WIXLIB

3LIST OF ACRONYMSThe following acronyms may appear in this UCRCRCDAD-ADAICDDARDCNDEMDERDHDLDMEDMIRAdvisory CircularAirworthiness DirectiveAutomatic Direction FinderAnalog to Digital (converter)Air Data Attitude Heading Reference SystemAir Data ComputerAutomatic Dependent Surveillance-BroadcastAircraft Flight ManualAbove Ground LevelAttitude Heading Reference SystemAirmen’s Meteorological InformationActive Matrix Liquid Crystal DisplayAmerican National Standards InstituteApproach with Vertical GuidanceAeronautical Radio, Inc.SAE Aerospace Recommended PracticeSAE Aerospace StandardAT Attachment (hard disk storage interface)Air Traffic ControlCourse Deviation IndicatorCockpit Display of Traffic InformationCritical Design ReviewGenesys Aerosystems, Inc.Configuration ManagementCommunicationCompany Project ManagerCentral Processing UnitChange RequestCyclic Redundancy CheckDecision AltitudeDigital to Analog (converter)Digital Aeronautical Information CDDesignated Airworthiness RepresentativeDocument Change NoticeDigital Elevation ModelDesignated Engineer RepresentativeDecision HeightData LinkDistance Measuring EquipmentDesignated Manufacturing InspectionRepresentativeDORTCA DocumentDODDepartment of DefenseDOFDigital Obstruction FileDPDeparture ProcedureDQRData Quality RequirementDRDead Reckoning or Defect ReportDSPDigital Signal ProcessingEFISElectronic Flight Instrument SystemEGPWS Enhanced Ground Proximity Warning SystemEIAElectronics Industry AssociationEICASEngine Instrument and Crew Alerting SystemETAEstimated Time of ArrivalETEEstimated Time EnrouteFAAFederal Aviation AdministrationFAFFinal Approach FixFARFederal Aviation RegulationFAWPFinal Approach Waypoint - same as FAFFDEFault Detection and ExclusionFHAFunctional Hazard AnalysisFIFO"First in, First out"FISFlight Information ServiceFIS-BFlight Information Service-BroadcastFLFlight LevelFLTAForward Looking Terrain GPSGPWSHALHATHFOMHPLHSIHULIAPFault Mode and Effects AnalysisFlight Management SystemFloating Point EmulationFeet per MinuteFull Scale DeflectionFlight Technical ErrorGNSS Landing SystemGround (potential)Global Navigation Satellite SystemGallons per HourGlobal Positioning SystemGround Proximity Warning SystemHorizontal Alert LimitHeight Above ThresholdHorizontal Figure of MeritHorizontal Protection LevelHorizontal Situation IndicatorHorizontal Uncertainty LimitInstrument Approach Procedure, also InitialApproach PointIASIndicated AirspeedIAWPInitial Approach Waypoint - same as IAPICIntegrated CircuitICAOInternational Civil Aviation OrganizationICDInterface Control DocumentIDIdentity or IdentificationIDUIntegrated Display UnitIFRInstrument Flight RulesILSInstrument Landing SystemIMInner MarkerIOInput/OutputIPVInstrument Procedure with Vertical GuidanceISRInterrupt Service RoutineJADJeppesen Aviation DatabaseJTAGJoint Test Action Group (IEEE 1149.1 Standard)KKilo 1000KBKilobyteKIASKnots Indicated AirspeedKTKnot - Nautical Mile per HourKTASKnots True AirspeedLDALocalizer-type Directional AidLEDLight Emitting DiodeLNAVLateral NavigationLOALetter of AuthorizationLOCLocalizerLRULine Replaceable UnitLSBLeast Significant Bit or ByteMAHPMissed Approach Holding PointMAHWP Missed Approach Holding Waypoint - same asMAHPMAPMissed Approach PointMASPS Minimum Aviation System Performance StandardMAWP Missed Approach Waypoint - same as MAPMBMegabyteMDAMinimum Descent AltitudeMEMSMicro Electro Mechanical SystemMFDMultifunction Display (an IDU with software forshowing multiple display screens)MMMiddle MarkerMOPSMinimum Operational Performance StandardMOTMark On TargetMSBMost Significant Bit or ByteMSLMean Sea LevelMSUMagnetic Sensor UnitMTBFMean Time Between FailuresGenesys Aerosystems, Inc. – ConfidentialPage 8 of 22

ational Aeronautical Charting OfficeU.S. National Airspace SystemNational Aeronautics and Space AdministrationNational Elevation DatasetNational Imagery and Mapping AgencyNavigation DisplayNondirectional BeaconNautical MileNon-Precision ApproachOutside Air TemperatureOmnibearing SelectorOuter MarkerOther Traffic (Traffic Function)Proximate Advisory (Traffic Function)Premature Descent AlertPreliminary Design ReviewPrimary Flight Display (the display screen showingprimary instrumentation -- can also refer to theprimary IDU with software that only shows primaryinstrumentation)PFDEPredictive Fault Detection and ExclusionPICPeripheral Interface ControllerPLIPitch Limit IndicatorPNPart NumberPRAIM Predictive Receiver Autonomous Integrity MonitoringPSACPlan for Software Aspects of CertificationPSCPProject Specific Certification PlanPSPPartnership for Safety PlanPTNProblem Tracking NumberQAQuality AssuranceQFEAltimeter setting that provides height abovereference point.QMQuality ManagementQNEAltimeter setting that provides pressure altitudereadoutQNHAltimeter setting that provides MSL altitude at areporting pointRAResolution Advisory (Traffic Function)RAMRandom Access MemoryRBPRemote Bug PanelRMIRadio Magnetic IndicatorRNAVArea NavigationRNPRequired Navigation PerformanceRSEIA Recommended StandardRTCReal Time ComputingRTCARadio Telephone Commission for AeronauticsRTDResistive Thermal DetectorRTLRun Time LibraryRxReceiveSASelective AvailabilitySAESociety of Automotive EngineersSASSoftware Accomplishment SummarySBASSatellite Based Augmentation SystemSCISoftware Configuration IndexSCMPSoftware Configuration Management PlanSCRSoftware Conformity ReviewSCSSoftware Coding StandardsSDDSoftware Design DocumentSDPSoftware Development PlanSDSSoftware Design StandardsSECISoftware Environment Configuration IndexSIGMET Significant Meteorological AdvisorySMASub-Miniature version A connectorSNSerial NumberSNISerial Number InformationSOIStage of Involvement (FAA software audit)SPRSoftware Problem ReportSQASoftware Quality AssuranceSQAPSoftware Quality Assurance PlanSQARSoftware Quality Assurance Representative01-000062SRDSoftware Requirements DocumentSRSSoftware Requirements StandardsSRTMShuttle Radar Topographical MissionSSASystem Safety AssessmentSTARStandard Terminal Arrival RoutesSTCSupplemental Type CertificateSTPSoftware Test ProtocolSTSSoftware Test SpecificationSUASpecial Use AirspaceSVService VehicleSVCPSoftware Verification Cases and ProceduresSVPSoftware Verification PlanSVRSoftware Verification ResultsSYRDSystem Requirements DocumentTATraffic Advisory (Traffic Function)TAFsTerminal Aerodrome ForecastsTASTraffic Advisory SystemTAWSTerrain Awareness and Warning SystemTCADTraffic Collision Alert DeviceTCASTraffic Collision Alert SystemTERPS Terminal Instrument ProceduresTCHThreshold Crossing HeightTDTraffic DisplayTFRTemporary Flight RestrictionTISTraffic Information ServiceTIS-BTraffic information Service-BroadcastTMSTexas Instruments family of DSP processorsTQPTool Qualification PlanTSOTechnical Standard OrderTxTransmitUARTUniversal Asynchronous Receiver-TransmitterUSGSUnited States Geological SurveyUTCUniversal Time CoordinatedVALVertical Alert LimitVFOMVertical Figure of MeritVFRVisual Flight RulesVHFVery High FrequencyVNAVVertical NavigationVORVHF Omnidirectional RadioVPLVertical Protection LevelVSIVertical Speed IndicatorVTFVectors to FinalVULVertical Uncertainty LimitSBASWide Area Augmentation SystemWGS84 World Geodetic System 1984Genesys Aerosystems, Inc. – ConfidentialPage 9 of 22

44.1SYSTEM OVERVIEWEFIS SYSTEMThe EFIS is a complete flight and navigation instrumentation system that intuitivelyprovides information to a pilot via computer generated screen displays on IDUs. Thescreen displays are a three-dimensional, enhanced situational awareness PFD and anMFD that can be configured to show a moving map, an HSI, traffic, terrain or weatherdisplays.Generally, IDUs are part of a complete flight and navigation instrumentation system thatintuitively provides information to a pilot via computer generated screen displays. TheIDUs may be configured as a PFD (a three-dimensional, enhanced situational awarenessPrimary Flight Display) or an MFD (Multi-Function Display that can be configured to showa moving map, an HSI, traffic, terrain or weather displays). A system consists of variousdiscrete digital sensor modules that communicate with IDUs via RS-232, RS-422 orARINC 429 serial data. Each IDU incorporates a high-brightness AMLCD screen, bezelkeys, a screen and keyboard lighting intensity control, rotary selector and enter switches,a central processing unit, numerous RS-232, RS-422 and ARINC 429 receive andtransmit ports, and discrete IO ports. Because the receive ports of the IDUs areconnected to the digital sensor modules in parallel, each IDU is independent from allother IDUs. The following is a typical system diagram.01-000062Genesys Aerosystems, Inc. – ConfidentialPage 10 of 22

CrosslinkGPS #1*TrafficSensor*GPS #2*RemoteTune RadiosIDU #1ADC #1*VideoIDU #1*IDU #2*ADC #2*RemoteBugs Panel*IDU #2*IDU #3AHRS #1*DigitalAutopilot*IDU #3*IDU #4*AHRS #2*Airframe/Engine Data*IDU #4Pilot*Datalink/ADS-B*WeatherRadar*WX-500*Mode STransponder*AnalogInterface*Fuel Flow/QuantitySynchSynchCo-PilotNote: * Optional4.2IDU NAVIGATION DATABASEThe navigation database provides information relating to navigation aids, procedures andcommunications. Database elements to support TSO-C146c Class Gamma-3 include:AirportsNavigation Aids (VORs, DMEs, VOR/DMEs, VORTACs and NDBs)Named Waypoints and IntersectionsRNAV DPsRNAV STARsLNAV, LNAV/VNAV and LPV Approach Procedures and Levels of ServiceFAS Data Blocks with embedded CRC-32sApproach Levels of ServiceApproach HALs and VALs01-000062Genesys Aerosystems, Inc. – ConfidentialPage 11 of 22

Additional database elements to support flight planning features and moving mapdepictions include:AirspaceAirwaysEnroute and airport communicationsNavigation data elements are obtained by electronic data transfer from the JeppesenAviation Database (JAD, Jeppesen Sanderson Inc.) on a 28-day update cycle. Requireddata elements are extracted from the ARINC-424 format JAD and reformatted withoutmodification to meet IDU requirements. Data elements selected for processing vary withthe area of coverage selected by the end-user. A detailed description of the packing tooldesign requirements are presented in the Navigation Database Conversion – SoftwareRequirements (Doc. No. 20-000058).4.3IDU OBSTRUCTION DATABASEThe obstruction database provides information relating to obstructions and hazards tonavigation including:Arches, balloons, bridges, buildings, building towers, catenaries, controltowers, cooling towers, crane, dams, domes, elevators, monuments, plants,poles, rigs, refineries, signs, spires, stacks, tanks, transmission line towers,towers, tramways, and windmills.Obstruction information is provided for the entire world. Obstruction data elements areobtained in digital format from Jeppesen Sanderson, Inc. on a 28-day update cycle.Required data elements are extracted from the supplied digital file and reformatted tomeet IDU requirements. A detailed description of the packing tool design requirementsare presented in the Obstruction Database Conversion – Software Requirements (Doc.No. 21-000005). The obstruction database is not covered by the Type 2 LOA and isdescribed here because it may be bundled with the navigation database.01-000062Genesys Aerosystems, Inc. – ConfidentialPage 12 of 22

55.1COMPATIBILITY MATRIXDATABASE PART NUMBERThe IDU navigation database can be delivered stand-alone or bundled with theobstruction database. The part number of the stand-alone or bundled database productis encoded as follows:CS[A][BBB] [xxxx] [wwwwwwww][A]DescriptionEFIS Software RevisionDatabase17.0D to 8.0CNavData only27.0C and earlierNavData only37.0D to 8.0CNavData bundled with Obstacles47.0C and earlierNavData bundled with Obstacles58.0D and laterNavData only68.0D and laterNavData bundled with Obstacles[BBB] apstone tailored WorldREGRega tailored WorldNotes: [1] [BBB] can be any 3-letter identifier to accommodate future tailoreddatabase customers.Field[xxxx][wwwwwwww]DescriptionDatabase cycle number. For example: 1604.8-character hexadecimal 32-bit CRC of database file. For example:EE9DB378.Notes: Database cycle number changes based on a schedule published by ate-schedule.jsp. 8-character CRCvalue changes with each cycle based on the contents of the database file.01-000062Genesys Aerosystems, Inc. – ConfidentialPage 13 of 22

Database Part Number Decoding Examples:Database Part NumberDescriptionCS4002 1604 EE9DB378Part Number Prefix:CS4002Contents:NavData bundled with ObstaclesEFIS Software Revision: 7.0C and earlierCS3REG 1513 7445F065Coverage:AmericasCycle:1604Filename:CS4002 1604 EE9DB378.zipPart Number Prefix:CS3REGContents:NavData bundled with ObstaclesEFIS Software Revision: 7.0D to 8.0CCS5001 1608 2E5E0A8ACoverage:Rega tailored WorldCycle:1513Filename:CS3REG 1513 7445F065.zipPart Number Prefix:CS5001Contents:NavData onlyEFIS Software Revision: 8.0D and 001 1608 2E5E0A8A.zipGenesys Aerosystems, Inc. – ConfidentialPage 14 of 22

5.2EFIS SOFTWARE REVISIONSThe EFIS software revision defines the compatible database part numbers. Table 5.1lists experimental EFIS equipment and the applicable approved and compatible EFISsoftware revisions. Table 5.2 lists the certified EFIS equipment (under FAA TSOA) andthe applicable approved and compatible EFIS software revisions. Images of the EFISequipment, identifying characteristics, hardware part number locations, and softwarerevision identification is provided in Appendix 1.Table 5.1 Experimental EFIS EquipmentMake [3]Part NumberModel [3]Software 20-345239-050C5.0C320-345239-060B6.0B-X SW-00067.0E25-EFIS70E-SW-0007Notes: [1] IDU-III is also called IDU-3.[2] X External sensor dash number.[3] “Series” parameter per AC 20-153A 9.b.(4)(c) is not applicable to this equipment.01-000062Genesys Aerosystems, Inc. – ConfidentialPage 15 of 22

Table 5.2 Certified EFIS Equipment (under FAA TSOA)Make[3]ModelPart Number[3]Software RevisionHardwareIDU-III [1]IDU-III -EFIS70F-SW-00027.0F25-EFIS70F-SW-0003IDU-IV 4]8.0E[4]8.0FNotes: [1] IDU-III is also called IDU-3.[2] IDU-IV is also called IDU-4 or IDU-IV Family.[3] “Series” parameter per AC 20-153A 9.b.(4)(c) is not applicable to this equipment.[4] Pending TSOA and software release.01-000062Genesys Aerosystems, Inc. – ConfidentialPage 16 of 22

5.3NAVIGATION DATABASE COMPATIBILITY BY SOFTWARE REVISIONTable 5.3 lists the EFIS software revisions and the applicable compatible navigationdatabase part number prefixes. A navigation database part number must have the listedprefix to be compatible with the associated EFIS software revision.Table 5.3 Navigation Database CompatibilityJeppesen DatabaseEFIS SoftwareRevisionNavData Obstacles [2] 5.0C6.0B-X[1]Database PartNumber Capstone [3]CS4CAPRega7.0A7.0B7.0CNavData Coverage stoneRega7.0D nternationalCS3003[3]7.0ECapstone7.0FRega ionalCS10038.0C CapstoneRega01-000062[3][3]Genesys Aerosystems, Inc. – ConfidentialCS3CAPCS1CAPCS1REGPage 17 of 22

Table 5.3 Navigation Database Compatibility (Continued)Jeppesen DatabaseEFIS SoftwareRevisionNavData Obstacles [2] NavData CoverageDatabase PartNumber sCS5002InternationalCS5003 CapstoneRegaCS6REG[3][3]CS5CAPCS5REGNotes: [1] X External sensor dash number.[2] Obstacle database coverage is always worldwide regardless ofthe NavData coverage selected.[3] Capstone and Rega tailored NavData coverage contains World NavData coverage.01-000062Genesys Aerosystems, Inc. – ConfidentialPage 18 of 22

APPENDIX 1: EQUIPMENT IDENTIFICATIONIDU-IIdentifyingCharacteristics4x5 inch display.8 line-select keys and 2 rotary encoders knobs at bottom.SmartMedia card slot at bottom near left rotary encoder knob.SmartMedia card inserted with contacts facing down.Bezel cut at 45 degree angle at all corners.Panel-mounted display.D-sub connectors on rear.PhysicalFeatures&HardwarePart NumberLocation(highlightedin red)EFISSoftwareRevision(shown onStatus Page,highlightedin red)01-000062Genesys Aerosystems, Inc. – ConfidentialPage 19 of 22

IDU-IIIIdentifyingCharacteristics4x5 inch display.8 line-select keys and 2 rotary encoders knobs at bottom.SmartMedia card slot centered at the bottom between the rotary encoder knobs.SmartMedia card inserted with contacts facing up.Square bezel.Tray-mounted display.PhysicalFeatures&HardwarePart NumberLocation(highlightedin red)EFISSoftwareRevision(shown onStatus Page,highlightedin red)01-000062Genesys Aerosystems, Inc. – ConfidentialPage 20 of 22

IDU-450IdentifyingCharacteristics4x5 inch display.8 line-select keys and 2 rotary encoder knobs at bottom.USB port centered at the bottom between the rotary encoder knobs.USB port exposed when sliding the slip or non-slip housing upwards.Square bezel.Panel-mounted display.PhysicalFeatures&HardwarePart NumberLocation(highlightedin red)EFISSoftwareRevision(shown onStatus Pagealong withSoftwarePart Number,highlightedin red)01-000062Genesys Aerosystems, Inc. – ConfidentialPage 21 of 22

IDU-680IdentifyingCharacteristics6x8 inch display.16 line-select keys and 4 rotary encoder knobs at bottom.USB port centered at the bottom between the inner rotary encoder knobs.USB port exposed when sliding the slip or non-slip housing upwards.Rectangular bezel.Panel-mounted display.PhysicalFeatures&HardwarePart NumberLocation(highlightedin red)EFISSoftwareRevision(shown onStatus Pagealong withSoftwarePart Number,highlightedin red)01-000062Genesys Aerosystems, Inc. – ConfidentialPage 22 of 22

RTCA/DO-178B Software Considerations in Airborne Systems and Equipment Certification RTCA/DO-200A Standards for Processing Aeronautical Data RTCA/DO-201A Standards for Aeronautical Information RTCA/DO-229D Minimum Operational Performance Standards for Global Positioning System System/Wide Area Augmentation System Airborne Equipment .