Canadair Regional Jet 100/200 - Aircraft General...1. ABBREVIATIONS The following abbreviations may be used by flight compartment displays, radio tuning units and flight management

1. ABBREVIATIONS

The following abbreviations may be used by flight compartment displays, radio tuning unitsand flight management system or be found throughout the manual. Some abbreviationsmay also appear in lower case letters. Abbreviations having very limited usage areexplained in the systems chapters where they are used.

AA/C . . . . . . . Air-Conditioning ALT . . . . . . Altitude, AltimeterA/G . . . . . . . Air/Ground ALT . . . . . . Altitude Hold (PFD/FD)A/ICE . . . . . Anti-ice ALT CAP . . Altitude Capture (PFD/FD)A/P . . . . . . . Autopilot ALT HOLD Altitude HoldA/S . . . . . . . Airspeed ALTN . . . . . AlternateA/SKID . . . Anti-skid ALTS . . . . . Selected Altitude Arm/Abort(PFD/FD)ABS . . . . . . Absolute AM . . . . . . . Amplitude ModulationAC . . . . . . . Advisory Circular AMB . . . . . . AmbientAC . . . . . . . Alternating Current AMP . . . . . . Amperes

ACARS . . .ARINC CommunicationsAddressing and ReportingSystem

ANNUN . . . Annunciator

ACCEL . . . Acceleration, accelerate(d),accelerometers ANT . . . . . . AntennaACM . . . . . . Air Cycle Machine AOA . . . . . . Angle of AttackACMP . . . . Alternating Current Motor Pump/Electric Hydraulic Pump AP . . . . . . . AutopilotACT . . . . . . Active APC . . . . . . Auxiliary Power ControlACU . . . . . . Air Conditioning Unit APP . . . . . . ApproachADC . . . . . . Air Data Computer APPROX . . ApproximatelyADDR . . . . Address APR . . . . . . Automatic PerformanceReserveADF . . . . . . Automatic Direction Finder APU . . . . . . Auxiliary Power UnitADF . . . . . . Automatic Direction Finding ARINC . . . . Aeronautical Radio IncorporatedADG . . . . . . Air Driven Generator ARP . . . . . . Air Data Reference PanelADI . . . . . . . Attitude Director Indicator ASYM . . . . AsymmetricalADS . . . . . . Air Data System ATA . . . . . . Air Transport AssociationAFCS . . . . . Automatic Flight Control System ATC . . . . . . Air Traffic ControlAFT . . . . . . Afterward ATT . . . . . . AttitudeAGL . . . . . . Above Ground Level ATTCS . . . . �� AHC . . . . . . Attitude Heading Computer ATTD . . . . . AttitudeAHRS . . . . Attitude Heading ReferenceSystem ATTND . . . AttendantAIL . . . . . . . Aileron AUTO . . . . AutomaticALIGN . . . . Aligning, alignment AUTO BAL Automatic BalanceALPHA . . . alpha AUTO XFER Automatic TransferAUX . . . . . . Auxiliary AVAIL . . . . . AvailableAV . . . . . . . Avionics AZ . . . . . . . Azimuth

Canadair Regional Jet 100/200 - Aircraft General

Page 1

BB/AIR . . . . . Bleed Air BLD . . . . . . BleedB/C . . . . . . . Back Course BOOM . . . . Headset microphoneB/CRS . . . . Back Course BRG . . . . . . BearingB/LEAK . . . Bleed Leak BRKR(s) . . Breaker(s)BARO . . . . Barometric BRT . . . . . . BrightBAT . . . . . . Battery BTL . . . . . . BottleBATT . . . . . Battery BTMS . . . . Brake Temperature MonitoringSystemBDI . . . . . . . Bearing Distance Indicator BTMU . . . . Brake Temperature MonitoringUnitBFO . . . . . . Beat Frequency Oscillator BYPS . . . . . BypassBITE . . . . . . Built-In-Test EquipmentBK . . . . . . . Brake

CC . . . . . . . . . Center, Caution, Cabin CLK . . . . . . ClockCAA . . . . . . Civil Aviation Authority (UK) Cm . . . . . . . CentimetersCAL . . . . . . Calibrate CMD . . . . . CommandCAP . . . . . . Capture CMPS . . . . CompassCAPT . . . . . Captain CMPTR . . . ComputerCAS . . . . . . Calibrated Air Speed CO2 . . . . . . . . . Carbon DioxideCAT . . . . . . Category COM . . . . . CommunicationCAT . . . . . . Clear Air Turbulence COMM . . . . CommunicationCAT I, II, III Category I, II, III COMP . . . . Compressor, ComparatorCB, C/B . . . Circuit Breaker COMPT . . . CompartmentCBP . . . . . . Circuit Breaker Panel COND . . . . Condition, ContinuedCCW . . . . . Counter Clockwise CONFIG . . ConfigurationCDL . . . . . . Configuration Deviation List CONN . . . . ConnectionCDP . . . . . . Compressor DischargePressure CONT . . . .

Control, Continuous, Contactor,Controller

CDU . . . . . . Control Display Unit COOL . . . . CoolingCFM . . . . . . Cubic Feet Per Minute CORR . . . . Correction

CPAM . . . . Cabin Pressure AcquisitionModuleCG . . . . . . . Center of Gravity CPLT . . . . . CopilotCH . . . . . . . Chapter, Channel CRS . . . . . . CourseCHAN . . . . Channel CRT . . . . . . Cathode Ray TubeCHGR . . . . Charger CRZ . . . . . . CruiseCHR . . . . . . Chronograph CSD . . . . . . Constant Speed DriveCHRT . . . . . Chart CTR . . . . . . CenterCK . . . . . . . Check CVR . . . . . . Cockpit Voice RecorderCKPT . . . . . Cockpit CW . . . . . . . ClockwiseCKT . . . . . . Circuit CYL . . . . . . CylinderCLB . . . . . . Climb


Page 2

DDA . . . . . . . Drift Angle DG . . . . . . . Directional GyroDBU . . . . . . Data Base Unit DH . . . . . . . Decision HeightDC . . . . . . . Direct Current DIFF . . . . . . DifferentialDCP . . . . . . Display Control Panel DIM . . . . . . DimmingDCU . . . . . . Data Concentrator Unit DIR . . . . . . . DirectDECEL . . . Decelerate(d) DIS . . . . . . . Distance (to way point),DisconnectDECR . . . . Decrease DISC . . . . . DisconnectDEFL . . . . . Defuel DISCH . . . . DischargeDEG . . . . . . Degree DISP . . . . . Dispatch, DisplayDEPR . . . . Depressurize DIST . . . . . DistanceDEPT . . . . . Departure DME . . . . . . Distance Measuring EquipmentDEST . . . . . Destination DN . . . . . . . DownDET . . . . . . Detector DOT . . . . . . Department of Transport(Canada)DEV . . . . . . Deviation DR . . . . . . . DoorDFDAU . . . Digital Flight Data AcquisitionUnitDFDR . . . . Digital Flight Data Recorder

EEAS . . . . . . Equivalent Airspeed EMER(G) . EmergencyECP . . . . . . EICAS Control Panel ENG . . . . . . EngineECS . . . . . . Environmental Control System EPC . . . . . . External Power ContactorECU . . . . . . Electronic Control Unit EQUIP . . . . EquipmentED . . . . . . . EICAS Display ERP . . . . . . Eye Reference Position DatumEDP . . . . . . Engine Driven Pump/EnginePrimary Hydraulic Pump ESS . . . . . . Essential

EFIS . . . . . . Electronic Flight InstrumentSystem ET . . . . . . . Elapsed TimeEGT . . . . . . Exhaust Gas Temperature ETA . . . . . . Estimated Time of ArrivalEICAS . . . . Engine Indication and CrewAlerting System EVAC . . . . . EvacuationEL . . . . . . . . Elevation EXH . . . . . . ExhaustELEC . . . . . Electrical EXTIN . . . . Extinguish(ed)ELEV . . . . . Elevator, ElevationELT . . . . . . Emergency Locator Transmitter


Page 3

FF/CTL . . . . Flight Controls FL CH . . . . Flight Level ChangeFAA . . . . . . Federal Aviation Administration(USA) FLD . . . . . . FieldFAIL . . . . . . Failure FLT . . . . . . . FlightFCC . . . . . . Flight Control Computer FLT DIR . . . Flight DirectorFCU . . . . . . Fuel Control Unit FLUOR . . . FluorescentFD, F/D . . . Flight Director FLX . . . . . . Flex thrust (Reduced take-offthrust)FDAU . . . . . Flight Data Acquisition Unit FM . . . . . . . Fan MarkerFDR . . . . . . Flight Data Recorder (Digital) FMS . . . . . . Flight Management SystemFECU . . . . . Flaps Electronic Control Unit FPM . . . . . . Feet Per MinuteFEED . . . . . Feeder FREQ . . . . FrequencyFF, F/F . . . . Fuel Flow FT . . . . . . . . Feet, FootFIRE BTL . Fire Bottle FW . . . . . . . Fire WallFIREX . . . . Fire Extinguisher FWD . . . . . Forward

GG (+/--) . . . . Receiver Gain GMT . . . . . . Greenwich Mean TimeG/S . . . . . . . Glide slope GND . . . . . . GroundGA . . . . . . . Go-around GPM . . . . . Gallons Per MinuteGAL . . . . . . Gallon GPWS . . . . Ground Proximity WarningSystemGALY . . . . . Galley GR . . . . . . . GearGCS . . . . . . Ground Clutter Suppression GRAV . . . . GravityGCU . . . . . . Generator Control Unit GS . . . . . . . Ground SpeedGE . . . . . . . . . General Electric Aero Engines GUIDE . . . . GuidanceGEN . . . . . . Generator GW . . . . . . . Gross WeightGLD . . . . . . Ground Lift Dumper (ing)

HHDG . . . . . . Heading HP . . . . . . . High PressureHDG HOLD Heading Hold HPA . . . . . . . . . Hecto PascalsHDG SEL . Heading Select HSI . . . . . . . Horizontal Situation IndicatorHEAT . . . . . Heater HSTA . . . . . Horizontal Stabilizer TrimActuatorHF . . . . . . . High Frequency (3 -- 30 mHz) HSTCU . . . Horizontal Stabilizer TrimControl UnitHg . . . . . . . Mercury HTR . . . . . . HeaterHGS . . . . . . Head-up Guidance System HUD . . . . . . Heads-up DisplayHI . . . . . . . . High HYD . . . . . . HydraulicHLDR . . . . . Holder Hz . . . . . . . . HertzHOR,HORIZ . . . . HorizontalHOT . . . . . . High Oil Temperature


Page 4

II/B . . . . . . . . Inboard INCR . . . . . IncreaseI/C . . . . . . . Intercom, Inspection Check IND . . . . . . . Indication, IndicatorIAPS . . . . . Integrated Avionics ProcessorSystem INFLT . . . . . In FlightIAS . . . . . . . Indicated Air Speed INHIB . . . . . InhibitICAO . . . . . International Civil AviationOrganization INOP . . . . . InoperativeICS . . . . . . . Idle Corrected Speed INPH . . . . . InterphoneID . . . . . . . . Identification INSP . . . . . InspectionIDENT . . . . Identification INST(S) . . . Instrument(s)IDG . . . . . . Integrated Drive Generator INST,INSTR . . . . InstrumentIFR . . . . . . . Instrument Flight Rules INT . . . . . . . Internal, Integral, IntersectionIGN . . . . . . Ignition INTEG . . . . IntegralILS . . . . . . . Instrument Landing System IRS . . . . . . . Inertial Reference SystemIM . . . . . . . . ILS Inner Marker IRU . . . . . . . Inertial Reference UnitIMC . . . . . . Instrument MeteorologicalConditions ISA . . . . . . .

International StandardAtmosphere

IMP . . . . . . Imperial ISO . . . . . . . International StandardOrganizationIN . . . . . . . . Inch, Inches ISOL . . . . . Isolation, IsolatedIN Hg . . . . . Inches of Mercury ITT . . . . . . . Inter Turbine TemperatureINBD . . . . . Inboard

JJAA . . . . . . Joint Airworthiness Authority

KK, KT, KTS Knots KIAS . . . . . Knots Indicated Airspeedkg(s) . . . . . . Kilogram(s) kW(s) . . . . . KiloWatt(s)kHz . . . . . . . KiloHertz


Page 5

LL . . . . . . . . . Left, Landing LK . . . . . . . . LeakL/T . . . . . . . Landing/Taxi LN . . . . . . . Left NoseLAV . . . . . . Lavatory LNAV . . . . . Lateral Navigationlb . . . . . . . . Pound(s) LOC . . . . . . ILS LocalizerLB(s) . . . . . Pound(s) LOGO . . . . Logo GraphicLCN . . . . . . Load Classification Number LOM, MM . Compass Locator at OuterMarkerLCV . . . . . . Load Control Valve LOP . . . . . . Low Oil PressureLDA . . . . . . Localizer-Type Directional Aid LP . . . . . . . . Low PressureLDG . . . . . . Landing LPM . . . . . . Liter Per MinuteLDG GR . . Landing Gear LR . . . . . . . Left RearLDU . . . . . . Lamp Driver Unit LRC . . . . . . Long Range CruiseLE . . . . . . . . Leading Edge LSB . . . . . . Lower Side BandLG . . . . . . . Landing Gear LT(s) . . . . . Light(s)LGC . . . . . . Landing Gear Controller LW . . . . . . . Left WingLGW . . . . . Landing Gross Weight LWD . . . . . . Left Wing DownLH . . . . . . . Left Hand LWR . . . . . . LowerLIM . . . . . . . Limit

MM . . . . . . . . Mach Number MIC . . . . . . Microphonem . . . . . . . . Meter MID AFT . . Middle AfterwardMAA . . . . . . Maximum Authorized IFRAltitude MID FWD . Middle ForwardMAC . . . . . . Mean Aerodynamic Chord MILS . . . . . .001 of an inchMAG . . . . . Magnetic MIN . . . . . . MinimumMAINT . . . . Maintenance MISC . . . . . MiscellaneousMALF . . . . . Malfunction MKR . . . . . . MarkerMAN . . . . . . Manual MLG . . . . . . Main Landing GearMAP . . . . . . Ground Map (WXR) MLS . . . . . . Microwave Landing SystemMAX . . . . . . Maximum MLW . . . . . Maximum Landing WeightMAZ . . . . . . MLS Azimuth MM . . . . . . . ILS Middle MarkerMB . . . . . . . Millibars MMEL . . . . Master Minimum Equipment List�� MMO . . . . . Maximum Operating Speed inMach NumberMCA . . . . . . Minimum Crossing Altitude MOCA . . . . Minimum Obstruction ClearanceAltitudeMCT . . . . . . Maximum Continuous Thrust MOD . . . . . ModuleMDA . . . . . . Minimum Descent Altitude MON . . . . . MonitorMEA . . . . . . Minimum Enroute IFR Altitude MPH . . . . . . Miles Per HourMECH . . . . Mechanic MRA . . . . . . Minimum Reception AltitudeMED . . . . . . Medium MSG . . . . . MessageMEL . . . . . . Minimum Equipment List MSL . . . . . . Mean Sea LevelMFD . . . . . . Multifunction Display MTG . . . . . . Miles to GoMGP . . . . . MLS Glideslope MTOW . . . . Maximum Takeoff WeightMHz . . . . . . MegaHertz MTW . . . . . Maximum Taxi WeightMI . . . . . . . . Miles MZFW . . . . Maximum Zero Fuel Weight


Page 6

MISC% . . . . . . . . Percent �C . . . . . . . . Degrees Centigrade& . . . . . . . . . and �F . . . . . . . . Degrees Fahrenheit

NN/A . . . . . . . Not applicable NLG . . . . . . Nose Landing GearN1 . . . . . . . Low Pressure Rotor NM . . . . . . . Nautical Mile(s)N2 . . . . . . . High Pressure Rotor No. . . . . . . . NumberNAV . . . . . . Navigation NOPT . . . . No Procedure Turn RequiredND . . . . . . . Nose Down, Navigation Display NORM . . . . NormalNDB (ADF) Nondirectional Beacon(Automatic Direction Finder) NOSE . . . . Nose WheelNEG . . . . . . Negative NR . . . . . . . Nose RightNEUT . . . . . Neutral NTO . . . . . . Normal Take-OffNL . . . . . . . Nose Left NU . . . . . . . Nose Up

OOAT . . . . . . Outside Air Temperature OVBD . . . . OverboardOB/OUTBD Outboard OVHT, OH . OverheatOBS . . . . . . Observer OVLD . . . . . OverloadOEI . . . . . . . One Engine Inoperative OVSP . . . . OverspeedOEW . . . . . Operating Empty Weight OVSPD . . . OverspeedOH, OVHD Overhead OVTEMP . . Over TemperatureOK . . . . . . . Okay OXY, O2 . . . . OxygenOM . . . . . . . ILS Outer Marker


Page 7

PP#6 . . . . . . Panel 6 PRESS . . . Pressure, PressurizationP/S . . . . . . . Pitot/Static PRI . . . . . . . PrimaryPA . . . . . . . Passenger Address PRIM . . . . . PrimaryPASS . . . . . Passenger PROC . . . . ProcedurePBE . . . . . . Portable Breathing Equipment(Smoke Hood) PROT . . . . ProtectionPCU . . . . . . Power Control Unit PROX . . . . ProximityPF . . . . . . . Pilot Flying PSEU . . . . . Proximity Sensor ElectronicsUnitPFD . . . . . . Primary Flight Display PSI . . . . . . . Pounds Per Square InchPLA . . . . . . Power Lever Angle PSIG . . . . . Pounds Per Square Inch GaugePLT(s) . . . . Pilot(s) PSS . . . . . . Proximity Sensor SystemPNF . . . . . . Pilot Not Flying PSU . . . . . . Passenger Service UnitPNLS(s) . . Panel(s) PT2 . . . . . . Engine Inlet PressurePO . . . . . . . Outside Air Pressure PTCT . . . . . ProtectPOS . . . . . . Position PTT . . . . . . Push To TalkPPH . . . . . . Pounds Per Hour PWR . . . . . Power

QQAR . . . . . . Quick Access Recorder QNH . . . . . . Altimeter SettingQEC . . . . . . Quick Engine Change QTY . . . . . . QuantityQFE . . . . . . Local Station Pressure

RR . . . . . . . . . Right RNAV . . . . . Area NavigationRA . . . . . . . Radio Altitude ROT . . . . . . RotationRAI . . . . . . . Registro Aeronautico Italiano(Italy) RPM . . . . . . Revolutions Per MinuteRAT . . . . . . Ram Air Turine RT, R/T . . . Receiver-TransmitterRCCB . . . . Remote Controlled CircuitBreaker RTE . . . . . . RouteRCDR . . . . Recorder RTE DATA Route DataRCVR . . . . Receiver RTO . . . . . . Rejected TakeoffRDR . . . . . . Radar RTU . . . . . . Radio Tuning UnitREC . . . . . . Receiver, Recorder RUD . . . . . . RudderRECOG . . . Recognition RVR . . . . . . Runway Visual RangeREF(s) . . . . Reference(s) RVSR . . . . ReverserREFL . . . . . Refuel RW . . . . . . . Right WingREV . . . . . . Reverse RWD . . . . . Right Wing DownRH . . . . . . . Right Hand RWY . . . . . RunwayRMI . . . . . . Radio Magnetic Indicator


Page 8

SS . . . . . . . . . Status SPKR . . . . . SpeakerSAT . . . . . . Static Air Temperature SPLR(s) . . Spoiler(s)SCAV . . . . . Scavenge SQL . . . . . . SquelchSDF . . . . . . Simplified Directional Facility SSB . . . . . . Single Side BandSEC . . . . . . Second, Secondary STA . . . . . . StationSECS . . . . . Spoiler Electronic ControlSystem STAB . . . . . StabilizerSECU . . . . Spoiler Electronic Control Unit STAT . . . . . StatusSEL . . . . . . Select, Selector STBY . . . . . StandbySELCAL . . Selective Call STEER . . . SteeringSENS . . . . . Sensitivity, Sensor SUPPL . . . SupplySERV,SVCE . . . . . Service SW(s) . . . . SwitchesSMKG . . . . Smoking SYN . . . . . . SynchronizeSOV . . . . . . Shutoff Valve SYNC . . . . SynchronousSP, SPD . . Speed SYS, SYST SystemSPC . . . . . . Stall Protection Computer

TT/C . . . . . . . Top of Climb TGT . . . . . . TargetT/D . . . . . . . Top of Descent TO, T/O . . . TakeoffT/R . . . . . . . Thrust Reverser �� TACAN . . . UHF Tactical Air Navigation Aid TOL . . . . . . ToleranceTAS . . . . . . True Airspeed TRB, TURB TurbulenceTAT . . . . . . Total Air Temperature TRK . . . . . . TrackTCAS . . . . . Traffic Alert and Collision

Avoidance System TRM . . . . . . TrimTE . . . . . . . Trailing Edge TRU . . . . . . Transformer Rectifier UnitTEMP . . . . Temperature TT2 . . . . . . Engine Inlet Temperature

UUNSCHD . Unscheduled USG . . . . . . United States GallonsUSB . . . . . . Upper Side Band UTIL . . . . . . Utility


Page 9

V

V . . . . . . . . . VoltVS0 . . . . . . . . . . . . Stalling Speed or the Minimum

Steady Flight Speed in theLanding Configuration

VA . . . . . . . . . . . . . . Design Maneuvering SpeedVS1 . . . . . . . . . . . . Stalling Speed or the Minimum

Steady Flight Speed Obtainedin a Specific Configuration

VB . . . . . . . . . . . . . . Design Speed for MaximumGust IntensityV1 . . . . . . . . . . . . . . Takeoff Decision Speed (former-

ly Denoted as Critical EngineFailure Speed)

VC . . . . . . . . . . . . . Design Cruising Speed V2 . . . . . . . . . . . . . . Takeoff Safety SpeedVD . . . . . . . . . . . . . Design Diving Speed V2 MIN . . . . . . . . . . Minimum Takeoff Safety SpeedVDF/MDF . . . . . . Demonstrated flight divingspeed. V/S . . . . . . . Vertical SpeedVEF . . . . . . . . . . . . Engine Failure Speed VERT . . . . . VerticalVF . . . . . . . . . . . . . . Design Flap Speed VFR . . . . . . Visual Flight RulesVFC /MFC . . . . . . Maximum Speed for StabilityCharacteristics VG . . . . . . . Vertical Gyro

VFE . . . . . . . . . . . . Maximum Flap Extended Speed VHF . . . . . . Very High Frequency(30 -- 300 mHz)VLE . . . . . . . . . . . . Maximum Landing GearExtended Speed VIB . . . . . . . Vibration

VLO . . . . . . . . . . . . Maximum Landing GearOperating Speed VMC . . . . . .Visual Meteorological Condi-tions

VLOF . . . . . . . . . . . Lift-off Speed VNAV . . . . . Vertical NavigationVMC . . . . . . . . . . . . Minimum Control Speed withthe Critical Engine Inoperative VOL . . . . . . Volume

VMO/MMO . . . . . Maximum Operating LimitSpeed VOLT . . . . . Voltage

VMU . . . . . . . . . . . . Minimum Unstick Speed VOR . . . . . . VHF Omnidirectional RangeStationVR . . . . . . . . . . . . . Rotation Speed VORTAC . . VOR and TACAN Co-located

VS . . . . . . . . . . . . . .Stalling Speed or the MinimumSteady Flight Speed at whichthe Airplane is Controllable

VSI . . . . . . . Vertical Speed Indicator

WW . . . . . . . . Warning WIND . . . . . WindowW/C . . . . . . Wind Component WOW . . . . . Weight-On-WheelW/S . . . . . . Wind Shear WPT(s) . . . Waypoint(s)W/W . . . . . . Wheel Well WRN . . . . . WarningWARN . . . . Warning WS . . . . . . . Second Segment LimitedWeightWF . . . . . . . Runway Length Limited Weight WSHLD . . . WindshieldWGT . . . . . Weight WX . . . . . . . WeatherWHLS . . . . Wheels WXR . . . . . Weather Radar


Page 10

XX . . . . . . . . . Cross Transfer XPNDR . . . TransponderXFER, XFR Transfer XTK . . . . . . Cross TrackXFLOW . . . Cross Flow XWC . . . . . Cross Wind ComponentXMIT . . . . . Transmit

YYD, Y/D . . . Yaw Damper

ZZFW . . . . . . Zero Fuel Weight


Page 11

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Page 12

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Page 14

56�� 7�� !"

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6.2 M(20 FT 4 IN)

2.7 M(8 FT 10 IN)

11.1 M36 FT 4 IN

1.6 M(5 FT 1 IN)

1.5 M(5 FT)

2.9 M(9 FT 6 IN)

6.299 M(20 FT 8 IN)

0.914 M(3 FT)

3.74 M(12 FT 3 IN)

21.21 M(69 FT 6 IN)

1.45 M(4 FT 9 IN)

3.1 M(10 FT 4 IN)

24.29 M(80 FT 4 IN)

26.77 M(87 FT 10 IN)


Page 15

5� �� (�8�� !"

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544 MPH

272 MPH

68 MPH

34 MPH

136 MPH

68 MPH

34 MPH

20 MPH

136 MPH

IDLETHRUST

MAXIMUMTHRUST

18 FT

IDLETHRUST

25 FT12 FT

APU EXHAUSTDANGER AREA(15 FEET)

18 FT

0

10

20

30

40

50 FT

60

70

80

90

100 FT

110

120

130

140

150 FT

160

170

0

10

20

30

40

50 FT

60

70

80

90

100 FT

110

120

130

140

150 FT

160

170

MAXIMUMTHRUST


Page 16

�6�� 9�� !"

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12.57 M(41 FT 3 IN)

15.7 M(51 FT 5 IN)

TURNCENTER

14.54 M(47 FT 7 IN)

16.3 M(53 FT 6 IN)


Page 17

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NO. 3 HYDRAULIC SYSTEMACCUMULATOR CHARGINGPOINT AND PRESSURE GAUGE

OVERWING GRAVITYFUEL FILLER (TYP)

FUEL LEVELINDICATOR

PRESSURE REFUEL/DEFUELPANEL AND ADAPTER

OXYGEN SYSTEMCHARGING VALVEAND GAUGE

AC EXTERNALPOWER

BRAKE ACCUMULATORCHARGING POINTSAND INTERPHONE

FUEL LEVELINDICATORS FUEL LEVEL

INDICATORFUEL TANKWATER DRAIN(TYP)

NO. 3 HYDRAULICSYSTEM

NO. 3 HYDRAULIC SYSTEMRESERVOIR FILLERCONNECTION

GROUND AIRCONNECTION

ENGINE OIL TANK

DC EXTERNALPOWER

LOW PRESSUREAIR GROUNDCONNECTION

NO. 2 HYDRAULICSYSTEM

NO. 1 HYDRAULICSYSTEM AND REARINTERPHONE

OIL REPLENISHMENTTANK PANEL(AFT EQUIPMENT BAY)


Page 18

Airplane Parking and MooringFigure 01--20--5

AIR DRIVENGENERATORLOCKING PIN

NOSE GEARLOCKING PIN

MAIN GEARLOCKING PIN

CHOCKSCHOCKS

PICKETING KIT

PICKETING KIT

B

B

C

C

D

D

E

E

F

G

G H

H

A

A

F


Page 19

Covers and PlugsFigure 01--20--6

ACU EXHAUST

RAM AIR INTAKE

APU EXHAUST

ICE DETECTORPROBE (LEFT & RIGHT) STATIC PRESSURE

SENSOR (LEFT & RIGHT)

HEAT EXCHANGERINLET

PITOT HEADS(LEFT & RIGHT)

ANGLE OF ATTACKTRANSDUCER VANE

ENGINEEXHAUST

ENGINE AIRINTAKE

A

A

B

B

C

C

D

D

E

E

F

F

G

H

G

H


Page 20

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WEATHERRADAR

GLIDESLOPE

VOR ANDLOCALIZER(BOTH SIDES)

EMERGENCYLOCATORTRANSMITTER

UNDERWATERLOCATORBEACONS(CVR AND FDR) MARKER BEACON 1MARKER BEACON 2

VHF 2ATC 2(BOTH SIDES)

TCASOMNIDIRECTIONAL

TCASDIRECTIONAL

ATC 2ATC 1 OTHER SIDE

VHF 3

VHF 1

ADF

RADIOALTIMETER DME 2

DME 1OTHER SIDE

RADIOALTIMETER

HF

GPS(BOTH SIDES)


Page 21

(�8��

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RADAR 25 WATT60 Centimeters (2 Feet)with radome closed.

HF ANTENNA175 watt (peak)50 watt (average)


Page 22

�� Airplanes 7002 to 7451, �� !"

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TWO INSTRUMENTS ARE TYPICAL.ONE UNIT ONLY FOR OPTION WHICH IS TOP UNIT.

NOTE

1

2

4

56

8

13

13

3

11

12

9

14

17

10

719

18

15

3

16

Indicates Chapter in which information on item may be found.

Effectivity:Airplanes 7002 to 7451.

17

LEGEND

125

12

1. Flight bag storage unit.2. Storage pocket.3. Circuit breaker panel (see next page).4. Check list holder.5. Chart holder (adjacent to

pencil holder and map light).6. Sun visor.7. HGS combiner .8. Overhead speaker.9. HGS overhead unit .

812

1

1

10. Hand hold.11. Crew escape hatch.12. Escape rope.13. Gaspers.14. Compass calibration card.15. Eye reference position datum.16. Pencil holder.17. Cup holder.18. Airplane operating manual storage unit.19. Integrated STD instrument

99


Page 23

�� Airplanes 7452 and Subsequent, �� !"

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Effectivity:Airplanes 7452 and subsequent.

LEGEND

11

11

1. Flight bag storage unit.2. Storage pocket.3. Circuit breaker panel (see next page).4. Check list holder.5. Chart holder (adjacent to

pencil holder and map light).6. Sun visor.7. HGS combiner .8. Overhead speaker.9. HGS overhead unit .

TWO INSTRUMENTS ARE TYPICAL.ONE UNIT ONLY FOR OPTION WHICH IS TOP UNIT.

NOTE

10. Hand hold.11. Crew escape hatch.12. Escape rope.13. Gaspers.14. Compass calibration card.15. Eye reference position datum.16. Pencil holder.17. Cup holder.18. Airplane operating manual storage unit.19. Integrated STD instrument

1

2

4

56

108

13

13

3

11

12

9

14

17

719

18

15

3

16

1

812

19

9

17

5


Page 24

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FLIGHT BAGCOMPARTMENT

NOSE WHEELSTEERING TILLER

OXYGEN MASKREGULATORSTORAGECOMPARTMENT

AIRCONDITIONINGSYSTEMOUTLET

ENGINEOIL LEVELPANEL SOURCE

SELECTOR/ISOLATIONVALVES 12

RHSTOP/STARTLH

16

20

9

SELECTORVALVE CLOSED

MACHTRANSDUCER

PITOT


MACHTRANSDUCER

STATICNORMAL NORMAL

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS

AIR CONDITIONINGSYSTEM INTAKE

5

MICHDPH


Page 28

)��=� �� )�� Airplanes 7002 to 7672,�� !"

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'


6. Stall protection panel.7. Lighting panel.8. Nose wheel steering subpanel.9. Air conditioning system gasper.

LEGEND1. Clock.2. Display control panel.3. Air data reference panel.4. Display reversionary panel.5. Windshield wiper control

panel.

1

2

3

4

7

6

9

NORM

PFD 1 EICAS

STALLPTCT

PUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF

NAVSOURCE

FORMAT RANGE

N/W STRGARMED

OFF

8

5

LIGHTINGFLOODDSPL INTEG

OFF OFF OFFBRT BRT BRT

OFF

ON

FLOOR

BARO

HPA/INMDADH

SPEED REFS

SEL

RA TESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE


12

215

12 1812 18 17

11

168


Page 29

)��=� �� )�� Airplanes 7673 and Subsequent, �� !"

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'


6. Stall protection panel.7. Lighting panel.8. Nose wheel steering subpanel.9. Air conditioning system gasper.

LEGEND1. Clock.2. Display control panel.3. Air data reference panel.4. Display reversionary panel.5. Windshield wiper control

panel.

1

2

3

4

7

6

9

NORM

PFD 1 EICAS

STALLPTCT

PUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF

NAVSOURCE

FORMAT RANGE

N/W STRGARMED

OFF

8

5



OFFON

FLOOR

BARO

HPA/INMDADH

SPEED REFS

SEL

RA TESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE

RST

SEL

ET

MODE

CHR

INT

CHR


215

12 1812 18

1217

11

168


Page 30

)��=� *�� )�� !"

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FLIGHTDIRECTOR / AUTOPILOTMODE ANNUNCIATOR

ALTIMETER

ATTITUDEDIRECTORINDICATOR

AIRSPEEDLIMITSPLACARD(TYPICAL)

PRIMARYFLIGHTDISPLAY

AIRSPEEDINDICATOR

NAVIGATIONANNUNCIATORS

COCKPITVOICERECORDER

HORIZONTALSITUATIONINDICATOR

VERTICAL SPEEDINDICATORAND TCASRESOLUTIONADVISORY

10

10

MULTIFUNCTIONDISPLAY

HSI MODENAVAID SECTORMAPPRESENTPOSITION MAPPLAN MAPTCAS TRAFFICWEATHERRADAR12

12

18

1812

5 12

18

18

FMS 2

FMS


Page 31

�� *�� )�� !"

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NOTE


MLG BAY OVHTDISPLAY COOL

Standby AttitudeIndicator 12

Standby Airspeed /Altitude / AttitudeIndicator 12

StandbyAltimeter/IndicatedAirspeed Indicator

12

8

Engine Indication and Crew AlertingSystem (EICAS) Primary Display

Engine InstrumentsCaution and Warning AnnunciatorFuel Flow and QuantityFlap Position IndicatorLanding Gear IndicatorPressurization Indicator (Manual Mode)

202

1311

16

EICAS Secondary DisplayAirplane Status Information(Messages, surface position, APUinstruments)Environmental Control SystemElectrical SystemFuel SystemFlight ControlsAnti--IceDoorsMenu (Flight No., N1 Bugs, Fuelreset) 2

615

1113

78

2

Placards apply onlyto aircraft with enginesmixed 3A1/3B1

KNOTS

mb/hPa In Hg

180 200 220 250

IAS


Page 32

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1. Electrical Power Panel2. Bleed Air Panel3. Fuel Panel4. Cabin Pressurization Panel5. Air--Conditioning Panel6. APU Panel7. Anti--Ice Panel8. Engine/Ignition Panel9. Miscellaneous Lights Panel

10. Hydraulic Panel11. Emergency Lights Panel12. Passenger Signs Panel13. Passenger Oxygen Panel14. Standby Compass15. Emergency Locator Transmitter16. Landing/Taxi Lights Panel17. External Lights Panel18. Fire Detection Panel

LEGEND

9

9

1714

1

12

1717

101720

8

719

13

84

15

CKPT CABIN

COLDHOTAIR

CARGOOFF

COND.

FA

CKPT CABIN

COLDHOT

OFF

FAN

N

FAIL

BOTTLEAPU

18

1

2 3 4

6

8

111213

14

15

17

16

5

7

910

15

ELT

MAN

ARM/RESET

AUTO

OFFON

OFFON

STROBE WINGINSP

MISC LTS

OFFON

DIM

STBYCOMP

OFF

DOMELIGHT

ONOFF

STERILE

ON

PASS SIGNS

APU

OFFON

OFFON

OFFON

NAV BEACON STROBEWING

EXTERNAL LTSINSP

OFFON

AUTOOFF OFF

ON

AUTOOFFON

AUTO

1 3A 3B 2

ON

HYDRAULIC

AIR--CONDITIONING

WING

OFFON

TEST

PROBESLH RH

LOWHI

LOWHI

OFF/RESETLH

MISC LTSOVHD

DIM BRT

OFFON

DIM

STBYCOMP

OFF

DOMELIGHT

PWRFUEL

START

FAILSOVFAILPUMP

ONINOP INOP

ON

FAIL FAILONON

OPEN

L R

L BOOSTPUMP

R BOOSTPUMP

FUEL

BLEED AIR14TH STAGE

10TH STAGEL ISOL R

L APU LCV ISOL R

CLOSED CLOSED

CLOSED CLOSEDOPENOPEN

OPENDUCTFAIL

DUCTFAIL

DUCTFAIL

DUCTFAILFAIL

TESTNORM

LOOP ALOOP B

DUCTMON

XFLOWGRAVITY

FAIL

XFLOWAUTO OVERRIDE

FIREX MONITOR

FIRE DETECTION

FAIL

BOTTLEENGINE BOTTLE

LH APU RH TESTWARNJETENG

ABOTH

B

JET ENG

NORM

TEST

NORM

TEST

1 APU2

ANTI--ICE

RHWSHLDOFF/RESET

START/STOP

AVAIL

ON

PASS OXY

STANDBY COMPASS WITH ALL RADIOS ON SWUNG BYTO FLY

STEER

N 45 E 135 S 225 W 315

EMER LTSNO

SMKGSEATBLTS

ONOFF

AUTO

ONOFFARMOFF

ELT

ON

ARM/RESET

FOR AVIATIONEMER USE ONLY

ELT

ON

NORMTEST 1

TEST 2

BOTTLECARGO

LOGO

OFFON

OFFON

NAV

EXTERNAL LTS

OFFON OFFON OFFONNAV BEACON STROBE

WINGEXTERNAL LTS

INSP

OFFONOFFON

LOGO


Page 33

�� !"

+!

%

RIGHT GLARESHIELD

LEFT GLARESHIELD

CENTER GLARESHIELD

1 2 3 4 5 6

7

9 6

5

12

34

8

7 7


LEGEND1. Roll Select Switch/Light.2. Master Warning Switch/Light.3. Master Caution Switch/Light.4. Stall Warning Switch/Light.5. GPWS and Glideslope Warning

Switch/Light.PULL UP / GND PROX GlideslopeSwitch/Light.

6. Engine Fire Warning Switch/Light.7. Firex Bottle Discharge Switch/Lights.8. Flight Control Panel.9. APU Fire Warning Switch/Light.

112

211

18

1010

310

18


Page 34

�� )�� 31��4 �� !"

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FMS

1 2 3

4 5 6

7 8 9

0

A

F

K

P

U

Z

B

G

L

Q

VSP

C

H

M

RW

DEL

D

I

N

S

X

/

E

J

O

T

YCLR

MOD BRT

MSG DIRINTC

PREVPAGEFPLN

NEXTPAGE

EXECMDCUMENULEGS

HOLD

VNAV

DEPARR

SECFPLN

RADIO PERF

MFDMENU

PROG

MFDADV

MFDDATA

RADIORADIO

INDEX FIX

1

1

746

32 5

OVSPTEST

FDREVENT

LAMPTEST

1

2

INDLTS

BRT

DIM

AURALWARN TEST

1

2OFF

1

2

MECH

PUSH

CALL

LDG GEAR

HORNBTMS OVHTWARN RESET

OFF

ARMEDANTI SKID

DN LCKREL

OVHT TESTWARN FAIL

MLG BAYOVHT

UPDN

MUTED

TEST

MECH

PUSH

CALL

FLAP

OVRD

TERRAIN

OFF

GRND PROX

8

1616

1616

5

2

12

5

FMS

1 2 3

4 5 6

7 8 9

0

A

F

K

P

U

Z

B

G

L

Q

VSP

C

H

M

R

W

DEL

D

I

N

S

X

/

E

J

O

T

YCLR

MOD BRT

MSG DIRINTC

PREVPAGEFPLN

NEXTPAGE

EXECMDCUMENULEGS

HOLD

VNAV

DEPARR

SECFPLN

RADIO PERF

MFDMENU

PROG

MFDADV

MFDDATA

RADIORADIO

INDEX FIX

1. FMS control display unit.2. Brake temperature monitoring system subpanel.3. Landing gear control panel.4. EICAS test panel.5. Antiskid system control panel.6. Main landing gear overheat test panel.7. Interphone panel.8. EGPWS/mechanic call panel.

LEGEND


Page 35

�� )��

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8


6

41 3

9

2

5

7

Option removesGround ProximityWarning System/FlapOverride Switch

1. Spoilers System Control Subpanel2. Pitch Disconnect Control3. Spoilers Lever Panel4. Roll Disconnect Control5. Flap Lever Panel6. Ground Proximity Warning System/Flap

Override Switch7. Metric Altimeter Subpanel 8. Thrust Lever Quadrant9. Thrust Reverser Subpanel

1111

1111

11

11

2020

LEGEND

12


Page 36

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3

45

789

103

16

14

2

1315 16

17

18

19

6

3

1

ACTSTBY

ELVG/S

FAULT CLR BRT + DIM --

1 2 34 5 67 8 9

ENTER 0 TEST

HGS

CARGOARMED

CARGO FIREX

STANDBYNORMAL

SMOKEPUSH

BOTTLEPUSH TO

DISCH

CARGOARMEDSMOKE

PUSH

BOTTLEPUSH TODISCH

6

20

PA

12

16A

PA

LEGEND

16

1212

8

511

16

12

718

11

7

5

10

11

18

25 18

17

11

2 12

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FMS 2

FMS

FLIGHTDIRECTOR / AUTOPILOTMODE ANNUNCIATOR

ATTITUDEDIRECTORINDICATOR

AIRSPEED LIMITSPLACARD (TYPICAL)

PRIMARYFLIGHTDISPLAY

AIRSPEEDINDICATOR

NAVIGATIONANNUNCIATORS

HORIZONTALSITUATIONINDICATOR

VERTICAL SPEEDINDICATORAND TCASRESOLUTIONADVISORY

18

1812

1812

123

12

ALTIMETER

MULTIFUNCTIONDISPLAY

HSI MODENAVAID SECTORMAPPRESENTPOSITION MAPPLAN MAPTCAS TRAFFICWEATHER RADAR

18

10

10

11


Page 38

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1 2

4 5

3

6

7

8

STALLPTCT

PUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF



OFFON

FLOOR

NORM

PFD 1 EICAS

NAVSOURCE

FORMAT RANGE

BARO

HPA/INMDADH

SPEED REFS

SEL

RA TESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE


LEGEND1. Clock.2. Air conditioning system gasper.3. Lighting panel.4. Windshield wiper control panel.5. Stall protection panel.6. Display reversionary panel.7. Air data reference panel.8. Display control panel.

9

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Page 39

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1 2

4 5

3

6

7

8

STALLPTCT

PUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF



OFFON

FLOOR

NORM

PFD 1 EICAS

NAVSOURCE

FORMAT RANGE

BARO

HPA/INMDADH

SPEED REFS

SEL

RA TESTTGT VSPDS

SET

SET

RST

SEL

ET

MODE

CHR

INTCHR

NAVSOURCE

FORMAT RANGE


LEGEND1. Clock.2. Air conditioning system gasper.3. Lighting panel.4. Windshield wiper control panel.5. Stall protection panel.6. Display reversionary panel.7. Air data reference panel.8. Display control panel.

9

16

208

12

132013

18

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Page 40

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AIRCONDITIONINGSYSTEMOUTLET

AUDIO WARNING

FLIGHT BAGCOMPARTMENT

SOURCESELECTOR/ISOLATIONVALVES


MACHTRANSDUCER

PITOT


MACHTRANSDUCER

STATICNORMAL NORMAL

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS

HDPHMIC

AUDIO WARNING

DATACONCENTRATORUNITAUDIO WARNINGDISABLE SWITCHES

OXYGEN MASKREGULATORSTORAGECOMPARTMENT

COPILOTHAT HOOK

AA

B

B

C

C


Page 41

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OBSERVER’SHEADSETHOOK

OBSERVER’S STATIONRIGHT HAND SIDE

OBSERVER’SSEAT

OBSERVER’S STATIONLEFT HAND SIDE

OBSERVER’SJACK PANEL

OBSERVER’SOXYGENMASK/REGULATORSTORAGEUNIT


Page 42

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STABILIZER TRIMDISCONNECTSWITCH (RED)

INTERCOM/RADIO TRANSMITSWITCH (BLACK)

STABILIZER TRIMLEVER SWITCHES(BLACK)

AUTOPILOT/STICKPUSHER DISCONNECTSWITCH (RED)

FLIGHT DIRECTORSYNC CONTROLSWITCH (BLACK)

PILOT’S CONTROL WHEEL(COPILOT’S OPPOSITE)

REAR VIEW

TOP VIEW

B

A

B

A


Page 43

1. ��

The reinforced flight compartment door is made to enhance the security, protect from ballisticthreat and prevent unauthorized access to the flight compartment. The door is made fromNomex core panels, sandwiched in the middle with a bullet proof insert.

The door consists of:

� Slide latch

� Deadbolt assembly

� Two quick--release hinge pins

� Viewer

� Decompression panel and latch

The slide latch is used to latch and unlatch the door.

The deadbolt assembly is used for added security to lock/unlock the door. A key is requiredto lock/unlock the door from the passenger compartment. To lock/unlock the door from theflight compartment, the deadbolt is manually rotated.

The two quick--release hinge pins are used to remove the door.

The viewer has two lenses (in a 1.5 “ thick plug) to increase the magnification for field ofview and to provide bullet resistance.

The decompression panel is held on the door by decompression latches. When thepressure differential between the passenger cabin and flight compartment is more than apreset limit, the latch releases the panel to equalize the pressure between the twocompartments.

A. Emergency Operation

The following steps are used to remove the door in an emergency if the latch has failedor the door has jammed. From the flight compartment,

(1) Unlock and lift the lower hinge pin

(2) Unlock and pull down on the upper hinge pin

(3) Kick the hinged side of the door towards the cabin

(4) When the door is free, rotate it clockwise and stow it against the galley bulkhead.


Page 44

CAUTION

The lower hinge pin must be released before the upperhinge pin. Failure to do so could result in the doorsuddenly coming disengaged from the hinges causinginjury to persons.

NOTE

In the event that a crew member becomes trapped inthe flight compartment or becomes incapacitated, thedoor can be opened using a crow bar or axe.


Page 45

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HINGE ASSEMBLY

COCKPIT DOOR

HINGE ASSEMBLY

UPPERDECOMPRESSIONPANEL

SLIDELATCH

DEADBOLTASSEMBLY

VIEWER(PEEPHOLEASSEMBLY)

POCKETENCLOSURE

A

AB


Page 46

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B

PRESSURERELEASELATCH

UPPER HINGEHANDLE

RETRACTABLEBOLTS

SLIDELATCH

DEADBOLT

NAMEPLATE

STRAPHANDLE

STRAPHANDLE

UPPER HINGEHANDLE


Page 47

Documents

Canadair Regional Jet 100/200 - Aircraft General...1. ABBREVIATIONS The following abbreviations may be used by flight compartment displays, radio tuning units and flight management