A318/A319/A320/A321 FLEET GEN-PLP-SOH P 1/2FCOM 06 MAR 14

LocalizationTitle

TocIndex

ID Reason

GENFCOM Revisions

K 1 Minor editorial change

Update of the RA term.Documentation update: Deletion of information.

GENAbbreviations

L 2

Addition of the RPCU abbreviation.


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SUMMARY OF HIGHLIGHTS


82U A318/A319/A320/A321 FLEET GEN-PLP-SOH P 2/2FCOM 06 MAR 14


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MAIN FCOM CHANGESIdent.: GEN-00012867.0001001 / 08 FEB 13Applicable to: ALL

The purpose of the Main FCOM Changes is to provide operators with general information about themost significant changes that are introduced in the current revision of the manual.The main FCOM changes are available on the Airbus World portal, under the Flight OperationsCommunity channel - Flight Operations Manuals - Main FCOM / FCTM / MMEL changes.In addition, every revised Documentary Unit (DU) has a revision highlight (HL) that:‐ Indicates the change(s) made to the DU‐ Can be found in the associated “Preliminary Pages – Summary of Highlights” subchapter.In addition to the Main FCOM Changes, the Modification Operational Impact (MOI) documentsavailable on the Airbus World portal (Flight Operations community channel - Operational Material - Modification Operational Impact MOI) provide the operational impact linked to a MOD number.

FCOM PURPOSEIdent.: GEN-00012627.0001001 / 18 NOV 13Applicable to: ALL

FCOM PURPOSEThe Flight Crew Operating Manual (FCOM) is the support documentation for flight crews. Itprovides them with the necessary information about the operational, technical, procedural,and performance characteristics of the Single Aisle aircraft family, to ensure safe and efficientoperations of the aircraft during normal and abnormal/emergency situations, that may occur onground, or in flight.The manual is not designed to provide basic jet aircraft piloting techniques, or information, that areconsidered as basic airmanship for trained flight crews that are familiar with that type of aircraftand with its general handling characteristics.The FCOM is intended to be used:‐ Directly as flight crew operating manual or to provide operators with a basis for their

development of a customized airline operations manual, in accordance with applicablerequirements

‐ As a comprehensive reference guide during initial and refresher flight crew training.Practical and training-oriented information is addressed in the Flight Crew Training Manual(FCTM).Refer to FCTM/OP-10 Introduction . Moreover, the FCOM is not intended to be used forteaching basic piloting skills.

The Flight Crew Operating Manual complements the approved Airplane Flight Manual (AFM).If the data contained in this manual differs from the data in the AFM, the AFM remains thereference.


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82U A318/A319/A320/A321 FLEET GEN P 2/30FCOM ← B to C → 06 MAR 14

For any questions or comments related to this manual, the Operator’s Flight OperationsManagement may contact the Airbus Flight Operations & Training support department.

FCOM CONTENTSThe contents of the FCOM are organized in the following six parts:‐ System Descriptions (DSC, organized by ATA)‐ Procedures

PRO ABN : Abnormal/EmergencyPRO NOR SOP : NormalPRO NOR SRP : System RelatedPRO SPO : Special OperationsPRO SUP : Supplementary

‐ Limitations (LIM)‐ Performance (PER, organized by phase of flight)‐ Operations Engineering Bulletins (OEB)‐ Flight Crew Bulletins (FCB).

DOCUMENTARY UNITSThe FCOM is made of Documentary Units (DU). The DU is the smallest part of information with atechnical content.The DUs are listed on a separate "List of Effective Documentary Units" (LEDU). Refer to theGeneral section.Note: 1. DUs can be grouped into Group of DU (GDU)

2. Temporary information may be provided via Temporary DU (TDU).IDENTIFICATION STRIP

Below the title of the DU, the identification strip provides:‐ The list of MSN the DU is applicable to‐ For TDU, the reference to the DU impacted by the TDU.

LIST OF EFFECTIVE SECTIONS/SUBSECTIONS (LESS) - PAPER ONLYIdent.: GEN-00013786.0001001 / 23 MAR 11Applicable to: ALL

The List of Effective Sections/Subsections (LESS) summarizes all the sections and subsectionscontained in the FCOM. For each revision, a new LESS is issued when at least one DU of thesection/subsection is changed.


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The LESS consists of:‐ The "M" field that may provide the following evolution code:

• The "N" letter indicates a new section introduced by the revision• The "R" letter indicates a section in which the content has been revised• The "E" letter indicates an aircraft validity change within the section• The "M” letter indicates a section that have move within the FCOM

‐ The “Localization” field that allows localizing the section within the manual with the productstructure

‐ The “Subsection title” field‐ The “Rev. Date” field that indicated the date at which the section was changed.

LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETINS (LEOEB)Ident.: GEN-00013787.0001001 / 23 NOV 11Applicable to: ALL

Refer to OEB-GEN Cross Reference Between the Former and New OEB Identifications

LIST OF EFFECTIVE DOCUMENTARY UNITS (LEDU) - PAPER ONLYIdent.: GEN-00013789.0001001 / 23 MAR 11Applicable to: ALL

For each revision, a new List of Effective Documentary Units (LEDU) is issued at the section level.The LEDU provides information about the DU localization, applicability, identification and issue date.The LEDU consists of:‐ The "M" field that may provide the following Evolution Code:

• The "N" letter indicates a new DU introduced by the revision• The "R" letter indicates a revised DU: The content of the DU is updated by the revision. A

vertical line in the margin of the DU locates the modified part• The "E" letter indicates an aircraft validity change for the DU: The list of MSNs for which the DU

is effective has been changed compared to the previous LEDU, by addition or deletion of one orseveral MSN

‐ The “Localization” field that allows localizing the DU in the manual with the product structure of themanual

‐ The "T" field (Temporary Information) that contains a cross if the associated DU is a TDU‐ The "DU title" that provides the title of the DU‐ The “DU identification” that identifies the DU with its own unique identification number or the GDU

with its own unique code.‐ The “DU date” that indicates when the DU has been released


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‐ The DU criteria which lists the technical or operational criteria for which the DU and solution isapplicable to.

‐ The “Applicable to” which provides the list of aircraft this DU and solution is applicable to‐ The “Impacted by TDU” which is the identification of the TDU superseding the DU

LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS (LETDU) - PAPER ONLYIdent.: GEN-00013803.0001001 / 29 MAR 11Applicable to: ALL

The List of Effective Temporary Documentary Units (LETDU) provides a summary of the TemporaryDU impacting the section.The LETDU consists of:‐ The "M" field that may provide the following Evolution Code:

• The "N" letter indicates a new TDU introduced by the revision• The "R" letter indicates a revised TDU: The content of the TDU is updated by the revision. A

vertical line in the margin of the TDU locates the modified part• The "E" letter indicates an aircraft validity change for the TDU: The list of MSNs the TDU is

applicable to has been changed compared to the previous LETDU, by addition or deletion ofone or several MSN

‐ The “Localization” field that allows localizing the TDU in the manual with the product structure ofthe manual

‐ The “TDU Title” that provides the title of the TDU‐ The “TDU identification” that identifies the TDU with its identification number with its own unique

code‐ The “TDU date” that indicates when the TDU has been released‐ The TDU criteria which lists the technical or operational criteria, the it is applicable to‐ The “Applicable to” which provides the list of aircraft this TDU is applicable to‐ The “Impacted DU” which is the Identification of DU superseded by the TDU‐ The “Reason for issue” of the TDUNote: 1. TDU is displayed on a yellow background

2. within the QRH the TDU replaces the impacted DU

AIRCRAFT ALLOCATION TABLE (AAT) - PAPER ONLYIdent.: GEN-00013804.0001001 / 23 MAR 11Applicable to: ALL

The Aircraft Allocation Table (AAT) provides a view of the fleet covered in the FCOM. For eachaircraft, the AAT provides its MSN, its registration number and the model.


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82U A318/A319/A320/A321 FLEET GEN P 5/30FCOM H to I → 06 MAR 14

LIST OF MODIFICATIONS (LOM) - PAPER ONLYIdent.: GEN-00013805.0001001 / 25 MAR 11Applicable to: ALL

The List of Modifications (LOM) lists the criteria (Modification Proposal (MP) or Service Bulletins(SB)) which the installation on the aircraft affects the FCOM.Note: Each MP has one or more associated MODs. The MP/MOD correlation is available in

AirN@v / Engineering.The LOM also indicates:‐ The title of the criteria‐ The date of incorporation of the criteria in the FCOM‐ The list of aircraft that have the criteria‐ The "M" field that may indicate the following evolution code

‐ The "E" letter indicates an aircraft validity change of the criteria. The list of aircraft to which thecriteria applies has changed compared to the previous FCOM revision, by addition or deletion ofone or several aircraft.

‐ The "N" letter indicates new criteria added by this FCOM revision‐ The "R" letter indicates a change in the criteria title or associated SB

FCOM USE AND ORGANIZATIONIdent.: GEN-00012688.0001001 / 23 MAR 11Applicable to: ALL

DEFINITIONS OF WARNINGS, CAUTIONS AND NOTESThe following are the official definitions of warnings, cautions and notes taken directly from theJAR25/CS-25 and applicable to Airbus flight operation documentation:WARNING An operating procedure, technique, etc. that may result in personal injury or

loss of life if not followed.CAUTION An operating procedure, technique, etc. that may result in damage to

equipment if not followed.NOTE An operating procedure, technique, etc. considered essential to emphasize.

Information contained in notes may also be safety related.


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82U A318/A319/A320/A321 FLEET GEN P 6/30FCOM ← I to J → 06 MAR 14

INFORMATION TYPE AND LAYERSThe FCOM has technical information that may be used for:‐ Flight crew operations in flight, or on ground‐ Airlines operations on ground‐ Training.To take the above-noted objectives into account, the FCOM is organized in three layers as follows:‐ Layer 1: "Need to know"

Layer 1 presents information that is necessary in the cockpit.‐ Layer 2: "Nice to know"

Layer 2 presents information that is used as a reference, in order to fully understand the logic ofthe aircraft and pilot interfaces.

‐ Layer 3: Detailed informationLayer 3 provides more detailed explanations, that are not necessarily needed in flight.

Note: For paper only, the following examples show the visual characteristics of each kind oflayer

EXAMPLE ‐ Text in layer 1Layer 1 is the default layer. No symbology when not following layer 2 or layer 3information.

L2 EXAMPLE ‐ Text in layer 2

L3 EXAMPLE ‐ Text in layer 3

L1 EXAMPLE ‐ Text in layer 1 (as this text follows a text in layer 2 or 3, symbology "L1")

OPTIONAL EQUIPMENTThe legend (if installed) indicates that a paragraph or a schematic is applicable only if therelated equipment is installed.

FCOM FORMAT AND STYLE INFORMATION - PAPER ONLYIdent.: GEN-00013793.0001001 / 08 FEB 13Applicable to: ALL

TABLE OF CONTENTSEach TOC entry has an alphabetical index that identifies this TOC entry within its subsection. Themanual user can easily find a TOC entry content within the manual thanks to this alphabetical


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index and the subsection identification. Both are indicated in the TOC and both cross-refer to thepaper page footer (see the TOC indexing part below).

HEADER AND FOOTER


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82U A318/A319/A320/A321 FLEET GEN P 8/30FCOM ← J → 06 MAR 14

1. Airline logo2. Aircraft types and manual3. Level 2 chapter (PSL level 2 : GEN, DSC, PRO, LIM, OEB, FCB, PER)4. Level 3 chapter5. Level 4 chapter6. Revision mark7. Key product (document identification and aircraft designation)8. Key product (manual code)9. Page index10. Last evolution date11. Identification strip (list of impacted aircraft)12. PSL pathREVISION MARK

In the paper format, a vertical bar in the margin of the DU identifies the modified part. Eachvertical bar has a numerical index that refers to the associated reason of the change in theSummary of Highlight.This Summary of Highlight lists all the changes and associated reasons of the change (ifnecessary) that the revision has introduced.

TOC INDEXINGIn the paper page footer, the TOC indexing is of the following type:

A : The paper page contains the whole "A" TOC entry contentA to B : The paper page contains the whole "A" and "B" TOC entries contentsA → : The "A" TOC entry content starts on this paper page and continues on

the following paper page← A : The "A" TOC entry content starts on a previous paper page and finishes

on this paper page← A → : The "A" TOC entry content starts on a previous paper page and

continues on the following paper pageA to C→ : The paper page contains the whole "A" and "B" TOC entries contents

but the "C" TOC entry content starts on this paper page and continueson the following paper page


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← A to C : The paper page contains the whole "B" and "C" TOC entries contentsbut the "A" TOC entry content starts on a previous paper page andfinishes on this paper page

← A to C → : The paper page contains the whole "B" TOC entry content but the "A"TOC entry content starts on a previous paper page and finishes on thispaper page and the "C" TOC entry content starts on this paper page andcontinues on the following paper page

Note: 1. The indexes follow the alphabetical order: A, B, C, ..., Z, AA, AB, AC, ..., AZ, BA,BB, BC, ...

2. For each subsection, the index starts again from A.3. When a TOC entry content continues on the following paper page, the text

"Continued on the following page" is also indicated.

FCOM REVISIONSIdent.: GEN-00012634.0001001 / 17 JAN 14Applicable to: ALL

FCOM REVISIONFCOM revisions are issued to add, update, or revise information. The Operator determines therevision periodicity.When necessary, a revision may be issued in between the defined periodicity (e.g. need for urgentupdate).A vertical bar appears to the left of all revised parts of the manual.

TEMPORARY INFORMATIONSome FCOM sections may need a temporary update (e.g. to explain a system behavior that willbe modified by a future standard). In such cases, the applicable FCOM section is updated with aTemporary Documentary Unit (TDU).Information contained in the TDU is highlighted in the manual and the initial content of the FCOMremains available for consultation and comparison and is highlighted (identification strip) as beingimpacted by the TDU.A List of Effective Documentary Units (LEDU) is provided in the FCOM

1 OPERATIONS ENGINEERING BULLETINSOperations Engineering Bulletins (OEB) are issued, when it is necessary, to rapidly transmittechnical and procedural information.The OEB chapter provides a list of all applicable OEBs.


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82U A318/A319/A320/A321 FLEET GEN P 10/30FCOM ← K to L → 06 MAR 14

FLIGHT CREW BULLETINSFlight Crew Bulletins (FCB) are issued, when it is necessary, to transmit complementary technicalor operational information.The FCB chapter provides a list of all applicable FCBs.

ABBREVIATIONSIdent.: GEN-00012598.0001001 / 25 FEB 14Applicable to: ALL

AAbbreviation Term

A>B A is greater than BA≥B A is greater than or equal to BA<B A is less than BA≤B A is less than or equal to BA/BRK AutobrakeA/C AircraftA/P AutopilotAP AutopilotA/S AirspeedA/SKID Anti-skidA/THR Auto ThrustAA Airworthiness AuthoritiesAB AbortABCU Alternate Braking Control UnitABN AbnormalABV AboveAC Alternating CurrentACARS ARINC Communication Addressing and Reporting SystemACAS Airbrone Collision Avoidance SystemACCEL AccelerationACC Active Clearance ControlACCU AccumulatorACP Audio Control PanelACSC Air Conditioning System ControllerACT Additional Center TankADF Automatic Direction FinderADIRS Air Data Inertial Reference SystemADIRU Air Data Inertial Reference UnitADM Air Data ModuleADR Air Data Reference

Continued on the following page


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Continued from the previous pageAbbreviation Term

ADS-B Automatic Dependent Surveillance-BroadcastADV AdvisoryAEVC Avionic Equipment Ventilation ControllerAFM Airplane Flight ManualAFS Auto Flight SystemAGL Above Ground LevelAIDS Aircraft Integrated Data SystemAIL AileronAIME Autonomous Integrity Monitoring ExtrapolationAIU Audio Interface UnitALT AltitudeALTN AlternateAMI Airline Modifiable InformationAMU Audio Management UnitANT AntennaAOA Angle of AttackAOC Airline Operational ControlAPP ApproachAPPR ApproachAPPU Assymetry Position Pick-off UnitAPU Auxiliary Power UnitAR Authorization RequiredARINC Aeronautical Radio IncorporatedARN Aircraft Registration NumberARP Aerospace Recommended PracticeARPT AirportASAP As Soon As PossibleASI Air Speed IndicatorASP Audio Selector PanelATC Air Traffic ControlATM Air Traffic ManagementATN Aeronautical Telecommunications NetworkATE Automatic Test EquipmentATIS Airbus Technical Information SystemATS Auto Thrust SystemATSAW Airbrone Traffic Situational AwarenessATSU Air Traffic Service UnitATT AttitudeAUTO AutomaticAVNCS AvionicsAWY Airway


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BAbbreviation Term

B/C Back CourseBARO BarometricBAT BatteryBCL Battery Charge LimiterBCDS Bite Centralized Data SystemBCU Backup Control UnitBDDV Brake Dual Distribution ValveBITE Built-In Test EquipmentBIU BITE Interface UnitBFE Buyer Furnished EquipmentBFO Beat Frequency OscillatorBMC Bleed Monitoring ComputerBNR BinaryBRG BearingBRK BrakeBRT BrightBSCU Braking Steering Control UnitBTC Bus Tie ContactorBTL BottleBUS Busbar

CAbbreviation Term

C/B Circuit BreakerCB Circuit BreakerC/L ChecklistCL ChecklistCAB CabinCAPT Captain, CaptureCAS Calibrated AirspeedCAT CategoryCBMS Circuit Breaker Monitoring SystemCCD Cursor Control DeviceCDL Configuration Deviation ListCDLS Cockpit Door Locking SystemCDSS Cockpit Door Surveillance SystemCDU Control Display UnitCF Cost of FuelCFDIU Centralized Fault Display Interface Unit



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CFDS Centralized Fault Display SystemCG Center of GravityCHAN ChannelCHG ChangeCHK CheckCI Cost IndexCIDS Cabin Intercommunication Data SystemCKPT CockpitCLB ClimbCLR ClearCLSD ClosedCM1(2) Crewmember 1 (left seat) or 2 (right seat)CM1 Crewmember 1 (left seat)CM2 Crewmember 2 (right seat)CMPTR ComputerCMS Constant Mach SegmentCMS Centralized Maintenance SystemCNSU Cabin Network Server UnitCO CompanyCO RTE Company RouteCOND ConditioningCONF ConfigurationCONT ContinuousCPC Cabin Pressure ControllerCPCU Cabin Pressure Controller UnitCPDLC Controller-Pilot Data Link CommunicationCRC Continuous Repetitive ChimeCRG CargoCRS CourseCRT Cathode Ray TubeCRZ CruiseCSAS Conditioned Service Air SystemCSCU Cargo Smoke Control UnitCSD Constant Speed DriveCSM/G Constant Speed Motor/GeneratorCSTR ConstraintCT Cost of TimeCTL ControlCTL PNL Control PanelCTR CenterCVR Cockpit Voice Recorder


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DAbbreviation Term

DA Drift AngleDAC Digital to Analog ConverterDAR Digital AIDS RecorderDC Direct CurrentDCDU Datalink Control and Display UnitDCL Digital Cabin LogbookDDRMI Digital Distance and Radio Magnetic IndicatorDECEL DecelerationDES DescentDEST DestinationDET Detection, DetectorDFA Delayed Flap ApproachDFDR Digital Flight Data RecorderDH Decision HeightDIR DirectionDIR TO Direct ToDISC DisconnectDISCH DischargeDIST DistanceDITS Digital Information Transfer SystemDIV DiverterDMC Display Management ComputerDME Distance Measuring EquipmentDMU Data Management Unit (Aids)DN DownDSDL Dedicated Serial Data LinkDTG Distance To GoDTO Derated TakeoffDU Display UnitDU Documentary Unit

EAbbreviation Term

EWD Engine/Warning DisplayECAM Electronic Centralized Aircraft MonitoringECAS Emergency Cockpit Alerting SystemECB Electronic Control Box (APU)ECM Engine Condition MonitoringECON Economic



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ECP ECAM Control PanelECS Environmental Control SystemECU Engine Control UnitEDP Engine-Driven PumpEEC Electronic Engine ComputerEFB Electronic Flight BagEFCS Electronic Flight Control SystemEFIS Electronic Flight Instruments SystemEFOB Estimated Fuel On BoardEGPWS Enhanced Ground Proximity Warning SystemEGT Exhaust Gas TemperatureEIS Electronic Instruments SystemEIU Engine Interface UnitELAC Elevator Aileron ComputerELEC ElectricsELT Emergency Locator TransmitterELEV ElevatorELV ElevationEMER EmergencyEMER GEN Emergency GeneratorENG EngineEO Engine-OutEOSID Engine-Out Standard Instrument DepartureEPE Estimated Position Error (equal to EPU)EPR Engine Pressure RatioEPU Emergency Power UnitEPU Estimated Position Uncertainty (equal to EPE)EROPS Extended Range OperationESS EssentialEST EstimatedETA Estimated Time of ArrivalETE Estimated Time EnrouteETOPS Extended Twin OperationsETP Equal Time PointEVMU Engine Vibration Monitoring UnitE/WD Engine/Warning DisplayEXP ExpediteEXT PWR External PowerEXTN Extension


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FAbbreviation Term

F FuelFAA Federal Aviation AdministrationFAP Forward Attendant PanelF/C Flight CrewF/O First OfficerFO First OfficerFAC Flight Augmentation ComputerFADEC Full Authority Digital Engine Control SystemFAF Final Approach FixFAP Forward Attendant PanelFAR Federal Aviation RegulationsFAV Fan Air ValveFCDC Flight Control Data ConcentratorFCMS Fuel Control and Monitoring SystemFCOM Flight Crew Operating ManualFCU Flight Control UnitFD Flight DirectorFDIMU Flight Data Interface and Management UnitFDIU Flight Data Interface UnitFDU Fire Detection UnitFEP Final End PointFF Fuel FlowFG Flight GuidanceFGC Flight Guidance ComputerF-G/S FLS Glide SlopeFIDS Fault Isolation and Detection SystemFL Flight LevelFLHV Fuel Lower Heating ValueF-LOC FLS LocalizerFLP FlapFLS FMS Landing SystemFLT FlightF/CTL Flight ControlFLT CTL Flight ControlFLXTO Flexible TakeoffFM Flight ManagementFMA Flight Mode AnnunciatorFMGC Flight Management and Guidance ComputerFMGS Flight Management and Guidance System



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FMS Flight Management SystemFNL FinalFOB Fuel On BoardFOM Figure Of MeritFPA Flight Path AngleF-PLN Flight PlanFPD Flight Path DirectorFPPU Feedback Position Pick-off UnitFPV Flight Path VectorFQI Fuel Quantity IndicationFQU Fuel Quantity UnitFREQ FrequencyFRT FrontFRV Fuel Return ValveFU Fuel UsedFWC Flight Warning ComputerFWD ForwardFWS Flight Warning System

GAbbreviation Term

G/S GlideslopeGA Go-AroundGAPCU Ground and Auxiliary Power Control UnitGBAS Ground Based Augmentation SystemGCU Generator Control UnitGDU Group of Documentary UnitGEN GeneratorGES Ground Earth StationGLC Generator Line ContactorGLS GBAS Landing SystemGLS GNSS Landing SystemGMT Greenwich Mean TimeGND GroundGND TEMP Ground TemperatureGPCU Ground Power Control UnitGPIRS Global Positioning and Inertial Reference SystemGPS Global Positioning SystemGPWS Ground Proximity Warning SystemGRND Ground



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GRP Geographic Reference PointGRVTY GravityGS Ground SpeedGW Gross Weight

HAbbreviation Term

HC Harness ConnectorHCU Hydraulic Control UnitHDG HeadingHDG/S Heading SelectedHDL HandleHF High FrequencyHI HighHLD HoldHM Holding Pattern with a Manual TerminationHMU Hydrau-Mechanical UnitHMS Heat Management SystemHP High PressureHPA HectopascalHPV High Pressure ValveHUD Head Up DisplayHYD Hydraulic

IAbbreviation Term

I/O Inputs/OutputsI/P Input or Intercept ProfileIAF Initial Approach FixIAS Indicated AirspeedIATA International Air Transport AssociationICAO International Air Transport OrganizationIDENT IdentificationIDG Integrated Drive GeneratorIFE In Flight EntertainmentIFR Instrument Flight RulesIGGS Inert Gas Generation SystemIGN IgnitionILS Instrument Landing SystemIM Inner Marker



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IMM ImmediateINB InboundINBO InboardINCREM IncrementINIT InitializationINOP InoperativeINR InnerINST InstrumentINTCP InterceptINV InverterIP Intermediate PressureIPC Intermediate Pressure Check valveIPPU Instrumentation Position Pick-off UnitIR Inertial ReferenceIRS Inertial Reference SystemISA International Standard AtmosphereISDU Initial System Display UnitISIS Integrated Standby Instrument SystemISOL IsolationISPSS In Seat Power Supply System

JAbbreviation Term

KAbbreviation Term

LAbbreviation Term

L/G Landing GearLAF Load Alleviation FunctionLAT LatitudeLAT REV Lateral RevisionLAV LavatoryLCD Liquid Crystal DisplayLCN Load Classification Number

Landing Distance AvailableLDA Localizer Directional AidLDG LandingLDS Laptop Docking Station



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LED Light Emiting DiodeLEDU List of Effective Documentary UnitsLEFCB List of Effective Flight Crew BulletinsLEOEB List of Effective Operations Engineering BulletinsLESS List of Effective Section/SubsectionsLF Low FrequencyLGCIU Landing Gear Control Interface UnitLGPIU Landing Gear Position Indicator UnitLH Left-HandLIM LimitationLIS Localizer Inertial SmoothingLK LockLL Latitude/LongitudeLLS Left-Line Select keyLO LowLOC LocalizerLONG LongitudeLP Low PressureLRRA Low Range Radio AltimeterLRU Line Replaceable UnitLS LoudspeakerLSK Line Select KeyLVL LevelLVL/CH Level ChangeLVR LeverLW Landing Weight

MAbbreviation Term

MABH Minimum Approach Break-off HeightMAC Mean Aerodynamic ChordMAG MagneticMAG DEC Magnetic DeclinationMAG VAR Magnetic VariationMAINT MaintenanceMAN ManualMAP Missed Approach PointMAX MaximumMAX CLB Maximum ClimbMAX DES Maximum Descent



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MAX END Maximum EnduranceMC Master CautionMCDU Multipurpose Control and Display UnitMCT Maximum Continuous ThrustMCU Modular Concept UnitMDA Minimum Descent AltitudeMDDU Multifunction Disk Drive UnitMDH Minimum Descent HeightMECH MechanicMEA Minimum En Route AltitudeMED MediumMEL Minimum Equipment ListMFA Memorized Fault AnnunciatorMIN MinimumMKR MarkerMLA Maneuver Load AlleviationMLS Microwave Landing SystemMLW Maximum Landing WeightMM Middle MarkerMMEL Master Minimum Equipment ListMMO Maximum Operating MachMMR Multi Mode ReceiverMN Mach numberMORA Minimum Off Route AltitudeMRIU Maintenance and Recording Interface UnitMSA Minimum Safe AltitudeMSG MessageMSL Mean Sea LevelMSU Mode Selector UnitMTBF Mean Time Between FailureMTOW Maximum Takeoff WeightMZFW Maximum Zero Fuel Weight

NAbbreviation Term

N/A Not ApplicableNA Not ApplicableN1 Low Pressure Rotor Speed (in %)N2 High Pressure Rotor Speed (in %)NACA National Advisory Committee for Aeronautics



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NAV NavigationNAVAID Navigation AidNCD Non Computed DataND Navigation DisplayNDB Non Directional BeaconNLG Nose Landing GearNORM NormalNW NosewheelNWS Nosewheel Steering

OAbbreviation Term

O/P OutputOANS On-board Airport Navigation SystemOAT Outside Air TemperatureOBRM On Board Replaceable ModuleOEB Operations Engineering BulletinOFF/R Off ResetOFST OffsetOIS Onboard Information SystemOIT Onboard Information TerminalOM Outer MarkerOP OpenOPP OppositeOPS OperationsOPT OptimumOUTB OutboundOUTR OuterOVBD OverboardOVHD OverheadOVHT OverheatOVRD OverrideOVSPD OverspeedOXY Oxygen

PAbbreviation Term

P/N Part NumberPN Part NumberPA Passenger Address



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P-ALT Profile AltitudePAX PassengerPBE Portable Breathing EquipmentP-CLB Profile ClimbPCU Power Control UnitP-DES Profile DescentPDB Performance Data BasePDU Pilot Display UnitPERF PerformancePES Passenger Entertainment SystemPF Pilot FlyingPFD Primary Flight DisplayPHC Probes Heat ComputerP-MACH Profile MachPNF Pilot Non FlyingPNL PanelPOB Pressure Off BrakePOS PositionPPOS Present PositionPPU Position Pick-off UnitPR PressurePRED PredictionPRESS Pressure, PressurizationPROC ProcedurePROC T Procedure TurnPROF ProfilePROG ProgressPROTEC ProtectionP-SPEED Profile SpeedPSL Product Structure LevelPSU Passenger Service UnitPT PointPTR PrinterPTT Push To TalkPTU Power Transfer Unit (Hydraulic)PVI Paravisual IndicatorPWR PowerPWS Predictive Windshear System


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QAbbreviation Term

QAR Quick Access RecorderQFE Field Elevation Atmosphere PressureQFU Runway HeadingQNE Sea Level Standard Atmosphere Pressure (1013 hPa)QNH Sea Level Atmosphere PressureQRH Quick Reference HandbookQT Quart (US)QTY Quantity

2 RAbbreviation Term

R/I Radio/InertialRA Radio AltimeterRA Resolution AdvisoryRACC Rotor Active Clearance ControlRAD RadioRAIM Receiver Autonomous Integrity MonitoringRAT Ram Air TurbineRATC Remote ATC BoxRCDR RecorderRCL RecallRCVR ReceiverREAC ReactiveREC RecommendedRED ReductionREG RegulationREL ReleaseREV ReverseRH Right-HandRLSK Right Line Select KeyRMI Radio Magnetic IndicatorRMP Radio Management PanelRNAV Area NavigationRNG RangeRNP Required Navigation PerformanceROP Runway Overrun ProtectionROPS Runway Overrun Prevention SystemROW Runway Overrun WarningRPCU Residual Pressure Control Unit



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RPM Revolution Per MinuteRPTG RepeatingRQRD RequiredRSV ReservesRTE RouteRTL Rudder Travel LimitRTO Rejected TakeoffRTOW Regulatory Takeoff WeightRUD RudderRVSM Reduced Vertical Separation MinimumRWY Runway

SAbbreviation Term

S SouthS/C Step ClimbS/D Step DescentS/D Shut DownS/F Slats/FlapsS/N Serial NumberSN Serial NumberSAAAR Special Aircrew and Aircraft Authorization RequiredSAT Static Air TemperatureSATCOM Satellite CommunicationSC Single ChimeSCP Software Control PanelSD System DisplaySDAC System Data Acquisition ConcentratorSDCU Smoke Detection Control UnitSDF Simplified Directional FacilitySEC Spoiler Elevator ComputerSEL SelectorSFCC Slat/Flap Control ComputerSFE Seller-Furnished EquipmentSID Standard Instrument DepartureSIM SimulationSLT SlatSPD SpeedSPD LIM Speed LimitSPLR Spoiler



OPERATING MANUAL

GENERAL INFORMATION



SRS Speed Reference SystemSTAR Standard Terminal Arrival RouteSTAT StaticSTAT INV Static InverterSTBY StandbySTD StandardSTEER SteeringSTRG SteeringSTS StatusSWTG SwitchingSYNC SynchronizeSYS System

TAbbreviation Term

T.O TakeoffT/O TakeoffTO TakeoffT/C Top of ClimbT/D Top of DescentTA Traffic AdvisoryTAC Taxiing Aid CameraTACAN Tactical Air NavigationTACT TacticalTAS True Air SpeedTAT Total Air TemperatureTAU Time to interceptTBC To Be ConfirmedTBD To Be DeterminedTCAS Traffic Collision Alert System or Threat-Analysis/Collision Avoidance SystemTDU Temporary Documentary UnitTEMP TemperatureTFTS Terrestrial Flight Telephon SystemTGT TargetTHR ThrustTHS Trimmable Horizontal StabilizerTK TankTK Track angleTKE Track Angle ErrorTLA Throttle Lever Angle



OPERATING MANUAL

GENERAL INFORMATION



TLU Travel Limitation UnitTMR TimerTOGA Takeoff - Go-AroundTOGW Takeoff Gross WeightTOW Takeoff WeightT-P Turn PointTPIS Tire Pressure Indicating SystemTR Transformer RectifierT-R Transmitter-ReceiverTRANS TransitionTRK TrackTROPO TropopauseTRU Transformer Rectifier UnitTRV TravelTSM Trouble Shooting ManualTTG Time to GoTVMC Minimum Control Speed TemperatureTWY Taxiway

UAbbreviation Term

UFD Unit Fault DataULB Underwater Locator BeaconUNLK UnlockUP Up, UpperUTC Universal Coordinated Time

VAbbreviation Term

V/S Vertical SpeedV1 Decision SpeedV2 Takeoff Safety SpeedVAPP Approach SpeedVBV Variable Bypass ValveVC Calibrated airspeedVDEV Vertical DeviationVEL VelocityVERT VerticalVERT REV Vertical RevisorVFE Maximum Speed for each Flap configuration



OPERATING MANUAL

GENERAL INFORMATION



VFEN VFE NextVFTO Final Takeoff SpeedVHF Very High FrequencyVHV Very High VoltageVIB VibrationVIP Vertical Intersection PointVLE Maximum Landing Gear Extended SpeedVLS Lowest Selectable SpeedVLV ValveVM Maneuvering SpeedVMAX Maximum Allowable SpeedVMCA Minimum Control Speed in the AirVMCG Minimum Control Speed on GroundVMCL Minimum Control Speed at LandingVMIN Minimum Operating SpeedVMO Maximum Operating SpeedVMU Minimum Unstick SpeedVOR VHF Omnidirectional RangeVOR-D VOR-DMEVR Rotation SpeedVREF Landing Reference SpeedVSI Vertical Speed IndicatorVSV Variable Stator VaneVU Visual Unit

WAbbreviation Term

WARN WarningWBC Weight and Balance ComputerWBS Weight and Balance SystemWGD Windshield Guidance DisplayWHC Window Heat ComputerWNDW WindowWPT WaypointWSHLD WindshieldWT WeightWTB Wing Tip BrakeWXR Weather Radar


OPERATING MANUAL

GENERAL INFORMATION

82U A318/A319/A320/A321 FLEET GEN P 29/30FCOM ← L 06 MAR 14

XAbbreviation Term

XBLD CrossbleedXCVR TransceiverXFR TransferXMTR TransmitterXPDR TransponderXTK Crosstrack Error

YAbbreviation Term

ZAbbreviation Term

ZFCG Zero Fuel Center of GravityZFW Zero Fuel WeightZFWCG Zero Fuel Weight Center of Gravity field


OPERATING MANUAL

GENERAL INFORMATION


82U A318/A319/A320/A321 FLEET GEN P 30/30FCOM 06 MAR 14

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