Post on 06-Apr-2022
GENERAL
Abbreviations 01−10−1
Conversion Factors 01−10−13
Temperature Conversion Table 01−10−14
General Airplane Description 01−10−15
Airplane Dimension Schematic 01−10−16
Dimensions and General Data 01−10−17Overall dimension 01−10−17Wing 01−10−17Spar locations 01−10−17Horizontal tail surface 01−10−17Vertical tail surface 01−10−17Fuselage 01−10−17Landing gear 01−10−17Areas 01−10−18Doors 01−10−18Baggage compartment door (LH, aft) 01−10−18
Antenna Location Schematic 01−10−19
Visual Eye References For Ground Operation 01−10−20
Steering Radii 01−10−21
Steering Radii Schematic 01−10−21
Turning Radii 01−10−22
Turning Radii Schematic 01−10−22
Jet Exhaust Single Engine Ground Idle Thrust 01−10−23
Jet Exhaust Single Engine Take-off Thrust 01−10−24
Jet Exhaust Two Engine Ground Idle Thrust 01−10−25
Jet Exhaust Two Engine Take-off Thrust 01−10−26
Airplane Jacking 01−10−27
Jacking Points Schematic 01−10−27
Towing 01−10−28
Tow Bar Attachment Schematic 01−10−28Ground Locking Safety Pins 01−10−28Towbarless Vehicle 01−10−29
Mooring 01−10−30
Mooring Attachment Points Schematic 01−10−30
AIRPLANE GENERAL
TABLE OF CONTENTS
CHAPTER 1
01−00−1
REV 51, Aug 14, 2006 Flight Crew Operating Manual
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Page
TABLE OF CONTENTS
GENERAL
Seat Assembly 01−10−31Seat Egression 01−10−32Moving the Seat Forward 01−10−32
Eye Locator−Seat Adjustment 01−10−33
Control Wheel 01−10−34Master Disconnect 01−10−34Pitch Trim Switch 01−10−34Autopilot/Flight Director (Touch Control) 01−10−34Radio Key 01−10−34
Flight Compartment General Arrangement 01−10−35
Flight Compartment (Aft View) 01−10−36
Pilot’s Side Console 01−10−37
Pilot’s Side Panel 01−10−38
Pilot’s Instrument Panel 01−10−39
Centre Instrument Panels 01−10−40
Overhead Panel 01−10−41
Glareshield 01−10−42
Centre Pedestal 01−10−43
Copilot’s Instrument Panel 01−10−44
Copilot’s Side Panel 01−10−45
Copilot’s Side Console 01−10−46
Airplane Doors 01−10−47
Passenger Door 01−10−47
Passenger Door Schematic 01−10−48
Passenger Door Components 01−10−48Airstair and Handrails Assembly 01−10−48Lift arms 01−10−49“G” Locks 01−10−49Vent Flap 01−10−49Locked Indication 01−10−50
Passenger Door Operating Handles 01−10−51
Passenger Door Switches 01−10−52
External Door Switch Access Panel 01−10−52
Passenger Door Operation 01−10−53External Door Operation 01−10−53Internal Door Operation 01−10−53
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Page
GENERALManual Closing 01−10−53
Emergency Exit 01−10−54
Aft Equipment Bay Door 01−10−56
Aft Equipment Bay Door Schematic 01−10−56Aft Equipment Bay Door Operation 01−10−57
Baggage Compartment Door 01−10−58Baggage Door Operation 01−10−59Baggage Door Indication 01−10−59
Door Indication and Control 01−10−60STAT Page 01−10−60Passenger Door 01−10−60Emergency Exit 01−10−60Baggage Door 01−10−61Large Maintenance Doors 01−10−61Aft Equipment Bay Door 01−10−61Small Service Doors 01−10−61
EICAS Messages 01−10−62
EMS CIRCUIT PROTECTION
CB − Doors Systems 01−20−1
AIRPLANE GENERAL
TABLE OF CONTENTS
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AIRPLANE GENERAL
TABLE OF CONTENTS
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ABBREVIATIONS
The following abbreviations may be used by cockpit displays, radio tuning units and flightmanagement system or be found throughout the manual. Some abbreviations may also appear inlower case letters. Abbreviations having very limited usage are explained in the systems chapterswhere they are used.
A
A/C Air ConditioningA/G Air/GroundA/ICE Anti-iceA/P AutopilotA/S AirspeedA/SKID Anti-skidABS AbsoluteAC Alternating CurrentACARS ARINC Communications
Addressing and ReportingSystem
ACSC Air Conditioning SystemController
ACCEL Acceleration, accelerate(d),accelerometers
ACM Air Cycle MachineACMP Alternating Current Motor
Pump/Electric HydraulicPump
ACPC Alternating Current PowerCenter
ACT ActiveACU Air Conditioning UnitACV Air Control ValveADC Air Data ComputerADDR AddressADF Automatic Direction FinderADI Attitude Director IndicatorADS Air Data SystemAFCS Automatic Flight Control
SystemAFT AftwardAGL Above Ground LevelAHC Attitude Heading ComputerAIL AileronALIGN Aligning, alignmentALPHA alphaALT Altitude, Altimeter
ALT Altitude Hold (PFD/FD)ALT CAP Altitude Capture (PFD/FD)ALT HOLD Altitude HoldALTN AlternateALTS Selected Altitude Arm/Abort
(PFD/FD)AM Amplitude ModulationAMB AmbientAMP AmperesANNUN AnnunciatorANT AntennaAOA Angle of AttackAP AutopilotAPC Auxiliary Power ControlAPP, APR ApproachAPPROX ApproximatelyAPU Auxiliary Power UnitARINC Aeronautical Radio
IncorporatedARP Air Data Reference PanelASCB Avionic Standard
Communication BusASYM AsymmetricalAT Auto ThrottleATA Air Transport AssociationATC Air Traffic ControlATS Air Turbine StarterATT AttitudeATTD AttitudeATTND AttendantAUTO AutomaticAUTO BAL Automatic BalanceAUTO XFER Automatic TransferAUX AuxiliaryAV AvionicsAVAIL AvailableAZ Azimuth
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ABBREVIATIONS (CONT'D)
B
B/AIR Bleed AirB/C, BC Back CourseB/CRS Back CourseBCU Brake Control UnitB/LEAK Bleed LeakBARO BarometricBAT BatteryBATT BatteryBDI Bearing Distance IndicatorBIT Built-In-TestBITE Built-In-Test EquipmentBRK Brake
BLD BleedBMC Bleed Management
ControllerBOOM Headset microphoneBRG BearingBRKR(s) Breaker(s)BRT BrightBTL BottleBTMS Brake Temperature
Monitoring SystemBTMU Brake Temperature
Monitoring UnitBYPS Bypass
C
C Center, Caution, CabinCAI Cowl Anti-IceCAA Civil Aviation Authority (UK)CAIMS Central Aircraft Information
Maintenance SystemCAL CalibrateCAP CaptureCAPT CaptainCAS Calibrated Air SpeedCAS Crew Alerting SystemCAT CategoryCAT II Category IICB, C/B Circuit BreakerCBP Circuit Breaker PanelCCBP Cockpit Circuit Breaker PanelCCW Counter ClockwiseCDL Configuration Deviation ListCDP Compressor Discharge
PressureCDU Control Display UnitCFM Cubic Feet Per MinuteCG Center of GravityCH Chapter, ChannelCL CentrelineCHG Change
CHAN ChannelCHGR ChargerCHRT ChartCK CheckCKPT CockpitCKT CircuitCL ClosedCLB ClimbCLK Clockcm CentimetersCMD CommandCMPS CompassCMPTR ComputerCO2 Carbon DioxideCOM CommunicationCOMM CommunicationCOMP Compressor, ComparatorCOMPT CompartmentCOND Condition, ContinuedCONFIG ConfigurationCONN ConnectionCONT Control, Continuous,
Contactor, ControllerCORR Correction
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ABBREVIATIONS (CONT'D)
CPAM Cabin Pressure AcquisitionModule
CPCP Cabin Pressure ControlPanel
CPC Cabin Pressure ControllerCPCS Cabin Pressure Control
SystemCPL CoupleCPLT CopilotCRS Course
CRT Cathode Ray TubeCRZ CruiseCTR CenterCPCS Cabin Pressure Control
SystemCTRL ControlCVR Cockpit Voice RecorderCW ClockwiseCYL Cylinder
D
DA Drift AngleDCT DirectDAU Data Acquisition UnitDBU Data Base UnitDC Direct CurrentDCP Display Control PanelDCPC Direct Current Power CenterDECEL Decelerate(d)DECR DecreaseDEFL DefuelDEG DegreeDEGRAD DegradedDEPR DepressurizeDEPT DepartureDEST DestinationDET DetectorDEV DeviationDFDAU Digital Flight Data Acquisition
Unit
DFDR Digital Flight Data RecorderDG Directional GyroDH Decision HeightDIFF DifferentialDIM DimmingDIR DirectDIS Distance (to way point),
DisconnectDISC DisconnectDISCH DischargeDISP Dispatch, DisplayDIST DistanceDME Distance Measuring
EquipmentDN DownDOT Department of Transport
(Canada)DR DoorDSPY Display
E
EAS Equivalent AirspeedECP EICAS Control PanelECS Environmental Control
SystemECU Electronic Control UnitED EICAS DisplayEEC Engine Electronic Controller
EDP Engine Driven Pump/EnginePrimary Hydraulic Pump
EFIS Electronic Flight InstrumentSystem
EGPWS Enhanced Ground ProximityWarning System ( includingwindshear)
EGT Exhaust Gas Temperature
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ABBREVIATIONS (CONT'D)
EICAS Engine Indication and CrewAlerting System
EL ElevationELEC ElectricalELEV Elevator, ElevationELT Emergency Locator
TransmitterEMER(G) EmergencyEMS Electrical Management
SystemEMS CDU Electrical Management
System Control Display UnitENG EngineEPC External Power ContactorEPLC External Power Line
ContactorEPCU External Power Control UnitEPGDS External Power Generation
and Distribution System
EPR Engine Pressure RatioEQUIP EquipmentERP Eye Reference Position
(datum)ESS EssentialET Elapsed TimeETA Estimated Time of ArrivalETTC Essential TRU Tie ContactorETOPS Extended Range Twin
Engine OperationEVAC EvacuationEXH ExhaustEXT PWR External PowerEXTIN Extinguish(ed)EVMU Engine Vibration Monitor UnitEVMS Engine Vibration Monitor
System
F
F/CTL Flight ControlsFAA Federal Aviation
Administration (USA)FADEC Full Authority Digital
Electronic ControlFAIL FailureFCC Flight Control ComputerFCU Flight Control UnitFD, F/D Flight DirectorFDAU Flight Data Acquisition UnitFDR Flight Data RecorderFEED FeederFF, F/F Fuel FlowFIDEEX Fire Detection and
Extinguishing SystemFIRE BTL Fire BottleFIREX Fire ExtinguisherFECU Flap Electronic Control Unit
FL Flight LevelFL CH, FLC Flight Level ChangeFLD FieldFLT FlightFLT DIR Flight DirectorFLUOR FluorescentFM Fan MarkerFMS Flight Management SystemFPM Feet Per MinuteFQMC Fuel Quantity Management
ComputerFMQGS Fuel Management Quantity
Gauging SystemFREQ FrequencyFT Feet, FootFW Fire WallFWD ForwardFWC Fault Warning Computer
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ABBREVIATIONS (CONT'D)
G
G (+/−) Receiver GainG/S GlideslopeGA Go-aroundGAL GallonGALY GalleyGCS Ground Clutter SuppressionGCU Generator Control UnitGE General ElectricGEN GeneratorGLC Generator Line ContactorGLD Ground Lift Dumper (ing)GMT Greenwich Mean Time
GND GroundGPM Gallons Per MinuteGPWS Ground Proximity Warning
SystemGR GearG GravityGS,G/S GlideslopeGS Ground SpeedGTC Generator Transfer
ContactorGP Guidance PanelGUIDE GuidanceGW Gross Weight
H
HBMU Heater Current/Brake TempMonitor Unit
HDG HeadingHDG HOLD Heading HoldHDG SEL Heading SelectHEAT HeaterHF High Frequency (3 − 30
MHz)Hg MercuryHI HighHLDR HolderHOR, HORIZ HorizontalHOT Hot Oil Temperature
HP High PressureHPSOV High Pressure Shut-off ValveHPA Hecto PascalsHSI Horizontal Situation IndicatorHSTA Horizontal Stabilizer Trim
ActuatorHSTCU Horizontal Stabilizer Trim
Control UnitHTR HeaterHUD Heads-up DisplayHYD HydraulicHz Hertz
I
I/B InboardI/C Intercom, Inspection CheckIAC Integrated Avionics
ComputerIAPS Integrated Avionics
Processor SystemIAS Indicated Air SpeedICAO International Civil Aviation
Organization
ICS Idle Corrected Speed,Inter-Communication System
ID IdentificationIDENT IdentificationIFR Instrument Flight RulesIGN IgnitionIGV Inlet Guide VanesILS Instrument Landing SystemIM ILS Inner Marker
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ABBREVIATIONS (CONT'D)
IMBAL ImbalanceIMC Instrument Meteorological
ConditionsIMP ImperialIN Inch, InchesIN Hg Inches of MercuryINBD InboardINCR IncreaseIND Indication, IndicatorINFLT In FlightINHIB, INHB InhibitINOP InoperativeINPH InterphoneINSP Inspection
INST(S) Instrument(s)INST, INSTR InstrumentINT Internal, Integral, IntersectionINTEG IntegralI/O Input/OutputIRS Inertial Reference SystemIRU Inertial Reference UnitISA International Standard
AtmosphereISO International Standard
OrganizationISOL Isolation, IsolatedITT Inter Turbine TemperatureIOP Input/Output Processor
J
JAA Joint Airworthiness Authority
K
K, KT, KTS Knotskg(s) Kilogram(s)kHz KiloHertz
KIAS Knots Indicated AirspeedkW(s) KiloWatt(s)
L
L Left, LandingL/T Landing/TaxiLAV LavatoryLB(s) Pound(s)LCN Load Classification NumberLCV Load Control ValveLDG LandingLGDCIS Landing Gear and Door
Control Indicating SystemLDG GR Landing GearLDU Lamp Driver UnitLE Leading EdgeLFE Landing Field ElevationLG Landing Gear
LGECU Landing Gear ElectronicControl Unit
LGW Landing Gross WeightLH Left HandLIM LimitLK LeakLN Left NoseLNAV Lateral NavigationLOC LocalizerLOGO Logo GraphicLOM, MM Compass Locator at Outer
MarkerLOP Low Oil PressureLP Low PressureLPM Liter Per Minute
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ABBREVIATIONS (CONT'D)
LPT Lo Pressure TurbineLR Left RearLRC Long Range CruiseLRN Long Range NavigationLSB Lower Side Band
LTG(s) Light(s)LW Left WingLWD Left Wing DownLWR Lower
M
M Mach Numberm MeterMAA Maximum Authorized IFR
AltitudeMAC Mean Aerodynamic ChordMADC Micro Air Data ComputerMAG MagneticMAINT MaintenanceMALF MalfunctionMAN ManualMAP Ground Map (WXR)MAX MaximumMAZ MLS AzimuthMB MillibarsMCA Minimum Crossing AltitudeMCL Maximum ClimbMCR Maximum CruiseMCT Maximum Continuous ThrustMDA Minimum Descent AltitudeMEA Minimum Enroute IFR
AltitudeMECH MechanicMED MediumMEL Minimum Equipment ListMFD Multi-function DisplayMGP MLS GlideslopeMHz MegaHertz
MI MilesMIC MicrophoneMID AFT Middle AftwardMID FWD Middle ForwardMILS .001 of an inchMIN MinimumMISC MiscellaneousMKR MarkerMLG Main Landing GearMLS Microwave Landing SystemMLW Maximum Landing WeightMM Middle MarkerMMEL Master Minimum Equipment
ListMMO Maximum Operating Speed
in Mach NumberMOCA Minimum Obstruction
Clearance AltitudeMOD ModuleMON MonitorMPH Miles Per HourMRA Minimum Reception AltitudeMSG MessageMSL Mean Sea LevelMTG Miles to GoMTO/MTOW Maximum Take-off WeightMTW Maximum Taxi WeightMZFW Maximum Zero Fuel Weight
Misc
% Percent& and
° C Degrees Centigrade° F Degrees Fahrenheit
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ABBREVIATIONS (CONT'D)
N
N/A Not ApplicableN2 High Pressure Rotor RPMNAV NavigationND Nose Down, Navigation
DisplayNDB (ADF) Nondirectional Beacon
(Automatic Direction Finder)NEG NegativeNEUT Neutral
NL Nose LeftNLG Nose Landing GearNM Nautical Mile(s)No. NumberNOPT No Procedure Turn RequiredNORM NormalNOSE, N/W Nose WheelNR Nose RightNU Nose Up
O
OAT Outside Air TemperatureOB/OUTBD OutboardOBS ObserverOEI One Engine InoperativeOEW Operating Empty WeightOH, OVHD OverheadOK OkayOM Outer Marker
OVBD OverboardOVHT, OH OverheatOVLD OverloadOVSP OverspeedOVSPD OverspeedOVTEMP Over TemperatureOXY, O2 Oxygen
P
P#6 Panel 6P/S Pitot/StaticPA Passenger AddressPASS PassengerPBE Portable Breathing
Equipment (Smoke Hood)PCU Power Control UnitPFD Primary Flight DisplayPLA Power Lever AnglePLT(s) Pilot(s)PNLS(s) Panel(s)PO Outside Air PressurePOS PositionPPH Pounds Per HourPRESS Pressure, Pressurization
PRI/PRIM PrimaryPROC ProcedurePROT ProtectionPROX ProximityPRV Bleed Pressure Regulating
and Shut-off ValvePSI Pounds Per Square InchPSID Pounds Per Square Inch
DifferentialPSIG Pounds Per Square Inch
GaugePSU Passenger Service UnitPTCT ProtectPTT Push To TalkPWR Power
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ABBREVIATIONS (CONT'D)
Q
QAR Quick Access RecorderQEC Quick Engine ChangeQFE Local Station Pressure
QNH Altimeter SettingQTY Quantity
R
R RightRA Radio AltitudeRA Resolution Advisory (TCAS)RAT Ram Air TurbineRAT GEN Ram Air Turbine GeneratorRATLC Ram Air Turbine Line
ContactorRADALT Radio AltimeterRCCB Remote Controlled Circuit
BreakerRCDR RecorderRCVR ReceiverR/D Refuel/DefuelRDCP Refuel/Defuel Control PanelRDR RadarREC Receiver, RecorderRECIRC RecirculationRECOG RecognitionREF(s) Reference(s)
REFL RefuelREV ReverseRH Right HandRMI Radio Magnetic IndicatorRMU Radio Management UnitROT RotationRPM Revolutions Per MinuteRSB Radio System BusRT, R/T Receiver-TransmitterRTE RouteRTE DATA Route DataRTO Rejected Take-offRTU Radio Tuning UnitRUD RudderRVR Runway Visual RangeRVSR ReverserRW Right WingRWD Right Wing DownRWY Runway
S
S StatusSAT Static Air TemperatureSBY, STBY StandbySCAV ScavengeSCV Surge Control ValveSCR Selector (Nav source)SEC Second, SecondarySEL Select, SelectorSELCAL Selected CallSENS Sensitivity, SensorSERV, SVCE ServiceSFCU Slats and Flaps Control Unit
SID Standard InstrumentDeparture
SMKG SmokingSOV Shut-off ValveSP, SPD SpeedSPC Stall Protection ComputerSPS Stall Protection SystemSPKR SpeakerSPLR(s) Spoiler(s)SQ SquelchSSB Single Side BandSTA Station
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ABBREVIATIONS (CONT'D)
STAB StabilizerSTAT StatusSTEER SteeringSUPPL SupplySW(s) Switches
SYN SynchronizeSYNC SynchronousSYS, SYST SystemSTD Standard
T
TA Traffic Advisory (TCAS)TACAN UHF Tactical Air Navigation
AidTAS True AirspeedTAT Total Air TemperatureTCAS Traffic Alert and Collision
Avoidance SystemTCS Touch Control SteeringT/C Top of ClimbT/D Top of DescentTE Trailing EdgeTEMP TemperatureTGT Turbine Gas Temperature or
Target
TLC TRU Line ContactorTMS Thermal Management
SystemTO, T/O Take-offTOL ToleranceT/R Thrust ReverserTRB, TURB TurbulenceTRK TrackTRM TrimTRU Transformer Rectifier UnitTST TestTTC TRU Transfer Contactor
U
UNSCHD UnscheduledUSB Upper Side Band
USG United States GallonsUTIL Utility
V
V VoltVA Design Maneuvering SpeedVB Design Speed for Maximum
Gust IntensityVC Design Cruising SpeedVD Design Diving SpeedVDF/MDF Demonstrated flight diving
speedVEF Engine Failure SpeedVF Design Flap SpeedVFC/MFC Maximum Speed for Stability
Characteristics
VFE Maximum Flap ExtendedSpeed
VLE Maximum Landing GearExtended Speed
VLO Maximum Landing GearOperating Speed
VLOF Lift-off SpeedVMC Minimum Control Speed with
the Critical EngineInoperative
VMO/MMO Maximum Operating LimitSpeed
VMU Minimum Unstick SpeedVR Rotation Speed
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ABBREVIATIONS (CONT'D)
VS Stalling Speed or theMinimum Steady FlightSpeed at which the Airplaneis Controllable
VS0 Stalling Speed or theMinimum Steady FlightSpeed in the LandingConfiguration
VS1 Stalling Speed or theMinimum Steady FlightSpeed Obtained in a SpecificConfiguration
V1 Take-off Decision Speed(formerly Denoted as CriticalEngine Failure Speed)
V2 Take-off Safety SpeedV2 MIN Minimum Take-off Safety
SpeedV/S, VS Vertical SpeedVERT VerticalVF Variable Frequency
VFG Variable FrequencyGenerator
VFR Visual Flight RulesVG Vertical GyroVHF Very High Frequency
(30 − 300 MHz)VIB VibrationVIGB Variable Inlet Guide VanesVMC Visual Meteorological
ConditionsVNAV Vertical NavigationVOL VolumeVOLT VoltageVOR VHF Omnidirectional Range
StationVORTAC VOR and TACAN
Co−locatedV/L VOR/LocalizerVSI Vertical Speed Indicator
W
WAIV Wing Anti-Ice modulating andShut-off Valve
WAI Wing Anti-IceW WarningW/C Wind ComponentW/S Wind ShearW/W Wheel WellWARN WarningWF Runway Length Limited
WeightWf Fuel Flow In Pounds Per
HourWGT Weight
WHLS WheelsWIND WindowWOW Weight-On-WheelWPT(s) Waypoint(s)WRN WarningWS Second Segment Limited
WeightWTC Windshield Temperature
ControlWSHLD WindshieldWX WeatherWXR Weather Radar
X
X Cross TransferXFEED CrossfeedXFER, XFR TransferXFLOW Cross Flow
XMIT TransmitXPNDR TransponderXTK Cross TrackXWC Cross Wind Component
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ABBREVIATIONS (CONT'D)
Y
YD, Y/D Yaw Damper
Z
ZFW Zero Fuel Weight
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CONVERSION FACTORS
Multiply By To Obtain
Centimeters 0.3937 in
Centimeters² 0.155 in²
Centimeters³ 0.061 in³
Cu ft³ 0.0283 meters³
Ft 0.3048 meters
Ft² 0.0929 m²
Gal, Imperial 1.20094.546
USGliters
Gal, US 3.78540.8327
litersImperial gal
In 2.54 cm
In² 6.452 cm²
In³ 16.387 cm³
Kilograms 2.205 lb
Kilometers 0.62140.54
milesnautical miles
Km/hr 0.540.6214
knotsmph
Knots 1.1511.852
mphkm/hr
kPa 0.145 psi
Liters 0.26420.22
USGImperial gal
Meters 3.281 ft
Meters² 10.76 ft²
Meters³ 35.3115 ft³
Miles 52801.6090.869
ftkmnautical miles
Mph 1.6090.869
km/hrknots
Nautical Miles 1.1511.852
milesm
Pounds (lb) 0.4536 kilograms
PSI 6.895 kPa
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TEMPERATURE CONVERSION TABLE
°C °F °C °F °C °F °C °F °C °F °C °F °C °F °C °F °C °F °C °F °C °F °C °F−73.3−72.8−72.2−71.7−71.1
−100−99−98−97−96
−148.0−146.2−144.4−142.6−140.8
−45.6−45.0−44.4−43.9−43.3
−50−49−48−47−46
−58.0−56.2−54.4−52.6−50.8
−17.8−17.2−16.7−16.1−15.6
01234
32.033.835.637.439.2
10.010.611.111.712.2
5051525354
122.0123.8125.6127.4129.2
37.838.338.939.440.0
100101102103104
212.0213.8215.6217.4219.2
65.666.166.767.267.8
150151152153154
302.0303.8305.6307.4309.2
−70.6−70.0−69.4−68.9−68.3
−95−94−93−92−91
−139.0−137.2−135.4−133.6−131.8
−42.8−42.2−41.7−41.1−40.6
−45−44−43−42−41
−49.0−47.2−45.4−43.6−41.8
−15.0−14.4−13.9−13.3−12.8
56789
41.042.844.646.448.2
12.813.313.914.415.0
5556575859
131.0132.8134.6136.4138.2
40.641.141.742.242.8
105106107108109
221.0222.8224.6226.4228.2
68.368.969.470.070.6
155156157158159
311.0312.8314.6316.4318.2
−67.8−67.2−66.7−66.1−65.6
−90−89−88−87−86
−130.0−128.2−126.4−124.6−122.8
−40.0−39.4−38.9−38.3−37.8
−40−39−38−38−36
−40.0−38.2−36.4−34.6−32.8
−12.2−11.7−11.1−10.6−10.0
1011121314
50.051.853.655.457.2
15.616.116.717.217.8
6061626364
140.0141.8143.6145.4147.2
43.343.944.445.045.6
110111112113114
230.0231.8233.6235.4237.2
71.171.772.272.873.3
160161162163164
320.0321.8323.6325.4327.2
−65.0−64.4−63.9−63.3−62.8
−85−84−83−82−81
−121.0−119.2−117.4−115.6−113.8
−37.2−36.7−36.1−35.6−35.0
−35−34−33−32−31
−31.0−29.0−27.4−25.6−23.8
−9.4−8.9−8.3−7.8−7.2
1516171819
59.060.862.664.466.2
18.318.919.420.020.6
6566676869
149.0150.8152.6154.4156.2
46.146.747.247.848.3
115116117118119
239.0240.8242.6244.4246.2
73.974.475.075.676.1
165166167168169
329.0330.8332.6334.4336.2
−62.2−61.7−61.1−60.6−60.0
−80−79−78−77−76
−112.0−110.2−108.4−106.6−104.8
−34.4−33.9−33.3−32.8−32.2
−30−29−28−27−26
−22.0−20.2−18.4−16.6−14.8
−6.7−6.1−5.6−5.0−4.4
2021222324
68.069.871.673.475.2
21.121.722.222.823.3
7071727374
158.0159.8161.6163.4165.2
48.949.450.050.651.1
120121122123124
248.0249.8251.6253.4255.2
76.177.277.878.378.9
170171172173174
338.0339.8341.6343.4345.2
−59.4−58.9−58.3−57.8−57.2
−75−74−73−72−71
−103.0−101.2−99.4−97.6−95.8
−31.7−31.1−30.6−30.0−29.4
−25−24−23−22−21
−13.0−11.2−9.4−7.6−5.8
−3.9−3.3−2.8−2.2−1.7
2526272829
77.078.880.682.484.2
23.924.425.025.626.1
7576777879
167.0168.8170.6172.4174.2
51.752.252.853.353.9
125126127128129
257.0258.8260.6262.4264.2
79.480.080.681.181.7
175176177178179
347.0348.8350.6352.4354.2
−56.7−56.1−55.6−55.0−54.4
−70−69−68−67−66
−90.0−92.2−90.4−88.6−86.8
−28.9−28.3−27.8−27.2−26.7
−20−19−18−17−16
−4.0−2.2−0.41.43.2
−1.1−0.60.00.61.1
3031323334
86.087.889.691.493.2
26.727.227.828.328.9
8081828384
176.0177.8179.6181.4183.2
54.455.055.656.156.7
130131132133134
266.0267.8269.6271.4273.2
82.282.883.383.984.4
180181182183184
356.0357.8359.6361.4363.2
−53.9−53.3−52.8−52.2−51.7
−65−64−63−62−61
−85.0−83.2−81.4−79.6−77.8
−26.1−25.6−25.0−24.4−23.9
−15−14−13−12−11
5.06.88.6
10.412.2
1.72.22.83.33.9
3536373839
95.096.898.6
100.4102.2
29.430.030.631.131.7
8586878889
185.0186.8188.6190.4192.2
57.257.858.358.959.4
135136137138139
275.0276.8278.6280.4282.2
85.085.686.186.787.2
185186187188189
365.0366.8368.6370.4372.2
−51.1−50.6−50.0−49.4−48.9
−60−59−58−57−56
−76.0−74.2−72.4−70.6−68.8
−23.3−22.8−22.2−21.7−21.1
−10−9−8−7−6
14.015.817.619.421.2
4.45.05.66.16.7
4041424344
104.0105.8107.6109.4111.2
32.232.833.333.934.4
9091929394
194.0195.8197.6199.4201.2
60.060.661.161.762.2
140141142143144
284.0285.8287.6289.4291.2
87.888.388.989.490.0
190191192193194
374.0375.8377.6379.4381.2
−48.3−47.8−47.2−46.7−46.1
−55−54−53−52−51
−67.0−65.2−63.4−61.6−59.8
−20.6−20.0−19.4−18.9−18.3
−5−4−3−2−1
23.024.826.628.430.2
7.27.88.38.99.4
4546474849
113.0114.8116.6118.4120.2
35.035.636.136.737.2
9596979899
203.0204.8206.6208.4210.2
72.863.363.964.465.0
145146147148149
293.0294.8296.6298.4300.2
90.691.191.792.292.8
195196197198199
383.0384.8386.6388.4390.2 G
F01
10_0
47
AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−14
GENERAL AIRPLANE DESCRIPTION
The airplane is a swept-wing monoplane with a pressurized cabin. It is capable of accommodating apilot, a copilot, a third crew member and up to 19 passengers. The airplane has two BMW/RollsRoyce BR 710 turbo fan engines.
The airplane structure, in general, is fabricated from aluminum alloys. Alloy steels, stainless steels,titanium and composites are also used.
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aLEGEND
Kevlar
Graphite
Hybrid (Mainly Graphite)
Glass
Attention and strict processes are given to surface finishes, protection against corrosion and toexternal surface smoothness throughout airplane. Sealing requirements include environmentalsealing, protection of faying surfaces (similar and dissimilar) against corrosion, pressure sealing andintegral fuel tank sealing.
At sea level, the airplane and its installed equipment is certificated for operation in ambienttemperatures ranging between −30°C (−22°F) and +50°C (122°F). The airplane pressurizationsystem is certified for operations up to a maximum pressure altitude of 51,000 feet.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−15
AIRPLANE DIMENSION SCHEMATIC
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AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−16
DIMENSIONS AND GENERAL DATA
The data that follows is for general information only and is not to be used for inspection or rejectionpurposes. When specific data is required, the applicable illustration should be used.
Overall dimension
Length 99 ft. 5 in. (30.30 m)
Height 24 ft. 10 in. (7.57 m)
Wing
Span 93 ft. 6 in. (28.5 m)
Root chord (BL 47.61) 21 ft. 1 in. (6.43 m)
Tip chord (W/STA 544) 4 ft. 1 in. (1.24 m)
Dihedral of Wing Ref. Plane 2.5°
Spar locations
Front 14.0%
Rear 67.0%
Flaps 3 per sideSingle Slotted Fowler Flaps
Slats 4 L.E. segments per side
Ground spoilers 2 per side
Multi-function spoilers 4 per side
Horizontal tail surface
Span 31 ft. 9 in. (9.68 m)
Root chord 10 ft. 5 in. (3.18 m)
Tip chord 5 ft. (1.52 m)
Anhedral 5.0°
Vertical tail surface
Span 13 ft. 9 in. (4.19 m)
Root chord 16 ft. 7 in. (5.05 m)
Tip chord 10 ft. 7 in. (3.22 m)
Fuselage
Diameter 8 ft. 10 in. (2.69 m)
Length 86 ft. 5 in. (26.34 m)
Landing gear
Main gear Nose gear
Wheel size 19 in. 10 in.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−17
DIMENSIONS AND GENERAL DATA (CONT'D)Landing gear (Cont’d)
Tire size 38 in. 21 in.
Max loaded tire pressure 172 psi. 154 psi
Main gear track 13 ft. 4 in. (4.06m)
Nose gear track 13.14 in. (33.4cm)
Wheel base (max.) 42 ft. 10 in. (13.06m)
Areas
Equivalent wing area (including ailerons,flaps spoilers and area within the fuselage)
1022 sq. ft. (94.95 sq. m)
Horizontal tail area (Gross) 245 sq. ft. (22.76 sq. m)
Vertical tail area (Gross) 186 sq. ft. (17.28 sq. m)
Doors
Passenger door (LH. fwd)
Height to sill (one step below the floor line) 6 ft. 2 in. (188 m)
Width 3 ft. (0.91 m)
Height to sill (at floor line) 5 ft. 4 in. (163 m)
Baggage compartment door (LH, aft)
Height 2 ft. 9 in. (0.84 m)
Width 3 ft. 7 in. (1.09 m)
Height to sill (floor line) 6 ft. 7 in. (2.01 m)
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−18
ANTENNA LOCATION SCHEMATIC
TCAS(Directional)
MODEMODE
S 1
S 2
DME#1
DME#2
MARKERBEACON
TCASOMNI
VHF COMM #2
MODE S1 & 2
VHF COMM #1
GPS #1ADF #1
ADF #2
ELT (Optional)
VOR/LOC
RAD ALTRAD ALT
RAD ALT
RAD ALT
#1 TX#2 TX
#1 RX
#2 RX
HF
(LH AND RH)(If installed)incorporated).
GF
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_003
VHF COMM #3(On airplanes withSB 700−23−002
SATCOM
WARNING
Personnel should not stand nearby or in front of the radar antennawhen it is transmitting.
GLIDESLOPE
WEATHER RADAR
RADAR 5 mW/cm
PERSONNEL DANGER AREA
366 cm (12 ft.) Refer to Pilot’s Manual Pub. No. A28−1146−056−02 G
F01
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04
2
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−19
VISUAL EYE REFERENCES FOR GROUND OPERATION
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AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−20
STEERING RADII
Steering radii are shown below.
STEERING RADII SCHEMATIC
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a
43 ft 0 in(13.10 m)
56 ft 6 in(17.24 m)
128 ft 2 in(39.07 m)
14 ft 0 in(4.26 m)
68 ft 0 in(20.73 m)
53 ft 2 in(16.23 m)
45 ft 2 in(13.78 m)
20 ft 8 in(4.23 m)
7 ft 4 in(2.3 m)
MINIMUMPAVEMENTWIDTH180° TURN
NOTEMaximum steering
Symmetrical and idle thrustNo differential braking75° steering angle3° slipDry runwaySlow continuous turnMax A/C weightAFT CG.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−21
TURNING RADII
Minimum paving width for 180° turn − 68 ft. (20.76 m)
TURNING RADII SCHEMATIC
AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−22
JET EXHAUST SINGLE ENGINE GROUND IDLE THRUST
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AIRPLANE GENERAL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−23
JET EXHAUST SINGLE ENGINE TAKE-OFF THRUST
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AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−24
JET EXHAUST TWO ENGINE GROUND IDLE THRUST
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AIRPLANE GENERAL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−25
JET EXHAUST TWO ENGINE TAKE-OFF THRUST
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AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−26
AIRPLANE JACKING
Three jacking points are provided, one on the forward fuselage and one on each wing rear spar forjacking the complete airplane.
JACKING POINTS SCHEMATIC
TYPICAL JACK
JACK
REAR FUSELAGE SUPPORT
NYLON PLUG JACK PAD
JACKING POINT
SUPPORT BEAM
REAR FUSELAGE SUPPORT
LEGEND
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The nose jacking point is located on the fuselage centerline. Gear jacking points are also provided fortire/wheel/brake changes. Jacking procedures are located in the Aircraft Maintenance Manual(Chapter 07).
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−27
TOWING
A fitting for towing or pushing the airplane is located on the nose landing gear.
During towing, nose wheel swivel through the range of ±75° each side of center is possible, withoutdisconnecting the nose wheel steering torque links. The Aircraft Maintenance Manual (Chapter 09)has a detailed description of towing operations.
NOTE
Disconnecting the nose wheel steering torque links is recommended forall towing operations.
TOW BAR ATTACHMENT SCHEMATIC
TOW BAR ASSEMBLY
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Ground Locking Safety Pins
Ground safety locks are provided for the nose and each main gear, gear doors and for the Ram AirTurbine (RAT). Refer to the applicable chapter for the safety pin installations.
AIRPLANE GENERAL
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−10−28
TOW BAR ATTACHMENT SCHEMATIC (CONT'D)Towbarless Vehicle
FG
F01
10_0
13
WINCH STRAP
TOW VEHICLE
WINCH CUT−OFFSWITCH PLATE
STRUT−STRAP
NOSE LANDINGGEAR
TOWBARLESS
REAR GATE CRADLE
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−29
MOORING
Fittings are provided on the fuselage and on the wing jacking points for mooring the airplane.Mooring procedures are located in the Aircraft Maintenance Manual (Chapter 10).
MOORING ATTACHMENT POINTS SCHEMATIC
MAIN AND NOSE AREAS
TAIL AREA
MOORING ADAPTER PLATE
JACKING PAD
TIE DOWN RING
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_014
30.25° 30.25°
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−30
SEAT ASSEMBLY
The crew seats provide adjustments fore and aft, inboard/outboard lateral adjustment (“J” track),height and armrest position.
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a
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−31
SEAT ASSEMBLY (CONT'D)Seat Egression
Make sure the seat is in the fully upright position, then pull on the fore/aft lever and move the seatto its fully aft position.
NOTE
The lateral tracking is now automatically enabled.
CAUTION
Do not try to move the seat laterally with the fore/aft lever in the upposition. This could cause damage to the mechanism.
Release the fore/aft lever.
Move the seat to its fully outboard position to facilitate egress from the seat.
Moving the Seat Forward
CAUTION
If the seat is moved forward when it is not in its fully inboard position,it can jam.
After getting back onto the seat, before touching the fore/aft lever, move the seat laterally to itsfully inboard position.
NOTE
There is no mechanical lock to keep the seat in its position until youmove it forward.
Keeping the seat in its fully inboard position, raise the fore/aft lever to move the seat forward. Theseat must be moved forward at least one inch (2.54 cm) before the lateral tracking latch isautomatically locked. Release the lever when the desired forward position is reached.
NOTE
When the seat moves forward, the lateral tracking mechanism isdisabled, and the seat should not move laterally.
CAUTION
If the seat jams or moves laterally when it is not in its fully aftposition, do not attempt to reset it using force, as damage to themechanism may occur. Call a maintenance technician fortroubleshooting and repair.
AIRPLANE GENERAL
REV 52, Nov 10, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−32
EYE LOCATOR-SEAT ADJUSTMENT
An eye locator is mounted on the centre windshield post to enable seat adjustment for correcteye-to-wheel height.
FRONT VIEWTOP VIEW
The support bracket is not shown.
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_016
PILOT’S
SIGHT LI
NE COPILOT’S
SIGHT LINE
NOTE
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−33
CONTROL WHEEL
The pilot and copilot control wheels contain the following switches:
• Master disconnect.• Pitch Trim Switch.• Autopilot/Flight Director Touch Control.• Radio Key.
Master Disconnect
The Master Disconnect switch disengages the autopilot, deactivates the stick pusher and the pitchtrim. When released, the stick pusher and the pitch trim system are immediately reactivated butthe autopilot remains disengaged.
Pitch Trim Switch
The Pitch Trim Switch enables the pilot/copilot to control the trim from each control wheel.
Autopilot/Flight Director (Touch Control)
The Touch Control Switch (TCS) is located on the control wheel. It enables the pilot to maneuverthe airplane without disconnecting the autopilot control.
Radio Key
The Radio Key activates the selected radio transmitter.
GF
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32
1
1. Master Disconnect2. Pitch Trim Switch3. Autopilot/Flight Director Touch Control4. Radio Key
Indicates Chapter in which information on item may be found.
4
10
6
4
4
(radio keylocated behind)
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−34
FLIGHT COMPARTMENT GENERAL ARRANGEMENT
GF
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1. Flight Bag Storage2. Pilot’s Side Console3. Pilot’s Side Panel 4. Pilot’s Instrument Panel5. EICAS Display6. Glareshield7. Overhead Panel
8. Standby Instruments9. Systems Display10. Copilot’s Instrument Panel 11. Copilot’s Side Panel12. Copilot’s Side Console13. Control Wheel14. Pedestal
Indicates Chapter in which information on item may be found.
8 15 17
7 10 11
11 17
10
3
3 4
2 3 5 7 9
12 13 14 16 18
7
11
32 10 12 13 18
11 17
7 10 11
8 15 176
6 104
3 6 7
15 16 17 18
10 11
1
2
3
4
5
6
7
89
10
11
12
1313
14
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
NB
MEMORY−1
STANDBY
ALT:
118.00
131.27TEMP−1
131.10
112.00
1605ANT
620.0
REL
NORMAL 2000
15423LV
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
NB
MEMORY−1
STANDBY
ALT:
118.00
131.27TEMP−1
131.10
112.00
1605ANT
620.0
REL
NORMAL 2000
15423LV
TUNE TUNE
TRIMS
L
AIL RUD
NL NR
WD
RWD
STABCH1 CH2
PUSH OFF/RESET
OFFOFF
PUSH TO RESET
LAV CALL CABIN CALL CREW AREA PA
ON
CABINCALL
FWD AFT
LAVCALL
FWD AFT
IRS1 IRS2 IRS3
PARK/EMERBRAKE
PARK/EMERBRAKE
EICAS
SCROLL SYSTEM SELECT
IDLE
REV
MAX REV
MAXTHRUST
ENGINERUNL R
OFF OFF
FLIGHTSPOILER
MAX
FULL
1/2
ENGINE
LN1
EPR
RN1
EPR
GND LIFTDUMPING
AUTO BRAKE
NOSE STEER LDG GEAR
HORN PILOTEVENT
EGPWS
OFFOVRDMUTED
INTEGRALCOCKPIT LIGHTS
DIM BRTL
DIM BRTCTR
DIM BRTR
DIM BRTCB
DIM BRTOVHD
ON
AUTO
OFFMASTER
BRT
DIM
OFFAREA
ON
OFFEYE REF
DIM
BRTPBA
ON
OFFFLOOR
FLOODCOCKPIT LIGHTS
OFF BRTL CTR R
OFF BRT OFF BRT
DISPLAY
DIM BRTL CTR R
DIM BRT DIM BRT
NORMALTN
PFD1
NORMALTN1
EICAS
NORMALTN
PFD2
ALTN2ALTN3
PFD1 PFD2
NORMALTN
SG1
NORMALTN
SG3
NORMALTN
SG2
IRS IRSADC ADC
MASTERWARNING/CAUTION
WARNING
CAUTION
ROLL SPLRS
PLT CONT
ROLLSELPLT
ROLL
MASTERWARNING/CAUTION
WARNING
CAUTION
ROLL SPLRS
CPLT CONT
ROLLSEL
CPLTROLL
RAD BAROMINIMUMS NAV SCR BARO SET
PUSH STD
HPaIN RAD BAROMINIMUMS NAV SCR BARO SET
PUSH STD
HPaINSPD
PUSH CHG
MANFMSCRS 1
PUSH DCT
HDG
PUSH SYNC
DN
UP
ALT CRS 1
PUSH DCT
B C10 10
DISCH
PULL
1 2
DISCH
PULL
1 2
DISCH
PULL
1 2
ELT
FOR AVIATIONEMER USE ONLY
UNAUTHORIZED OPERATION PROHIBITED
ON
ARM/RESET
L HYD SOV
HYDRAULIC
CLOSED
L HYD SOV
CLOSED
HYDRAULIC
ELECTRICAL
ONOFF
AUTOON
OFF
ONOFF
AUTO
ONOFF
AUTO
1B 3A 3B 2B
ON
BATT MASTER
OFFEMS
ON ON
AVAIL AVAIL
EXT AC EXT DC
PUSH OFF/RESET
OFF OFF
FAIL FAIL
GEN 3 GEN 4
OFF
FAIL
GEN 2
OFF
FAIL
GEN 1
OFF
FAIL
APU GEN
PUSHOFF/RESET
OFF
FAIL
RAT GEN
ENGINE
APU
RUNOFF START
IGNITION L CRANK L CRANKAUTO
ENG START
AUTOWING XFER
OFF
AUTOAFT XFER
OFF ON
WING FEEDINHIBIT
AUX PUMP
OFF
PRI PUMP
OFF
L RECIRC
OFF
LWING FEED
INHIBIT
AUX PUMP
OFF
PRI PUMP
OFF
R RECIRC
OFF
R
XFEED SOV
FAIL
OPEN
PUSH TO MUTE
IAC 1 IAC 2
AURAL WARNING
MUTEDMUTED
TEMPERATURE
COCKPIT
COLD HOT
FWD CABIN
COLD HOT
AFT CABIN
COLD HOT
OFF OFF ON
RECIRC TRIM AIR RAM AIR
AUX PRESS
ON
HOT
COLD
L MANTEMP
R MANTEMP
HOT
COLD
LO HIGH
PACK CONTROLNORM
MAN
R PACK
OFF
FAIL
L PACK
OFF
FAIL
XBLEEDAUTO
CLSD OPEN
L ENG BLEEDAUTO
OFF ON
R ENG BLEEDAUTO
OFF ON
R ENG BLEEDAUTO
OFF ON
AUTOOFF ON
AUTOOFF ON
AUTOOFF ON
R COWLWINGL COWL
ANTI−ICE
AUTOFROM L FROM R
WING XBLEED
R
WINDSHIELD HEAT
MAN AUTOPRESSURIZATIONAUTO/MAN
MAN
MAN ALT
UP
DN
OUTFLOW VALVE
CLOSED
1
CLOSED
2DITCHING
ON
MAN
FMS
UP
DN
HIGH
NORM
LDG ELEV RATE
DEPRESS
ON
EMER
ONOFF/RESET
LONOFF/
RESET
EXTERNAL LIGHTS
LANDING
NAV BEACON STROBE WING INSP LOGO
WHT
OFFRED
OFFON
OFFON
OFFON
OFFON
L WING NLG R WING TAXI/RECOG/
OFFON
OFFON
OFFON
OFFON
PASS SIGNS EMER LIGHTSNO SMKG SEAT BELTS
OFFAUTO
ON
OFFAUTO
ON
OFFARM
ON
NO SMOKING
CIRCUIT BREAKER − SYSTEM 1/2
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
STALLPUSHER
ON
OFF
CHR
ET
CIRCUIT BREAKER − SYSTEM 1/2
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
STALLPUSHER
ON
OFF
CHR
ET
STSGSTK
SYSTEM SELECT
FROM TO WPT
ON
OXYGEN MASK
RESET
TEST
NPUSH100%
COCKPIT VOICE RECORDER MICROPHONE MONITOR
TESTERASE
STATUS HEADPHONE
PASSENGER OXYGEN
CLOSED OVERRIDE
NORMAL
FIRST AID
TEST PORT
PASS ONOFF
FAULT
LOWPPR
OP
EN
PU
SH
PU
SH
TO
CL
OS
EO
PE
NP
US
H
OXYGEN MASK
RESET
TEST
NPUSH100%
SYSTEMSEICASMFDPFD MFD PFD
STBY
STBY
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−35
FLIGHT COMPARTMENT (AFT VIEW)
GF
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Indicates Chapter in which information on item may be found.
1 2
5
3
4
7
6
(If installed)
280 BULKHEADFWD FACERH SIDE
280 BULKHEADFWD FACELH SIDE
1. Refuel/Defuel Panel2. Oil Replenishment Panel3. Circuit Breaker Panel4. Halon Fire Extinguisher
5. Data Upload/Download Panel6. Portable Breathing Equipment7. Crash Axe
12
18
7
8
8
8
6
OIL REPLENISHMENTPOWER
RESERVOIR LH ENG APU RH ENG
SYSTEMON
TANKLO
PUMPON
LOOILVLV
OPEN
LOOILVLV
OPEN
LOOILVLV
OPEN
PRINT MAINTREPORT
DATAUPLOAD/DOWNLOAD
DAU 1ADAU 1B
DAU 2ADAU 2B
DAU 3A
DAU 3B
DAU 4A
DAU 4BIRS 1
IRS 2IRS 3
WX
SPARE
IAC 1IAC 2
IAC 3GPWS
SATCOM SDU
CABIN COMM
GPS 1GPS 2
ADC 1ADC 2
ADC 3
REFUEL/DEFUEL PANEL MASTERON
INCR
DECR
PRESELRIGHTAFT
TOTALLEFTCTR
30000100008000
LB 30000100002000
LB
MANUAL
LEFT CTR RIGHT AFT
OPEN
CLOSE
REFUEL
DEFUEL
AUTO REFUEL
START
REFUELAUTO
STOP
AFTON
OFF
SHUTOFFTEST
REFUEL/DEFUEL PANEL
LEFT CENTER RIGHT
AFT PRESELTOTAL
MANUAL
LEFT CTR RIGHT AFT
OPEN
CLOSE
INCR
DECR
PRESEL
START
STOP/SOVTEST
REFUEL
DEFUEL
AUTOOFF
MANUAL
REFUEL
REFUELNO AFT
OFF
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−36
PILOT'S SIDE CONSOLE
GF
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1. Oxygen Mask/Regulator2. Headset Panel3. Navigation Display Unit4. Nosewheel Steering Handwheel
4
3
1
2
HEADSET PANEL
FLASHLIGHT
FLASHLIGHT
Indicates Chapter in which information on item may be found.
8
6
17
15
STSGSTK
SYSTEM SELECT
FROM TO WPT
ON
OXYGEN MASK
RESET
TEST
NPUSH100%
MICHEADSET
HDPH
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−37
PILOT'S SIDE PANEL
GF
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_021
Indicates Chapter in which information on item may be found.
1. Electrical Management System2. Stall Pusher Switch3. Clock4. Air Conditioning Gasper
7
10
2
11
1
23
4
CIRCUIT BREAKER − SYSTEM 1/2
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
STALLPUSHER
ON
OFF
CHR
ET
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−38
PILOT'S INSTRUMENT PANEL
GF
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TOC3
KSRP
KPHX
WX SAT
GSPD
−56TATTAS
−40234345
LX
HDG330
ETE 1+36
KLAX
KPHXTOC
KSRPKDVT
4000 4000
FL180
12.5 NMKDVT
LUF
KDVT
5
N
5
360
TERROFF
30
6
33
Indicates Chapter in which information on item may be found.
1. Airspeed Placard2. Primary Flight Display3. Multi−Functional Display
MAP ModePLAN FormatWX RadarTCAS Traffic
CREW LIFE VESTUNDER SEAT
AIRSPEED LIMITS − (INDICATED SPEEDS)
VFE (SLATS OUT, 0° FLAPS).............. 225VFE (SLATS OUT, 6° FLAPS).............. 210VFE (SLATS OUT, 16° FLAPS)............ 210VFE (SLATS OUT, 30° FLAPS)............ 185VA (MANEUVERING)(AT SEA LEVEL AT 95,000 LB)............ 250(AT 20,000 FT AT 78,600 LB)............... 225
VMO (BELOW 8,000 FT)...................... 300VMO (8,000 TO 30,267 FT).................. 340MMO (30,267 FT TO 35,000 FT).......... 0.89MMO (AT 47,000 FT).......................... 0.871MMO (AT 51,000 FT).......................... 0.855VLO (EXT) (L/G EXTENSION)...............200VLO (RET) (L/G RETRACTION)............200VLE (L/G EXTENDED)...........................250
AIRSPEED LIMITS − (INDICATED SPEEDS)
VFE (SLATS OUT, 0° FLAPS).............. 225VFE (SLATS OUT, 6° FLAPS).............. 210VFE (SLATS OUT, 16° FLAPS)............ 210VFE (SLATS OUT, 30° FLAPS)............ 185VA (MANEUVERING)(AT SEA LEVEL AT 95,000 LB)............ 250(AT 20,000 FT AT 78,600 LB)............... 225
VMO (BELOW 8,000 FT)...................... 300VMO (8,000 TO 30,267 FT).................. 340MMO (30,267 FT TO 35,000 FT).......... 0.89MMO (AT 47,000 FT).......................... 0.871MMO (AT 51,000 FT).......................... 0.855VLO (EXT) (L/G EXTENSION)...............200VLO (RET) (L/G RETRACTION)............200VLE (L/G EXTENDED)...........................250
11 17
11 17
2 3
1
2020
1010
1010
2020
VALTLNAV AP1VNAVVAPP
29.92 IN600 RAD
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−39
CENTRE INSTRUMENT PANELS
GF
0110
_023
102030
302010
01
2
3
4
7
9
65 29 9 210 13
ALT
1 0 1 30
001 FEET
mb/hPa in Hg
180 200
IAS KNOTS
BARO
Standby AttitudeIndicator
Engine Indication and Crew AlertingSystem (EICAS) Primary Display
EICAS Sytem DisplayStandby Altimeter/Airspeed Indicator
Indicates Chapter in which information on item may be found.
Engine InstrumentsCaution and Warning AnnunciatorFuel QuantityFlap/Slat and Spoiler StatusLanding Gear StatusFlight Control Trims
Bleed SystemAnti−Ice SystemElectrical System (AC and DC)Fuel SystemFlight ControlsHydraulics
Airplane Status Information andthe following synoptic pages:
11
11
18
3
12
10
15
10
2
2
7
12
10
13
OIL QTY (QTS)ENGAPURES
RPM EGT
BRAKE TEMP
10.4
90
13% 13%
400100
0303 03 03
4.55.0
10.4
OXYGEN
OPEN OPEN
OUTFLOW VALVES00
1 2
1 2
2
APU
%
1
CKPT (°C) AFTCABIN (°C)CABIN (°C)
FWD
20
1300
0.0020
CAB ALT
CAB RATE
P2319 21 22
TOTALFUEL(LBS) 41550
1.541.54
73.373.3
789789
14600 1460010000 2350 ND
STAB
NU
RUDDERNL
LWD RWD
NR
TRIMS
7.2
N2FF (PPH)OIL TEMPOIL PRESS
93.45750 115 81
93.45750 115 81
EPR
N1
ITT
AIL
1.651.65
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−40
OVERHEAD PANEL
GF
0110
_024
1
2
3
4
56
7
8
9
10
12
11
13
161415
1. Electrical Panel2. Hydraulic Panels3. ELT Panel4. Gasper5. Aural Warning Panel6. Fire Discharge Handles7. Bleed/Air Conditioning/Anti−Ice Panel8. Pressurization Panel
9. Windshield Heat Panel10. External Lights Panel11. Passenger Signs/Emergency Lights Panel12. Engine Panel13. Standby Compass14. APU Panel15. Fuel Panel16. CVR Area Microphone
7
13
6
2
3
9
2
2 14 18
14
16
16
18
17
5
12
6
Indicates Chapter in which information on item may be found.
B C10 10
DISCH
PULL
1 2
DISCH
PULL
1 2
DISCH
PULL
1 2
ELT
FOR AVIATIONEMER USE ONLY
UNAUTHORIZED OPERATION PROHIBITED
ON
ARM/RESET
L HYD SOV
HYDRAULIC
CLOSED
L HYD SOV
CLOSED
HYDRAULIC
ELECTRICAL
ONOFF
AUTOON
OFF
ONOFF
AUTO
ONOFF
AUTO
1B 3A 3B 2B
ON
BATT MASTER
OFFEMS
ON ON
AVAIL AVAIL
EXT AC EXT DC
PUSH OFF/RESET
OFF OFF
FAIL FAIL
GEN 3 GEN 4
OFF
FAIL
GEN 2
OFF
FAIL
GEN 1
OFF
FAIL
APU GEN
PUSHOFF/RESET
OFF
FAIL
RAT GEN
ENGINE
APU
RUNOFF START
IGNITION L CRANK L CRANKAUTO
ENG START
AUTOWING XFER
OFF
AUTOAFT XFER
OFF ON
WING FEEDINHIBIT
AUX PUMP
OFF
PRI PUMP
OFF
L RECIRC
OFF
LWING FEED
INHIBIT
AUX PUMP
OFF
PRI PUMP
OFF
R RECIRC
OFF
R
XFEED SOV
FAIL
OPEN
PUSH TO MUTE
IAC 1 IAC 2
AURAL WARNING
MUTEDMUTED
TEMPERATURE
COCKPIT
COLD HOT
FWD CABIN
COLD HOT
AFT CABIN
COLD HOT
OFF OFF ON
RECIRC TRIM AIR RAM AIR
AUX PRESS
ON
HOT
COLD
L MANTEMP
R MANTEMP
HOT
COLD
LO HIGH
PACK CONTROLNORM
MAN
R PACK
OFF
FAIL
L PACK
OFF
FAIL
XBLEEDAUTO
CLSD OPEN
L ENG BLEEDAUTO
OFF ON
R ENG BLEEDAUTO
OFF ON
APU BLEEDAUTO
OFF ON
AUTOOFF ON
AUTOOFF ON
AUTOOFF ON
R COWLWINGL COWL
ANTI−ICE
AUTOFROM L FROM R
WING XBLEED
R
WINDSHIELD HEAT
MAN AUTOPRESSURIZATIONAUTO/MAN
MAN
MAN ALT
UP
OUTFLOW VALVE
CLOSED
1
CLOSED
2DITCHING
ON
MAN
FMS
UP HIGH
NORM
LDG ELEV RATE
DEPRESS
ON
EMER
ONOFF/RESET
LONOFF/
RESET
EXTERNAL LIGHTS
LANDING
NAV BEACON STROBE WING INSP LOGO
WHTOFF
REDOFFON
OFFON
OFFON
OFFON
L WING NLG R WING TAXI/RECOG/
OFFON
OFFON
OFFON
OFFON
PASS SIGNS EMER LIGHTSNO SMKG SEAT BELTS
OFFAUTO
ON
OFFAUTO
ON
OFFARM
ON
NO SMOKING
DN DN
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−41
GLARESHIELD
Left Glareshield
Centre Glareshield
Right Glareshield
2
3
GF
0110
_025
1
4
Indicates Chapter in which information on item may be found.
1. Roll Select Switch2. Primary Flight Display Controller3. Guidance Panel4. Master Warning/Caution Switch
10
11
4
3
MASTERWARNING/CAUTION
WARNING
CAUTION
ROLL SPLRS
PLT CONT
ROLLSELPLT
ROLL
MASTERWARNING/CAUTION
WARNING
CAUTION
ROLL SPLRS
CPLT CONT
ROLLSEL
CPLTROLL
RAD BAROMINIMUMS NAV SCR BARO SET
PUSH STD
HPaIN
RAD BAROMINIMUMS NAV SCR BARO SET
PUSH STD
HPaIN
SPD
PUSH CHG
MANFMSCRS 1
PUSH DCT
HDG
PUSH SYNC
DN
UP
ALT CRS 1
PUSH DCT
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−42
CENTRE PEDESTAL
GF
0110
_026
a
1
2
4
5
6
7
8
9
10
3
11
12
14
16
18
19
20
21
22
13
17
15
1. Landing Gear Panel
2. Gnd Lift Dump/Autobrake Panel
3. Engine Control Panel
4. Flight Spoiler Lever
5. Weather Radar Control Panel
6. EICAS Control Panel
7. Parking Brake Handle
8. Flt Control Trim Panel
9. DC Power Emergency Ovrd
10. IRS Mode Selector Panel
11. EGPWS Panel
12. FMS Control Display Panel.
13. Radio Management Unit
14. Thrust Lever Quadrant
15. MFD Control Panel
17. Flap Selector Panel
18. Cockpit Lights − Integral/Misc
19. Cockpit Lights − Flood/Display
20. Reversion Control Panel
21. Landing Gear Manual Release Handle
22. RAT Manual Release Handle
16. Audio Panel
Indicates Chapter in which information on item may be found.
15
15 10
18
10
17
3
15
10
7
17
17
17
6
18
13
6
17
10
16
16
3
15
3
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
NB
MEMORY−1
STANDBY
ALT:
118.00
131.27TEMP−1
131.10
112.00
1605ANT
620.0
REL
NORMAL 2000
15423LV
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
NB
MEMORY−1
STANDBY
ALT:
118.00
131.27TEMP−1
131.10
112.00
1605ANT
620.0
REL
NORMAL 2000
15423LV
TUNE TUNE
TRIMS
L
AIL RUD
NL NR
WD
RWD
STABCH1 CH2
PUSH OFF/RESET
OFFOFF
IRS1 IRS2 IRS3
PARK/EMERBRAKE
PARK/EMERBRAKE
EICAS
SCROLL SYSTEM SELECT
IDLE
REV
MAX REV
MAXTHRUST
ENGINERUNL R
OFF OFF
FLIGHTSPOILER
MAX
FULL
1/2
ENGINE
LN1
EPR
RN1
EPR
GND LIFTDUMPING
AUTO BRAKE
NOSE STEER LDG GEAR
HORN PILOTEVENT
EGPWS
OFFOVRDMUTED
INTEGRALCOCKPIT LIGHTS
DIM BRTL
DIM BRTCTR
DIM BRTR
DIM BRTCB
DIM BRTOVHD
ON
AUTO
OFFMASTER
BRT
DIM
OFFAREA
ON
OFFEYE REF
DIM
BRTPBA
ON
OFFFLOOR
FLOODCOCKPIT LIGHTS
OFF BRTL CTR R
OFF BRT OFF BRT
DISPLAY
DIM BRTL CTR R
DIM BRT DIM BRT
NORMALTN
PFD1
NORMALTN1
EICAS
NORMALTN
PFD2
ALTN2ALTN3
PFD1 PFD2
NORMALTN
SG1
NORMALTN
SG3
NORMALTN
SG2
IRS IRSADC ADC
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−43
COPILOT'S INSTRUMENT PANEL
GF
0110
_027
Indicates Chapter in which information on item may be found.
1. Airspeed Placard2. Primary Flight Display3. Multi−Functional Display
MAP ModePLAN FormatWX RadarTCAS Traffic
11 17
11 17
TOC3
KSRP
KPHX
WX SAT
GSPD
−56TATTAS
−40234345
LX
HDG330
ETE 1+36
KLAX
KPHXTOC
KSRPKDVT
4000 4000
FL180
12.5 NMKDVT
LUF
KDVT
5
N
5
360
TERROFF
30
6
33
CREW LIFE VESTUNDER SEAT
3 2
1
AIRSPEED LIMITS − (INDICATED SPEEDS)
VFE (SLATS OUT, 0° FLAPS).............. 225VFE (SLATS OUT, 6° FLAPS).............. 210VFE (SLATS OUT, 16° FLAPS)............ 210VFE (SLATS OUT, 30° FLAPS)............ 185VA (MANEUVERING)(AT SEA LEVEL AT 95,000 LB)............ 250(AT 20,000 FT AT 78,600 LB)............... 225
VMO (BELOW 8,000 FT)...................... 300VMO (8,000 TO 30,267 FT).................. 340MMO (30,267 FT TO 35,000 FT).......... 0.89MMO (AT 47,000 FT).......................... 0.871MMO (AT 51,000 FT).......................... 0.855VLO (EXT) (L/G EXTENSION)...............200VLO (RET) (L/G RETRACTION)............200VLE (L/G EXTENDED)...........................250
AIRSPEED LIMITS − (INDICATED SPEEDS)
VFE (SLATS OUT, 0° FLAPS).............. 225VFE (SLATS OUT, 6° FLAPS).............. 210VFE (SLATS OUT, 16° FLAPS)............ 210VFE (SLATS OUT, 30° FLAPS)............ 185VA (MANEUVERING)(AT SEA LEVEL AT 95,000 LB)............ 250(AT 20,000 FT AT 78,600 LB)............... 225
VMO (BELOW 8,000 FT)...................... 300VMO (8,000 TO 30,267 FT).................. 340MMO (30,267 FT TO 35,000 FT).......... 0.89MMO (AT 47,000 FT).......................... 0.871MMO (AT 51,000 FT).......................... 0.855VLO (EXT) (L/G EXTENSION)...............200VLO (RET) (L/G RETRACTION)............200VLE (L/G EXTENDED)...........................250
2020
1010
1010
2020
VALTLNAV AP1VNAVVAPP
29.92 IN600 RAD
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−44
COPILOT'S SIDE PANEL
GF
0110
_028
Indicates Chapter in which information on item may be found.
1. Electrical Management System2. Stall Pusher Switch3. Clock4. Air Conditioning Gasper
7
10
2
11
1
234
CIRCUIT BREAKER − SYSTEM 1/2
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
STALLPUSHER
ON
OFF
CHR
ET
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−45
COPILOT'S SIDE CONSOLE
GF
0110
_029
a
1. Mach Transducer Source Selector Valve2. Headset Panel3. Oxygen Mask/Regulator4. Passenger Oxygen Selector
FLASHLIGHT
Indicates Chapter in which information on item may be found.
10
6
8
8
6
4
5
2
1
5. Cockpit Voice Recorder6. Cockpit Printer (If installed)
6
6
3
COCKPIT VOICE RECORDER MICROPHONE MONITOR
TESTERASE
STATUS HEADPHONE
PASSENGER OXYGEN
CLOSED OVERRIDE
NORMAL
FIRST AID
TEST PORT
PASS ONOFF
FAULT
LOWPPR
OP
EN
PU
SH
PU
SH
TO
CL
OS
EO
PE
NP
US
H
SELECT VALVECLOSED
SELECT VALVECLOSED
PITOT STATIC
OXYGEN MASK
RESET
TEST
NPUSH100%
MICHEADSET
HDPH
(on airplanes9002 thru 9158)
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−46
AIRPLANE DOORS
The airplane is equipped with the one passenger door (which serves as an emergency exit), oneoverwing emergency exit, one baggage compartment door, one rear fuselage equipment bay doorand several service doors and panels.
The door warning system provides the flight crew with a visual indication (EICAS), when any of thefollowing exterior doors/exits are opened or incorrectly latched:
• Passenger door.• Cargo door.• Aft equipment bay door.• Left or right emergency exit.
Description and operation of the emergency features of the wing emergency exits are in this manualChapter 8, EMERGENCY EQUIPMENT.
The door warning system also provides the flight crew with a visual indication (EICAS), when any ofthe landing gear doors are not in their commanded position. Description and operation of the landinggear doors are in this manual Chapter 15, LANDING GEAR.
PASSENGER DOOR
The passenger door is the main entrance /exit for passengers as well as the flight crew and islocated on the left side of the airplane, aft of the flight compartment. The door is a mechanicallybalanced airstair with an attached door. The door assembly which opens outwards and downwards,turns on two brackets attached to each side of the airstairs and hinge points in the fuselage.Handrails are attached to each side of the airstairs and the fuselage. They extend and retract as thedoor opens and closes.
The door operation is power assisted with a cable system and a DC electric motor. The door lockingmechanism is capable of operations from inside and outside the airplane. A single operation fromeither handle will unlock the door and lift it clear of its latching mechanism.
The door opens under a controlled descent through a tension spring arrangement and mechanicaldamping using a pulley and cable mechanism.
The door is normally closed from inside or outside of the airplane through an electrical actuator. Thedoor can also be manually closed without electrical power.
A hinged flap (vent flap) opens in the exterior surface of the door to protect against pressurization ofthe fuselage, to an unsafe level, until the door is closed and locked.
The door locks have proximity switches to display an EICAS indication of closed and locked.
Lights are provided in each step riser to illuminate the steps. Door lighting automatically shuts-offwhen the passenger door closes.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−47
PASSENGER DOOR SCHEMATIC
CABLE ASSEMBLY
HANDRAIL ASSEMBLY
CLOSED POSITION
GF
0110
_030
a
OP
NE
OPEN
PASSENGER DOOR COMPONENTS
The following components are described to provide an understanding of the passenger dooroperating system.
Airstair and Handrails Assembly
The airstairs act as the steps for embarking/disembarking the airplane. They also act as supportfor the door structure, which hangs below the airstairs when open. The airstairs are hinged to theairplane via two hinges and two pins.
The handrails are attached to the fuselage and the airstairs. They support the weight of the doorand airstair assembly and passenger loading. Handrails are capable of supporting the weight ofthe door and passenger loading.
The design of the door is such that there is no contact with the ground when the door is in theopen position.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−48
PASSENGER DOOR COMPONENTS (CONT'D)Lift arms
Two levers are connected from either end of the lockshaft to the fixed linked arms on the airstairstructure. They are driven by the handles, assisted by the tension spring. Their purpose is to liftthe door out of its frame and hold it up and out in relation to the airstair, while the door is opening.
“G” Locks
In the locked position, the “G” lock hooks hold the door relative to the airstairs and prevent anyupward movement in the door frame during turbulence or negative “G” flight.
Vent Flap
A pressurization vent flap is centrally located at the top of the door under the lockshaft. The flapprevents pressure building up until the “G” locks engage. Once the locks are in and the flap isshut, the pressure holds the flap firmly shut. The vent flap is opened by the lockshaft mechanismas the “G” locks are disengaged, to release any residual pressure from the pressurization system.
LIFT ARM
VENT FLAP
FORWARD "G" LOCK
AFT "G"
LOCKING HANDLE G
F01
10_0
31a
LOCK
OPEN
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−49
PASSENGER DOOR COMPONENTS (CONT'D)Locked Indication
Visual indication of latching and locking is given to the cabin crew by the red band indicators onthe internal handle cover and the handle. The red band across the handle and cover clearly showsthe handle in the locked position. A safe indication is indicated by the alignment of the two redlines.
Effectivity:
• Airplanes 9002 to 9095 not incorporating Service Bulletin:
• SB 700−52−22, Passenger Door − Internal Handle Indication Improvement.
LIFT ARM
VENT FLAP
FORWARD "G" LOCK
AFT "G"
MECHANICAL INDICATOR
GREEN LOCKED
OP
EN
LOCKING HANDLE G
F01
10_0
31
LOCK
Visual indication of latching and locking is given by an indicator arm that is driven directly by thelast motion of the internal handle. The indicator, in the form of a green line, lines up with a greenline on the airstairs only after the door latches and detents are engaged. The indication is viewedthrough a window cutout in the internal handle cover. A safe indication is indicated by thealignment of the two green lines. A window in the handle exposes a red fixed plate when thehandle is out of the safe locked position.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−50
PASSENGER DOOR OPERATING HANDLES
The external handle is set into a box in the lower door structure. It is connected by push/pull rodsinside the door to the lockshaft, at the forward end.
position until the handle moves to the full down position.
LOCKSHAFT
GF
0110
_032
The door is not in the fully closed
EXTERNAL HANDLE
NOTE
As the lockshaft reaches its fully locked position, the handles are held in position with spring tension.When the handles are moved out of the locked position, the spring assists in lifting the door andreduces the load on the handles.
The internal handle is a lever on the forward side of the door directly attached to a lockshaft and tothe forward door lift arm.
(stowed) position. The door is not in the fully closed position until the handle moves fully down.
GF
0110
_033
NOTE Handle shown in the locked
INTERNAL HANDLE
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−51
PASSENGER DOOR SWITCHES
The internal door operating switch is controlled on and off by the “DOOR” switch installed internally inthe door frame, next to the main passenger door.
INTERNAL SWITCH (view looking from inside the airplane)
EXTERNAL SWITCH
NOTE Both switches are guarded but not shown.
GF
0110
_034
The external door operating switch is controlled on and off by the “DOOR” switch installed next to themain passenger door.
EXTERNAL DOOR SWITCH ACCESS PANEL
DOOR OPERATINGSWITCH
DOOR OPERATION
PUSH IN FLAP TOGRASP HANDLE
LIFT HANDLE FULL UPPULL DOOR OUT
1. OPERATE SWITCH TOROTATE DOOR FULLYINTO DOOR APERTURE
2. PULL HANDLEDOWNWARDS TO STOW
TO OPEN TO CLOSE
NOTE: DO NOT RE−CYCLE HANDLE DURING CLOSING OPERATION WITHOUT RE− OPENING DOOR SUFFICIENTLY TO RE−ARM DOOR UPLOCK LEVER
OperatingInstructions
GF
0110
_035
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−52
PASSENGER DOOR OPERATION
The following examples are intended to familiarize the operator with events which occur whenmoving the passenger door from either the open or closed positions. The door operations aredescribed in detail and should be followed as per Aircraft Maintenance Manual Chapter 52.
External Door Operation
To open the passenger door externally:
• PUSH IN FLAP TO GRASP HANDLE• LIFT HANDLE FULL UP• PULL DOOR OUT
To close the passenger door externally:
NOTE
Do not re-cycle the handle during closing operation withoutre-opening door sufficiently to re-arm door uplock lever.
• DISENGAGE HANDRAIL LOCK• PRESS AND HOLD DOOR CLOSE SWITCH• PULL HANDLE DOWNWARDS TO STOW
Internal Door Operation
To open the passenger door internally:
• OPERATE DOOR HANDLE FROM THE LOCKED POSITION• DOOR MOVES INWARD AND UPWARD• PUSH DOOR OUT TO OPEN
To close the passenger door internally:
• PUSH FOOT PEDAL (to disengage handrail lock)• PRESS AND HOLD DOOR CLOSE SWITCH• MOVE DOOR HANDLE FULLY DOWN• CHECK GREEN VISUAL INDICATION IN THE HANDLE
Manual Closing
A rope wound around a pulley on the aft end of the torque shaft must be unwound sufficiently to bebrought into the cabin. The handrail latch must be released and then the rope can be pulled,rotating the torque shaft and raising the door via the normal cables. Once the door is raised it maybe lowered into the frame and locked by the normal method with the lock handle.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−53
EMERGENCY EXIT
An overwing emergency plug type emergency exit is installed on the right side of the airplane. Theexit is an inward opening plug type and can be unlatched from the interior or exterior of the airplane.Emergency door operation from inside the cabin is achieved by single action of the emergency exitoperating handle.
EMERGENCY EXIT DOOR GF
0110
_036
Two lower hook fittings and two upper latch fittings position the door in the door opening. Three stopfittings on each side of the door and surround structure react to the pressurization forces of the plugdoor type.
HOOK FITTING
LATCH FITTING
HAND HOLD
LATCH MECHANISM
DOOR STOP BOTH SIDES
GF
0110
_037
When the door is removed, handling is facilitated by an interior hand grip, flush-mounted within thedoor box structure.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−54
EMERGENCY EXIT (CONT'D)
To unlatch the emergency exit door from the interior, the upper door handle is pulled inward. Thismotion opens the exterior push plate/vent flap to bleed any residual pressure and disengages the twolatch pins. The door moves inward and pivots on the lower hook fittings. A grip of the upper handle ismaintained while grasping the lower hand grip and the door is lifted inwards away from the dooropening.
QUICK RELEASE LATCH MECHANISM
HAND GRIP
GF
0110
_038
To unlatch the emergency exit door from the exterior, the upper push plate/vent flap is depressed todisengage the latch pins and the door is pushed inwards away from the opening.
PUSH IN FLAPPUSH DOOR INWARD
GF
0110
_039
Visual indication of a locked condition of the overwing emergency is the exit door secured in position,with the interior handle recessed in the surround structure.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−55
AFT EQUIPMENT BAY DOOR
The unpressurized aft equipment bay is accessed by a maintenance door in the fuselage fairing. Thedoor is horizontally hinged at it’s forward edge with initial and subsequent opening movements beingdownward and outward. When the door is opened, it is restrained from over travel and striking thebelly fairing using two, door-to-fairing mounted lanyards.
The door locking mechanism is capable of operation only from outside of the airplane.
AFT EQUIPMENT BAY DOOR SCHEMATIC
LANYARD
LATCH MECHANISM
GF
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_040
During the closing cycle, two rollers, one on either side of the door, act as guides to locate and centrethe door within its belly fairing aperture.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−56
AFT EQUIPMENT BAY DOOR SCHEMATIC (CONT'D)Aft Equipment Bay Door Operation
DOOR OPENING − Door opening is accomplished by depressing the trigger and pulling thehandle to the full open position.
DOOR LATCH HANDLE ASSEMBLY
GF
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_041
DOOR CLOSING − The door latch handle is flush fitting and is secured by an integral push trigger,which when depressed, releases the handle to the free open position. The door is secured byreturning the handle flush with the door.
Visual indication of secure latching and locking is given by the door, the push trigger and theexternal handle all being flush with the fuselage’s surface.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−57
BAGGAGE COMPARTMENT DOOR
A baggage compartment plug type access door is installed in the fuselage aft section on the left sideforward of the rear pressure bulkhead.
Aft Passenger Compartment Bulkhead
Cargo Compartment
CARGO DOOR OPENING
BAGGAGE COMPARTMENT INTERIOR
DOOR HANDLE
GF
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_042
The door is an inward opening plug type and can be unlatched from outside or inside the airplane.The door is accessible, but not visible, from the passenger compartment and is not an emergencyexit. The door moves inward and upward to a stowed position above and clear of the door aperture.
DOOR HANDLE RECESS
PUSH TRIGGER
OUTER HANDLE
CARGO DOOR OPEN
STOWED POSITION
GF
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The latch mechanism consists of inner and outer handles directly coupled together and mounted onthe forward and aft sides of the door. The handle assembly contains a trigger lock which holds thehandle in the stowed position. The door is latched when the exterior handle is rotated to engage latchpins and locked when the handle is stowed and latched in its housing recess.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−58
BAGGAGE COMPARTMENT DOOR (CONT'D)
A vent door is located in the upper portion of the door and will not close until the door is fully closedand the handle stowed in the locked position.
VENT DOOR/SEAL
INTERIOR DOOR HANDLE
DETENT BUTTON GF
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_044
Baggage Door Operation
CLOSING THE BAGGAGE DOOR EXTERNALLY − Rotate the outer handle 90 degrees to latchthe door. Push the handle into the recessed housing until the trigger button is latched into thetrigger mechanism.
CLOSING THE BAGGAGE DOOR INTERNALLY − Rotate the inner handle 90 degrees counterclockwise to latch the door. Pull the handle until the outer handle trigger latches into the triggermechanism and the handle is stowed into the recessed housing.
OPENING THE BAGGAGE DOOR EXTERNALLY − Press the trigger button to release and ejectthe outer handle from the recessed housing. Rotate the handle 90 degrees counter clockwise tounlatch and open the door.
OPENING THE BAGGAGE DOOR INTERNALLY − Press the release button on the inside handleto unlock the handle from the trigger. Rotate the handle 90 degrees clockwise to open the door.
Baggage Door Indication
Visual indication of a locked condition is the baggage door secured in position and the exteriorhandle stowed and locked in the handle recess.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−59
DOOR INDICATION AND CONTROL
The airplane door position and locked indication is provided to the EICAS by the LGECU. TheLGECU provides data that is used to generate alerts and synoptic displays for the fuselage doors.
Door position information is displayed on the STAT page and message information is displayed onthe PRIMARY page.
The STAT page presents the following doors:
• PASSENGER• EMERGENCY OVERWING EXIT• BAGGAGE• SERVICE DOORS
STAT Page
PASSENGER DOORBAGGAGE DOOR
OVER WING EMERGENCY EXIT
SERVICE DOOR ANNUNCIATION
Airplane Door Position Airplane Door Graphic
CLOSED
OPEN
INVALIDG
F01
10_0
45
SERVICE DOORS
Passenger Door
The passenger door is monitored by three proximity sensors to determine the locked and handlestowed position. Proximity sensors (one at each location) are located on the passenger doorforward and aft latch to monitor the “G” latch position. A proximity sensor is mounted in thepassenger door to monitor the outer handle stowed condition.
The sensor information is used by the Landing Gear Electronic Control Unit (LGECU) for doorposition and locked indication and sends the results to EICAS for position and locked displays.
Emergency Exit
One proximity sensor is installed at the top of the door position and senses the door in the closedposition.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−60
DOOR INDICATION AND CONTROL (CONT'D)Baggage Door
Two proximity sensors monitor the door position and provide signals to the LGECU which in turnprovides the EICAS display.
Large Maintenance Doors
Two (optional third) separate large hinged and latched maintenance hatches, are monitored by theLGECU. Each door is monitored by one proximity sensor to determine the door closed condition.In each case, the proximity sensor is mounted on the airplane structure and monitors a sensor onthe hatch. The information is used by the LGECU for door position indication.
The LGECU combines the status of the aft equipment bay door with the status of the maintenancehatches to produce a single EICAS indication.
The maintenance hatches that are monitored are:
• Rear hydraulic system access door.• Refuel/defuel station door.• Optional belly fairing stowage access door.
Aft Equipment Bay Door
An electrical proximity sensor provides indication to the EICAS system when the door is properlyclosed. The LGECU monitors the signals and provides the input to EICAS.
Small Service Doors
The LGECU monitors the signals and provides input to EICAS when any one of the access/smallservice doors is not properly closed.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 201−10−61
EICAS MESSAGES
GF
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c
PASSENGER DOORCARGO DOORL−R EMER EXITDOOR SYS FAILLARGE SERV DOORSSMALL SERV DOORS
PASSENGER DOOR Comes on to indicate that the passenger door is not closed and locked.
DOOR SYS FAILComes on to indicatethe loss of fuselage and gear door indication.
CARGO DOORComes on to indicatethat the cargo door is not closed and latched.
L−R EMER EXITComes on to indicatethat the applicable emergency exit door is not in position.
SMALL SERV DOORSComes on to indicatethat any one or more of the small service doors are not closed.
LARGE SERV DOORSComes on to indicatethat one or more of the following doors are not closed:
Equipment bay.
Rear hydraulic system access.
Refuel/defuel station.
Optional belly fairing stowage access.
INT CABIN DOOR
INT CABIN DOORComes on to indicate that the interiorcabin door is closed for takeoff and landing.
AIRPLANE GENERAL
REV 51, Aug 14, 2006Flight Crew Operating Manual
CSP 700−6
Volume 201−10−62
CB - DOORS SYSTEMS
GF
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_001
STAT SYS BUS PREV CNTL TESTPAGE
NEXTPAGE
EMERCNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
SYSTEMCIRCUIT BREAKER
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
PAX DOOR MOTOR
1/1CB − DOORS SYSTEMS
AV BATT DCPC IN
BRT
AIRPLANE GENERAL
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 201−20−1
AIRPLANE GENERAL
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004Flight Crew Operating Manual
CSP 700−6
Volume 201−20−2
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