Honeywell PRIMUS 1000 Manual

PRIMUS 1000
Integrated Avionics System
Pilot's Manual for the
Embraer 145
AD-52817@

Printed inU.S.A.Pub.No.A28--1146--112--00 August1997
Business and CommuterAviation Systems
Honeywell Inc.
Box 29000
Phoenix,Arizona 85038--9000
PRIMUSr1000Integrated
AvionicsSystem
forthe
Embraer Model145
Pilot’sManual

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E1997 Honeywell Inc.
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PRIMUSr1000 Integrated Avionics System
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TC--1
TableofContents
Section Page
1. INTRODUCTION1-1.............................
2.SYSTEMDESCRIPTION2-1.....................
FlightGuidanceSystem(FGS)2-3.................
ElectronicDisplaySystem(EDS)2-4...............
AirDataSystem(ADS)2-5.......................
PRIMUSâ660 WeatherRadarSystem2-6..........
Attitude and Heading ReferenceSystem(AHRS)2-6.
PRIMUSâII Integrated RadioSystem2-7...........
RadioAltimeterSystem2-7.......................
TrafficAlertand Collision AvoidanceSystem
(TCAS)2-8....................................
PRIMUSâ880 WeatherRadarSystem(Option)2-8. .
FlightManagementSystem(FMS) (Option)2-9......
OtherSwitchesand Controls2-9...................
3.ELECTRONIC DISPLAY SYSTEM(EDS)3-1.......
Introduction 3-1.................................
MFDBezelControllerBasicOperation 3-5..........
Map Range Control3-6........................
ControllerConventions3-6.....................
ReversionaryControllersand Dimming Panel3-7....
SystemReversionaryPanel3-7................
DataAcquisition Unit(DAU)ReversionaryPanel3-8
EDSDimming Panel3-8.......................
4.ELECTRONICFLIGHTINSTRUMENTSYSTEM
(EFIS)4-1.....................................
Introduction 4-1.................................
Controls4-5....................................
PrimaryFlightDisplay(PFD)BezelController4-5...
Multifunction Display(MFD)BezelController4-6....
DisplayController (DC)4-20.....................
GuidanceControllerCourse and Heading
Controls4-22................................
EFIS PreflightSelf--Test4-23....................
Displays 4-25....................................
PrimaryFlightDisplay(PFD)4-25................
TypicalPFDPresentations4-53..................
PFD Caution and FailureDisplay4-61............

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4.ELECTRONICFLIGHTINSTRUMENTSYSTEM
(EFIS) (CONT)
Multifunction Display(MFD)4-68.................
MFDSystemDisplays 4-86.....................
SystemDisplayFailureAnnunciation 4-95.........
StandbyNavigation Display4-96.................
5.ENGINEINSTRUMENTAND CREWALERTING
SYSTEM(EICAS)5-1..........................
Introduction 5-1.................................
Controls5-5....................................
EICAS BezelController5-5....................
MasterWarning and Caution Annunciation
Switches5-5................................
Displays 5-6....................................
EICAS Display5-6............................
PrimaryEngine Displays 5-7...................
CrewAlerting System(CAS)5-22................
CAS Messages5-23...........................
CAS DisplayFailureIndications5-29.............
EICAS ReversionaryModes5-30................
Backup EICAS Display5-31.....................
Backup EICAS DisplayFailureIndications5-34....
6.FLIGHTGUIDANCE SYSTEM(FGS)6-1...........
GuidanceController (GC)6-1.....................
Autopilot(AP)/Yaw Damper (YD)/Couple(CPL)
Buttons6-1.................................
FlightDirector (FD)Mode Selection 6-3..........
RemoteAutopilotSwitchesand Annunciators6-5...
AutopilotPower--UpTest6-5...................
FGSCaution and AdvisoryMessages6-5........
AutopilotController6-6...........................
PitchWheel6-6..............................
TurnKnob 6-7................................
7.SYSTEMLIMITS7-1............................
GlossaryofTerms7-1............................
Attitude DirectorIndicator (ADI)Command
Cue 7-1....................................

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7.SYSTEMLIMITS(CONT)
Glideslope (GS)GainProgramming asaRadio
Altitude (RA)Function 7-2....................
GSGainProgramming asaRAand Vertical
Speed (VS)Function 7-2.....................
GSCapture(CAP)7-2........................
LateralBeamSensor (LBS)7-2.................
LateralGainProgramming 7-3..................
Localizer/Back Course(BC)Track 7-3...........
True Airspeed (TAS)GainProgramming 7-3......
VerticalBeamSensor (VBS)7-4................
VOR Capture(CAP)7-4.......................
VOROverStation Sensor (OSS)7-4............
VORAfterOverStation Sensor (AOSS)7-4......
SystemPerformance and Operating Limits7-5......
8.MODES OFOPERATION8-1.....................
Heading (HDG)HoldMode,WingsLevel8-1........
Roll HoldMode 8-2..............................
Heading SelectMode 8-3.........................
VOR Navigation (NAV)Mode 8-4..................
VORApproach(VAPP)Mode 8-9..................
FlightManagementSystem(FMS)Navigation
Mode (Option)8-10..............................
Localizer (LOC)Mode 8-12........................
Back Course(BC)Mode 8-17......................
InstrumentLanding System(ILS)ApproachMode 8-20. .
PitchHoldMode 8-25.............................
PitchHoldMode Operation,AP Engaged 8-25.....
PitchHoldMode Operation,AP NotEngaged 8-25...
TakeOff Mode 8-26...............................
VerticalSpeed HoldMode 8-27.....................
Speed HoldMode 8-28............................
FlightLevelChange (FLC)Mode 8-31...............
Altitude Preselect(ASEL)Mode 8-32................
Altitude Hold(ALTHOLD)Mode 8-37................
Windshear (WDSHEAR)Mode 8-38.................
Go--Around (GA)Mode (WingsLevel)8-40...........

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9.TROUBLESHOOTING9-1.......................
PilotWriteup 9-1.................................
CommonlyUsed Terms9-3....................
TypicalProblems9-4..........................
Ground MaintenanceTest9-9.....................
Multifunction Display(MFD)ChecklistUpload
Procedure 9-11.................................
10.HONEYWELL PRODUCTSUPPORT10-1..........
Publication Ordering Information 10-4.............
11.ABBREVIATIONS11-1...........................
APPENDICES
A--1AHZ--800 ATTITUDEAND HEADINGREFERENCE
SYSTEM(AHRS)A--1...........................
Introduction A--1.................................
Attitude and Heading ReferenceUnitA--5............
AHRSControland EICAS Annunciation A--5.........
AHRSControlsA--5............................
EICAS AnnunciationsA--6......................
Operation A--7...................................
StandardOperation A--7........................
Reduced PerformanceOperation A--8............
Power--UpTestA--8..............................
PilotSelf--TestA--9...............................
Ground Initialization A--9..........................
AbnormalOperationsA--10......................
B--1PRIMUSâ660 WEATHER RADAR SYSTEMB--1....
Introduction B--1.................................
Description B--1..................................
WeatherRadarControllerB--2.....................
Controlsand IndicatorsB--2.....................
NormalOperation B--8.........................
MaximumPermissibleExposure Level(MPEL)B--12....

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C--1PRIMUSâII RADIOSYSTEMC--1..................
Introduction C--1.................................
SystemDescription C--5...........................
GeneralC--5..................................
Integrated Navigation UnitC--5..................
Integrated Communication UnitC--6..............
RadioManagementUnit(RMU)C--6.............
AudioPanelC--6..............................
Tuning Backup ControlHead C--7................
RadioManagementUnit(RMU)Operation C--7.......
GeneralC--7..................................
ControlsC--8..................................
MemoryPagesC--11............................
System(SYS)On--Off Page C--11................
VHFCommunicationsTransceiverOperation C--13. .
Navigation ReceiverOperation C--17..............
ATCTransponderand TCAS OperationsC--20.....
ADFOperation C--24............................
Cross--Side Operation C--27.....................
Built--In--Test(BIT)C--28.........................
MaintenanceC--32..............................
RMU DisplayDimming C--32.....................
AudioPanelOperation C--33........................
GeneralC--33..................................
ControlsC--33..................................
Tuning Backup ControlHead Operation C--35.........
GeneralC--35..................................
NormalMode C--36.............................
Emergency Mode C--36.........................
Controlsand AnnunciationsC--37.................
INDEX Index--1.............................................

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ListofIllustrations
FigurePage
1--1PRIMUSâ1000 inthe Embraer145 Cockpit1-5.....
2--1PRIMUSâ1000 Block Diagram2-11.................
3--1CockpitLayoutofEFIS3-3.......................
3--2MFDBezelControls3-5..........................
3--3SystemReversionaryPanel3-7...................
3--4DAU ReversionaryPanel3-8......................
4--1EFIS Block Diagram4-3..........................
4--2PFDBezelController4-5.........................
4--3MFDBezelController4-6.........................
4--4Menu Inop Display4-6...........................
4--5MFDMenu Tree 4-7.............................
4--6MainMenu 4-8..................................
4--7System Menu Selections4-8......................
4--8MainMenu -- MFDButton 4-10.....................
4--9MFDMainMenu (WithoutFMS)4-10................
4--10 MFDMainMenu (WithFMS)4-11..................
4--11 VSPEEDSSubmenu 4-11...........................
4--12 Joystick Submenu 4-13............................
4--13 ChecklistMenu 4-15..............................
4--14 TCAS Selection from MainMenu 4-18...............
4--15 WX Selection from MainMenu 4-18.................
4--16 MAP Plan Selection From MainMenu 4-19...........
4--17 DisplayController4-20............................
4--18 GuidanceController4-22..........................
4--19 PFDFunctionalDivisions4-25......................
4--20 ADIand Annunciation Display4-27..................
4--21 PFDWithCATII Annunciations4-35................
4--22 HSICompass DisplayOnPFD4-37.................
4--23 HSIArcDisplayWithFMSMap and Weather
Radar4-41.....................................
4--24 Airspeed Display4-45.............................
4--25 AltimeterDisplay4-48.............................
4--26 VerticalSpeed Display4-51........................
4--27 Takeoff Mode 4-53................................
4--28 ClimbtoInitialAltitude 4-54........................
4--29 EnrouteCruise 4-55...............................
4--30 Setup forApproach 4-56...........................

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4--31 TCAS II Resolution AdvisoryApproaching the
Glideslope 4-57.................................
4--32 ApproachCaptureTracking atDH 4-58..............
4--33 Comparison MonitorAnnunciators4-59..............
4--34 PFDWithARC HSIDisplayand Caution/Failure
Annunciations4-61..............................
4--35 PFD Caution IndicationsforVerticaland Course
Deviation 4-63..................................
4--36 FailureIndicationsforATT,MADC,HDG,CRS
Selectand FD4-65..............................
4--37 ExcessiveAttitude Declutter4-66...................
4--38 PFDTestMode 4-68..............................
4--39 MFD Common Symbols4-69.......................
4--40 MFDMap DisplaySymbols4-72....................
4--41 Map Mode WithWeather4-74......................
4--42 Map Failure/Warning 4-75..........................
4--43 Map Mode WithoutWeather4-76...................
4--44 Map Mode WithWeather4-77......................
4--45 MFDPlan View4-78..............................
4--46 Plan Mode Caution and Warning Displays 4-79.......
4--47 TypicalPlan Mode WithNavaidComponentsand
FlightPlan 4-80.................................
4--48 TypicalChecklistDisplay4-83......................
4--49 MFDWithMap Mode Displayand OptionalTCAS 4-84
4--50 Takeoff Display4-87..............................
4--51 EnvironmentalControlSystem(ECS)System
Display4-88....................................
4--52 FuelPage 4-90...................................
4--53 Hydraulic(HYD)SystemPage 4-92.................
4--54 Electrical(ELEC)SystemDisplay4-93..............
4--55 StandbyNavigation Display(Typical)4-97............
4--56 RMUBackup Navigation Display4-98...............
4--57 RMUBackup Navigation DisplayWithFailures4-101...
5--1EICAS Block Diagram5-3........................
5--2EICAS BezelController5-5.......................
5--3MasterWarning and Caution Annunciation Switches5-5. .
5--4EICAS DisplayFunctionalDivisions5-6.............
5--5EICAS Engine InstrumentsDisplay5-8.............
5--6EICAS inthe Takeoff Condition (Typical)5-20........
5--7Engine InstrumentDisplayWithFailures5-21........

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5--8CrewAlerting Systemon EICAS Display5-22........
5--9EICAS InvalidDisplayFormats5-30.................
5--10 Backup EICAS Displayon RMU-- Page 1 5-32.......
5--11 Backup EICAS Displayon RMU-- Page 2 5-33.......
5--12 RMUBackup Engine DisplayFailureIndication 5-34....
6--1GuidanceController6-1..........................
6--2AutopilotController6-6...........................
8--1Heading HoldMode 8-1..........................
8--2Roll HoldMode 8-2..............................
8--3VOR Navigation Mode RadialInterceptView8-5.....
8--4VOR Navigation Mode InterceptPFD8-5...........
8--5VOR Navigation Mode CapturePlan View8-6.......
8--6VOR Navigation Mode Capture 8-7................
8--7VOR Navigation Mode Tracking 8-8...............
8--8VOR Navigation Mode -- Tracking OverStation 8-9....
8--9 Long Range Navigation Mode Display8-11...........
8--10 LocalizerMode ArmDisplay8-13...................
8--11 LocalizerMode CapturePlan View8-14.............
8--12 LocalizerCaptureDisplay8-15.....................
8--13 LocalizerMode Tracking ProfileView8-16...........
8--14 LocalizerTracking Display8-16.....................
8--15 Back CourseMode InterceptPlan View8-17.........
8--16 Back CourseTracking Display8-19.................
8--17 ILS Approach LocalizerIntercept8-20...............
8--18 ILS ApproachMode Glideslope Capture,Profile
View8-23......................................
8--19 ILS ApproachMode Tracking PFD8-24..............
8--20 ILS ApproachMode Tracking,ProfileView8-25.......
8--21 Takeoff Mode 8-26................................
8--22 VerticalSpeed HoldMode PFD8-28................
8--23 Speed HoldMode PFD8-29.......................
8--24 Altitude PreselectPlan View8-34...................
8--26 WindshearMode PFD8-39........................
8--27 Go--Around Mode (WingsLevel)PFD8-41...........
9--1 LateralMode Conditionsand Problems9-5..........
9--2VerticalMode Conditionsand Problems9-7.........
9--3Ground MaintenanceTestDisplay(Typical)9-10......

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A--1AHRU Block DiagramA--3.........................
A--2AHRSControlsA--5..............................
B--1WeatherRadarControllerB--2.....................
B--2PFD DisplayWeatherRadarTestPatternB--9........
B--3MFD DisplayWeatherRadarTestPatternB--10.......
B--4RadarBeamIllumination High Altitude
12--InchRadiatorB--11...........................
B--5RadarBeamIllumination LowAltitude
12--InchRadiatorB--11...........................
B--6MPELBoundaryB--12.............................
C--1PRIMUSâII RadioSystemInterfaceBlock DiagramC--3
C--2RadioManagementUnitControlsC--8...............
C--3Page Menu C--10..................................
C--4COMFrequency Storage Page C--11.................
C--5SystemOn--Off Page C--12.........................
C--6RMUinCOMTuning Mode C--14....................
C--7RMUTuning C--14.................................
C--8Exchanging the Presetand ActiveFrequenciesC--15....
C--9COM Message (SquelchOpen)C--16................
C--10 NAV Frequency SelectWindow C--17................
C--11 Toggling Active and PresetFrequenciesC--18.........
C--12 DMEHoldC--19...................................
C--13 RMUATC/TCAS ControlsC--21.....................
C--14 ADFControlsC--25................................
C--15 AudioPanelC--33.................................
C--16 Tuning Backup ControlHead C--36..................
C--17 Tuning Backup ControlHead Controlsand
AnnunciationsC--37..............................

PRIMUSr1000 Integrated Avionics System
A28--1146--112--00
Table ofContents
TC--10
TableofContents(cont)
ListofTables
TablePage
1--1SupplementalPilot’sManuals1-1.................
1--2EquipmentList1-2..............................
4--1CursorMovement/Action 4-16.....................
4--2Navigation Bearing Pointers4-21..................
4--3Yaw DamperStatusAnnunciations4-26............
4--4Pitch Limit Indicator4-29.........................
4--5PitchScaleTape Markings4-29...................
4--6On--Side SensorSources4-31....................
4--7AutopilotStatusAnnunciations4-32................
4--8MarkerBeacon Annunciations4-33................
4--9Bearing PointerSelections4-38...................
4--10 GSPD,TTG,ETRanges4-39.....................
4--11 Navigation SymbolColors4-40....................
4--12 Approach and TerminalAnnunciators4-42..........
4--13 WeatherRadarAnnunciations4-43................
4--14 Selected SourceDistanceRange 4-44.............
4--15 VSPEEDBug Identification 4-46.....................
4--16 LowSpeed Awareness ColorLogic4-47............
4--17 Comparison MonitorParameters4-60..............
4--18 Yaw DamperStatusAnnunciations4-64............
4--19 TCAS FailureAnnunciations4-64..................
4--20 ExcessiveAttitude DeclutterParameters4-67.......
4--21 WeatherRadarMode Annunciationson MFD4-70...
4--22 DesignatingaNewWaypointProcedure 4-81........
4--23 Engine T/OMode Logic4-88......................
4--24 Oxygen Pressure LimitsinPSI4-89................
4--25 Bleed AirTemperatureColorLimits4-89............
4--26 FuelQuantityColorCoding 4-90...................
4--27 HydraulicPressure and FluidQuantityLimits4-92...
4--28 BrakeTemperature Limits4-93....................
4--29 MarkerBeacon Colors4-99.......................
5--1N1Analog Scale 5-9.............................
5--2FADECModesofOperation 5-10...................
5--3ITT Limits5-11...................................
5--4IgnitorAnnunciation ColorDefinition 5-11............
5--5N2Limits5-12....................................
5--6Oil Pressure LimitsforN2<88%5-12................
5--7Oil Pressure LimitsforN2>88%5-13................