CHAPTER 1 --- AIRPLANE GENERAL - SmartCockpit · Vol. 1 01--00--1 REV56,Jan31/03 AIRPLANE GENERAL Table of Contents Flight Crew Operating Manual CSP A--013 MASTER CHAPTER 1 --- …

01--00--1Vol. 1

REV 56, Jan 31/03AIRPLANE GENERAL

Table of Contents

Flight Crew Operating ManualCSP A--013

MASTER

CHAPTER 1 --- AIRPLANE GENERAL

Page

TABLE OF CONTENTS 01--00Table of Contents 01--00--1

INTRODUCTION 01--10Abbreviations 01--10--1Conversion Factors 01--10--13Temperature Conversion Table 01--10--14

EXTERIOR 01--20

FLIGHT COMPARTMENT 01--30Reinforced Flight Compartment Door <0093, FAA> 01--30--22

Emergency Operation 01--30--22

LIST OF ILLUSTRATIONS

INTRODUCTIONFigure 01--10--1 Atmosphere Table 01--10--12

EXTERIORFigure 01--20--1 External Airplane Dimensions 01--20--1Figure 01--20--2 Engine Hazard Areas 01--20--2Figure 01--20--3 Taxiing and Turning Radii 01--20--3Figure 01--20--4 Airplane Servicing Points 01--20--4Figure 01--20--5 Airplane Parking and Mooring 01--20--5Figure 01--20--6 Covers and Plugs 01--20--6Figure 01--20--7 Airplane Antenna Locations 01--20--7Figure 01--20--8 Hazard Areas -- Radar and HF 01--20--8

FLIGHT COMPARTMENTFigure 01--30--1 Airplanes 7002 to 7451,

Flight Compartment General Arrangement 01--30--1Figure 01--30--1 Airplanes 7452 and Subsequent,

Flight Compartment General Arrangement 01--30--2Figure 01--30--2 Airplanes 7002 to 7451,

Flight Compartment (Forward View) 01--30--3Figure 01--30--2 Airplanes 7452 and Subsequent,

Flight Compartment (Forward View) 01--30--4Figure 01--30--3 Flight Compartment (AFT View) 01--30--5

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MASTERFlight Crew Operating ManualCSP A--013

Figure 01--30--4 Pilot’s Side Console 01--30--6Figure 01--30--5 Airplanes 7002 to 7672,

Pilot’s Side Panel 01--30--7Figure 01--30--5 Airplanes 7673 and Subsequent

Pilot’s Side Panel 01--30--8Figure 01--30--6 Pilot’s Instrument Panel 01--30--9Figure 01--30--7 Center Instrument Panel 01--30--10Figure 01--30--8 Overhead Panel 01--30--11Figure 01--30--9 Glareshield 01--30--12Figure 01--30--10 Center Pedestal (Upper) 01--30--13Figure 01--30--11 Center Pedestal -- Thrust Lever and Flight Controls 01--30--14Figure 01--30--12 Center Pedestal (Lower) 01--30--15Figure 01--30--13 Copilot’s Instrument Panel 01--30--16Figure 01--30--14 Airplanes 7002 to 7672,

Copilot’s Side Panel 01--30--17Figure 01--30--14 Airplanes 7673 and Subsequent

Copilot’s Side Panel 01--30--18Figure 01--30--15 Copilot’s Side Console 01--30--19Figure 01--30--16 Fwd Attendant/Observer Position 01--30--20Figure 01--30--17 Control Wheels 01--30--21Figure 01--30--18 Reinforced Cockpit Door 01--30--24

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MASTER

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.

A

A/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 . . . . . Alternate

A/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 . . . . . . Antenna

ACM . . . . . . Air Cycle Machine AOA . . . . . . Angle of Attack

ACMP . . . . Alternating Current Motor Pump/Electric Hydraulic Pump AP . . . . . . . Autopilot

ACT . . . . . . Active APC . . . . . . Auxiliary Power ControlACU . . . . . . Air Conditioning Unit APP . . . . . . ApproachADC . . . . . . Air Data Computer APPROX . . Approximately

ADDR . . . . Address APR . . . . . . Automatic PerformanceReserve

ADF . . . . . . 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 . . . . . . Attitude

AGL . . . . . . Above Ground Level ATTCS . . . . Automatic Take-off Thrust Con-trol System

AHC . . . . . . Attitude Heading Computer ATTD . . . . . Attitude

AHRS . . . . Attitude Heading ReferenceSystem ATTND . . . Attendant

AIL . . . . . . . Aileron AUTO . . . . AutomaticALIGN . . . . Aligning, alignment AUTO BAL Automatic BalanceALPHA . . . alpha AUTO XFER Automatic TransferAUX . . . . . . Auxiliary AVAIL . . . . . AvailableAV . . . . . . . Avionics AZ . . . . . . . Azimuth

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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 . . . . . . Bottle

BATT . . . . . Battery BTMS . . . . Brake Temperature MonitoringSystem

BDI . . . . . . . Bearing Distance Indicator BTMU . . . . Brake Temperature MonitoringUnit

BFO . . . . . . 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 . . . . Connection

CDP . . . . . . Compressor DischargePressure CONT . . . . Control, Continuous, Contactor,

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

CPAM . . . . Cabin Pressure AcquisitionModule

CG . . . . . . . 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

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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 . . . . . . . Direct

DECEL . . . Decelerate(d) DIS . . . . . . . Distance (to way point),Disconnect

DECR . . . . Decrease DISC . . . . . DisconnectDEFL . . . . . Defuel DISCH . . . . DischargeDEG . . . . . . Degree DISP . . . . . Dispatch, DisplayDEPR . . . . Depressurize DIST . . . . . DistanceDEPT . . . . . Departure DME . . . . . . Distance Measuring EquipmentDEST . . . . . Destination DN . . . . . . . Down

DET . . . . . . Detector DOT . . . . . . Department of Transport(Canada)

DEV . . . . . . Deviation DR . . . . . . . Door

DFDAU . . . Digital Flight Data AcquisitionUnit

DFDR . . . . 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 Datum

EDP . . . . . . Engine Driven Pump/EnginePrimary Hydraulic Pump ESS . . . . . . Essential

EFIS . . . . . . Electronic Flight InstrumentSystem ET . . . . . . . Elapsed Time

EGT . . . . . . Exhaust Gas Temperature ETA . . . . . . Estimated Time of Arrival

EICAS . . . . Engine Indication and CrewAlerting System EVAC . . . . . Evacuation

EL . . . . . . . . Elevation EXH . . . . . . ExhaustELEC . . . . . Electrical EXTIN . . . . Extinguish(ed)ELEV . . . . . Elevator, ElevationELT . . . . . . Emergency Locator Transmitter

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FF/CTL . . . . Flight Controls FL CH . . . . Flight Level Change

FAA . . . . . . Federal Aviation Administration(USA) FLD . . . . . . Field

FAIL . . . . . . Failure FLT . . . . . . . FlightFCC . . . . . . Flight Control Computer FLT DIR . . . Flight DirectorFCU . . . . . . Fuel Control Unit FLUOR . . . Fluorescent

FD, 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 Minute

GAL . . . . . . Gallon GPWS . . . . Ground Proximity WarningSystem

GALY . . . . . 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 Indicator

HEAT . . . . . Heater HSTA . . . . . Horizontal Stabilizer TrimActuator

HF . . . . . . . High Frequency (3 -- 30 mHz) HSTCU . . . Horizontal Stabilizer TrimControl Unit

Hg . . . . . . . Mercury HTR . . . . . . HeaterHGS . . . . . . Head-up Guidance System HUD . . . . . . Heads-up DisplayHI . . . . . . . . High HYD . . . . . . HydraulicHLDR . . . . . Holder Hz . . . . . . . . HertzHOR,HORIZ . . . . HorizontalHOT . . . . . . High Oil Temperature

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II/B . . . . . . . . Inboard INCR . . . . . IncreaseI/C . . . . . . . Intercom, Inspection Check IND . . . . . . . Indication, Indicator

IAPS . . . . . Integrated Avionics ProcessorSystem INFLT . . . . . In Flight

IAS . . . . . . . Indicated Air Speed INHIB . . . . . Inhibit

ICAO . . . . . International Civil AviationOrganization INOP . . . . . Inoperative

ICS . . . . . . . Idle Corrected Speed INPH . . . . . InterphoneID . . . . . . . . Identification INSP . . . . . InspectionIDENT . . . . Identification INST(S) . . . Instrument(s)

IDG . . . . . . Integrated Drive Generator INST,INSTR . . . . Instrument

IFR . . . . . . . Instrument Flight Rules INT . . . . . . . Internal, Integral, IntersectionIGN . . . . . . Ignition INTEG . . . . IntegralILS . . . . . . . Instrument Landing System IRS . . . . . . . Inertial Reference SystemIM . . . . . . . . ILS Inner Marker IRU . . . . . . . Inertial Reference Unit

IMC . . . . . . Instrument MeteorologicalConditions ISA . . . . . . . International Standard

Atmosphere

IMP . . . . . . Imperial ISO . . . . . . . International StandardOrganization

IN . . . . . . . . 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

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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 Graphic

LCN . . . . . . Load Classification Number LOM, MM . Compass Locator at OuterMarker

LCV . . . . . . 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 Afterward

MAA . . . . . . Maximum Authorized IFRAltitude MID FWD . Middle Forward

MAC . . . . . . 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

mbs . . . . . . Millibars MMO . . . . . Maximum Operating Speed inMach Number

MCA . . . . . . Minimum Crossing Altitude MOCA . . . . Minimum Obstruction ClearanceAltitude

MCT . . . . . . 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

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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 . . . . Normal

NDB (ADF) Nondirectional Beacon(Automatic Direction Finder) NOSE . . . . Nose Wheel

NEG . . . . . . 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

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PP#6 . . . . . . Panel 6 PRESS . . . Pressure, PressurizationP/S . . . . . . . Pitot/Static PRI . . . . . . . PrimaryPA . . . . . . . Passenger Address PRIM . . . . . PrimaryPASS . . . . . Passenger PROC . . . . Procedure

PBE . . . . . . Portable Breathing Equipment(Smoke Hood) PROT . . . . Protection

PCU . . . . . . Power Control Unit PROX . . . . Proximity

PF . . . . . . . Pilot Flying PSEU . . . . . Proximity Sensor ElectronicsUnit

PFD . . . . . . 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 . . . . . . Rotation

RAI . . . . . . . Registro Aeronautico Italiano(Italy) RPM . . . . . . Revolutions Per Minute

RAT . . . . . . Ram Air Turine RT, R/T . . . Receiver-Transmitter

RCCB . . . . Remote Controlled CircuitBreaker RTE . . . . . . Route

RCDR . . . . 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

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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 . . . . . . Station

SECS . . . . . Spoiler Electronic ControlSystem STAB . . . . . Stabilizer

SECU . . . . Spoiler Electronic Control Unit STAT . . . . . StatusSEL . . . . . . Select, Selector STBY . . . . . StandbySELCAL . . Selective Call STEER . . . SteeringSENS . . . . . Sensitivity, Sensor SUPPL . . . SupplySERV,SVCE . . . . . Service SW(s) . . . . Switches

SMKG . . . . 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 TOGA . . . . . Take-off / Go-aroundTACAN . . . UHF Tactical Air Navigation Aid TOL . . . . . . ToleranceTAS . . . . . . True Airspeed TRB, TURB TurbulenceTAT . . . . . . Total Air Temperature TRK . . . . . . TrackTCAS . . . . . Traffic Alert and Collision

Avoidance System TRM . . . . . . Trim

TE . . . . . . . Trailing Edge TRU . . . . . . Transformer Rectifier UnitTEMP . . . . Temperature TT2 . . . . . . Engine Inlet Temperature

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

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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 Intensity

V1 . . . . . . . . . . . . . . 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 Speed

VDF/MDF . . . . . .Demonstrated flight divingspeed. V/S . . . . . . . Vertical Speed

VEF . . . . . . . . . . . . Engine Failure Speed VERT . . . . . VerticalVF . . . . . . . . . . . . . . Design Flap Speed VFR . . . . . . Visual Flight Rules

VFC /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-

tionsVLOF . . . . . . . . . . . Lift-off Speed VNAV . . . . . Vertical Navigation

VMC . . . . . . . . . . . .Minimum Control Speed withthe Critical Engine Inoperative VOL . . . . . . Volume

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

VMU . . . . . . . . . . . . Minimum Unstick Speed VOR . . . . . . VHF Omnidirectional RangeStation

VR . . . . . . . . . . . . . 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 . . . . . Warning

WARN . . . . Warning WS . . . . . . . Second Segment LimitedWeight

WF . . . . . . . Runway Length Limited Weight WSHLD . . . WindshieldWGT . . . . . Weight WX . . . . . . . WeatherWHLS . . . . Wheels WXR . . . . . Weather Radar

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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

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Atmosphere TableFigure 01---10---1

7000 2296.56

ALTITUDE PRESSURE TEMPERATURE

Feet Meters Hg Mb PSIA ûCûF

0 29.92 1013.2 14.70 59 15

1000 328.08 28.86 977.2 14.17 55.4 13

ATMOSPHERE TABLE

2000 656.16 27.82 942.1 13.66 51.8 11

3000 984.24 26.82 908.1 13.17 48.3 9.1

4000 1312.32 25.84 875.1 12.69 44.8 7.1

5000 1640.40 24.90 843.0 12.23 41.2 5.1

6000 1972.48 23.98 812.0 11.78 37.6 3.1

23.09 781.9 11.34 34.0 1.1

22.23 752.6 10.92 30.5 ---.9

21.39 724.3 10.51 26.9 ---2.8

10,000 3280.80 20.58 696.8 10.11 23.3 ---4.8

15,000 4921.20 16.89 571.8 8.29 5.5 ---14.7

20,000 6561.60 13.75 465.6 6.75 ---12.3 ---24.6

25,000 8202.0 11.10 376.0 5.45 ---30.1 ---34.5

30,000 9842.4 8.90 300.9 4.36 ---47.9 ---44.4

35,000 11,482.8 7.04 238.4 3.46 ---65.7 ---54.3

40,000 13,152.0 5.54 187.5 2.72 ---69.7 ---56.5

0

8000 2624.64

9000 2952.72

NOTE

The above table is presented for guidancepurposes only. For more information, refer tothe ICAO Standard Atmosphere Tables.

01--10--13Vol. 1


Introduction


MASTER

2. CONVERSION FACTORS

Multiply By To Obtain Multiply By To Obtain

Centimeters 0.3937 in Km/hr 0.540.6214

knotsmph

Centimeters2 0.155 in2 Knots 1.1511.852

mphkm/hr

Centimeters3 0.061 in3 kPa 0.145 psi

Ft 0.3048 meters Liters 0.26420.22

USGImperial gal

Ft2 0.0929 meters2 Meters 3.281 ftFt3 0.0283 meters3 Meters2 10.76 ft2

Gal, Imperial 1.2014.546

USGliters Meters3 35.3115 ft3

Gal, US 3.7850.8327

litersImperial gal Miles

52801.6090.869

ftkm

nautical miles

In 2.54 cm Mph 1.6090.869

km/hrknots

In2 6.452 cm2 Nautical Miles 1.1511.852

milesm

In3 16.387 cm3 Pounds (lb) 0.45 kilogramsKilograms 2.205 lb PSI 6.895 kPa

Kilometers 0.62140.54

milesnautical miles

REV 56, Jan 31/03


Introduction


3. TEMPERATURE CONVERSION TABLE

ûC a ûFbûC 'ûF ûC a ûFbûC 'ûF ûC a ûFbûC 'ûF ûC a ûFbûC 'ûF ûC a ûFbûC 'ûF ûC a ûFbûC 'ûF-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

5.06.88.610.412.2

1.72.22.83.33.9

3536373839

95.096.898.6100.4102.2

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

01--20--1Vol. 1


Exterior


MASTER

External Airplane DimensionsFigure 01---20---1

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)

REV 56, Jan 31/03


Exterior


Engine Hazard AreasFigure 01---20---2

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

01--20--3Vol. 1


Exterior


MASTER

Taxiing and Turning RadiiFigure 01---20---3

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)

REV 56, Jan 31/03


Exterior


Airplane Servicing Points <MST>Figure 01---20---4

NO. 3 HYDRAULIC SYSTEMACCUMULATOR CHARGINGPOINT AND PRESSURE GAUGE

OVERWING GRAVITYFUEL FILLER (TYP)

FUEL LEVELINDICATOR

PRESSURE REFUEL/DEFUELPANELAND ADAPTER

OXYGEN SYSTEMCHARGING VALVEAND GAUGE

AC EXTERNALPOWER

BRAKE ACCUMULATORCHARGING POINTSAND INTERPHONE

FUEL LEVELINDICATORS

FUEL LEVELINDICATORFUEL TANK

WATER DRAIN(TYP)

NO. 3 HYDRAULICSYSTEM

NO. 3 HYDRAULIC SYSTEMRESERVOIR FILLERCONNECTION

GROUND AIRCONNECTION

ENGINE OIL TANK

DC EXTERNALPOWER

LOW PRESSUREAIR GROUNDCONNECTION<0007>

NO. 2 HYDRAULICSYSTEM

NO. 1 HYDRAULICSYSTEM AND REARINTERPHONE

OIL REPLENISHMENTTANK PANEL(AFT EQUIPMENT BAY)

01--20--5Vol. 1


Exterior


MASTER

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

REV 56, Jan 31/03


Exterior


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

01--20--7Vol. 1


Exterior


MASTER

Airplane Antenna Locations <MST>Figure 01---20---7

WEATHERRADAR

GLIDESLOPE

VOR ANDLOCALIZER(BOTH SIDES)

EMERGENCYLOCATORTRANSMITTER

UNDERWATERLOCATORBEACONS(CVR AND FDR) MARKER BEACON 1

MARKER BEACON 2

VHF 2ATC 2(BOTH SIDES)

TCASOMNIDIRECTIONAL

TCASDIRECTIONAL

ATC 2ATC 1 OTHER SIDE

VHF 3<0008><0014>

VHF 1

ADF

RADIOALTIMETER DME 2

DME 1OTHER SIDE

RADIOALTIMETER<0045>

HF<0011, 0060>

GPS(BOTH SIDES)<0027, 0047>

REV 56, Jan 31/03


Exterior


Hazard Areas --- Radar and HF <MST>Figure 01---20---8

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

HF ANTENNA175 watt (peak)50 watt (average)<0011><0060>

01--30--1Vol. 1

REV 56, Jan 31/03AIRPLANE GENERALFlight Compartment


MASTER

Flight Compartment General Arrangement Airplanes 7002 to 7451, <MST>Figure 01---30---1

<0083>

TWO INSTRUMENTS ARE TYPICAL.ONE UNIT ONLY FOR OPTION <0083>WHICH IS TOP UNIT.

NOTE

1

2

4

5

6

8

13

13

3

11

12

9

14

17

10

7

19

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 topencil holder and map light).

6. Sun visor.7. HGS combiner <0026>.8. Overhead speaker.9. HGS overhead unit <0026>.

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 <0083>

99

REV 56, Jan 31/03

Vol. 1 01--30--2AIRPLANE GENERALFlight Compartment


Flight Compartment General Arrangement Airplanes 7452 and Subsequent, <MST>Figure 01---30---1


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 topencil holder and map light).

6. Sun visor.7. HGS combiner <0026>.8. Overhead speaker.9. HGS overhead unit <0026>.

<0083>

TWO INSTRUMENTS ARE TYPICAL.ONE UNIT ONLY FOR OPTION <0083>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 <0083>

1

2

4

5

6

108

13

13

3

11

12

9

14

17

7

19

18

15

3

16

1

812

19

9

17

5

01--30--3Vol. 1



MASTER

Flight Compartment (Forward View) Airplanes 7002 to 7451, <MST>Figure 01---30---2

AC essential bus circuitbreaker panel CBP--3(Pilot’s side console,forward foot--well area).

DC essential bus circuitbreaker panel CBP--4(Copilot’s side console,forward foot--well area).

CIRCUIT BREAKER PANELS

OVERHEADPANEL

CENTERINSTRUMENTPANEL

COPILOT’SINSTRUMENTPANEL

COPILOT’SSIDE CONSOLE

PILOT’SINSTRUMENTPANEL

PILOT’SSIDECONSOLE

CENTERPEDESTAL

GLARESHIELD

COPILOT’SSEAT

<0026>

1

PILOT’SSEAT 1

7

<0083>



REV 56, Jan 31/03



Flight Compartment (Forward View) Airplanes 7452 and Subsequent, <MST>Figure 01---30---2

AC essential bus circuitbreaker panel CBP--3(Pilot’s side console,forward foot--well area).

DC essential bus circuitbreaker panel CBP--4(Copilot’s side console,forward foot--well area).

CIRCUIT BREAKER PANELS 7

COPILOT’SINSTRUMENTPANEL

COPILOT’SSIDE CONSOLE

PILOT’SINSTRUMENTPANEL

PILOT’SSIDECONSOLE

CENTERPEDESTAL

GLARESHIELD

COPILOT’SSEAT 1

PILOT’SSEAT 1

CENTERINSTRUMENTPANEL

OVERHEADPANEL



<0026>

<0083>

01--30--5Vol. 1



MASTER

Flight Compartment (AFT View) <MST>Figure 01---30---3


CIRCUITBREAKERPANEL (CBP--2)

CIRCUITBREAKERPANEL (CBP--1)

FLASHLIGHT FLASH

LIGHT

PORTABLEBREATHINGEQUIPMENT (PBE)(SMOKE HOOD)

EMERGENCYAXE

LIFE VEST (2):BENEATH PILOTAND COPILOT SEATS

MULTI--FUNCTIONDISPLAYMAINTENANCEMODE SWITCH

MAINT

MFD 2

MFD 1

OFF

FUEL QUANTITY PRESELECTPANEL <0017> B

A

2

13

PILOT HATCLIP ANDDECAL

HATCLIPHAT CLIP

COPILOTHAT CLIPAND DECAL

9

B

A

7

9

HALON (1211)FIRE EXTINGUISHER

9

7

9

Airplane LevelIndicators -- Used withmagnetic level indicators, tomanually gauge fuel quantity.

C

13

C NOTEEscape roperepositioned.

9

REV 56, Jan 31/03



Pilot�s Side ConsoleFigure 01---30---4


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

01--30--7Vol. 1



MASTER

Pilot�s Side Panel Airplanes 7002 to 7672,<MST>Figure 01---30---5


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

LEGEND

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

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

<0040>

BARO

HPA/INMDADH

SPEED REFS

SEL

RATESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE


12

215

12 1812 18 17

11

168

REV 56, Jan 31/03



Pilot�s Side Panel Airplanes 7673 and Subsequent, <MST>Figure 01---30---5


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

LEGEND

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

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

<0040>

BARO

HPA/INMDADH

SPEED REFS

SEL

RATESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE

RST

SEL

ET

MODE

CHR

INT

CHR


215

12 1812 18

1217

11

168

01--30--9Vol. 1



MASTER

Pilot�s Instrument Panel <MST>Figure 01---30---6


FLIGHTDIRECTOR / AUTOPILOTMODE ANNUNCIATOR

ALTIMETER

ATTITUDEDIRECTORINDICATOR

AIRSPEEDLIMITSPLACARD(TYPICAL)

PRIMARYFLIGHTDISPLAY

AIRSPEEDINDICATOR

NAVIGATIONANNUNCIATORS

COCKPITVOICERECORDER

HORIZONTALSITUATIONINDICATOR

VERTICAL SPEEDINDICATORAND TCASRESOLUTIONADVISORY

<0015>

10

10

MULTIFUNCTIONDISPLAYHSI MODENAVAID SECTORMAPPRESENTPOSITION MAP<0024><0050>PLAN MAP<0024><0050>TCAS TRAFFICWEATHERRADAR12

12

18

1812

5 12

18

18

<0024>

<0049, 0050>

FMS 2

FMS

REV 56, Jan 31/03



Center Instrument Panel <MST>Figure 01---30---7

NOTE


MLG BAY OVHTDISPLAY COOL

<0015>

<0083>

Standby AttitudeIndicator 12

<0006><0039>

Standby Airspeed /Altitude / AttitudeIndicator 12

StandbyAltimeter/IndicatedAirspeed Indicator

12

8

Engine Indication and Crew AlertingSystem (EICAS) Primary DisplayEngine 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

01--30--11Vol. 1



MASTER

Overhead Panel <MST>Figure 01---30---8


<0043><0053><0059>

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

<0013><0034><0074>

CKPT CABIN

COLDHOTAIR

CARGOOFF

COND.

FA

CKPT CABIN

COLDHOT

OFF

FAN

N

FAIL

BOTTLEAPU

<0057>18

1

2 3 4

6

8

111213

14

15

<0016>

17

16

5

7

910

15

ELT

MAN

ARM/RESET

AUTO

OFF

ON

OFF

ON

STROBEWINGINSP

<0020>

<0091>

MISC LTS

OFFON

DIM

STBYCOMP

OFF

DOMELIGHT

ONOFF

STERILE

ON

PASS SIGNS

APU

OFF

ON

OFF

ON

OFF

ON

NAV BEACON STROBEWING

EXTERNAL LTS

INSP

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

ON

INOP INOP

ON

FAIL FAIL

ONON

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

LOOPA

LOOP B

DUCTMON

XFLOWGRAVITY

FAIL

XFLOWAUTOOVERRIDE

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 WITHALL RADIOS ON SWUNG BY

TO FLY

STEER

N 45 E 135 S 225 W 315

EMER LTSNO

SMKGSEATBLTS

ONOFFAUTO

ONOFFARM

OFF

ELT

ON

ARM/RESET

FORAVIATIONEMER USE ONLY

ELT

ON

NORMTEST 1

TEST 2

BOTTLECARGO

LOGO

OFF

ON

OFF

ON

NAV

EXTERNAL LTS

<0020,0021> OFF

ON

OFF

ON

OFF

ON

NAV BEACON STROBEWING

EXTERNAL LTS

INSP

OFF

ON

OFF

ON

LOGO

REV 56, Jan 31/03



Glareshield <MST>Figure 01---30---9

RIGHT GLARESHIELD

LEFT GLARESHIELD

CENTER GLARESHIELD

1 2 3 4 5 6

7

9 6

5

12

34

8

7 7

<0040>


<0040>

LEGEND1. Roll Select Switch/Light.2. Master Warning Switch/Light.3. Master Caution Switch/Light.4. Stall Warning Switch/Light.5. GPWS and Glideslope WarningSwitch/Light.PULL UP / GND PROX GlideslopeSwitch/Light. <0040>

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

1122

11

18

1010

310

18

01--30--13Vol. 1



MASTER

Center Pedestal (Upper) <MST>Figure 01---30---10


<0024, 0049, 0050>

FMS

1 2 3

4 5 6

7 8 9

0

A

F

K

P

U

Z

B

G

L

Q

V

SP

C

H

M

R

W

DEL

D

I

N

S

X

/

E

J

O

T

Y

CLR

MOD BRT

MSGDIRINTC

PREVPAGE

FPLNNEXTPAGE

EXECMDCUMENULEGS

HOLD

VNAV

DEPARR

SECFPLN

RADIO PERF

MFDMENU

PROG

MFDADV

MFDDATA

RADIORADIO

INDEX FIX

<0024>

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

ARMED

ANTI SKID

DN LCKREL

OVHT TESTWARN FAIL

MLG BAYOVHT

UPDN

MUTED

TEST

MECH

PUSH

CALL

FLAP

OVRD

TERRAIN

OFF

GRND PROX

8

<0040>

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

V

SP

C

H

M

R

W

DEL

D

I

N

S

X

/

E

J

O

T

Y

CLR

MOD BRT

MSGDIRINTC

PREVPAGE

FPLNNEXTPAGE

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

REV 56, Jan 31/03



Center Pedestal --- Thrust Lever and Flight Controls <MST>Figure 01---30---11

8

<0006>


6

41 3

9

2

5

7

<0029>

Option removesGround ProximityWarning System/FlapOverride Switch

<0040>

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 <0029>8. Thrust Lever Quadrant9. Thrust Reverser Subpanel

1111

1111

11

11

2020

LEGEND

12

01--30--15Vol. 1



MASTER

Center Pedestal (Lower) <MST>Figure 01---30---12


1

3

45

7

89

10

3

16

14

2

1315 16

17

18

19

6

3

1

<0028>

ACT

STBY

ELV

G/S

FAULT CLR BRT + DIM --

1 2 3

4 5 6

7 8 9ENTER 0 TEST

HGS

CARGOARMED

CARGO FIREX

STANDBYNORMAL

SMOKEPUSH

BOTTLE

PUSH TODISCH

CARGOARMEDSMOKE

PUSH

BOTTLE

PUSH TODISCH

6

20<0026>

<0012>

PA

<0060>

12

16A<0025>

<0008> <0014><0011>

<0008><0011> <0014>

PA

<0008><0014> <0060>

LEGEND

16

1212

8

511

16

12

718

11

7

5

10

11

18

25 18

17

11

2 12

5

REV 56, Jan 31/03



Copilot�s Instrument Panel <MST>Figure 01---30---13


<0015>

<0024>

<0049, 0050>

FMS 2

FMS

FLIGHTDIRECTOR / AUTOPILOTMODE ANNUNCIATOR

ATTITUDEDIRECTORINDICATOR

AIRSPEED LIMITSPLACARD (TYPICAL)

PRIMARYFLIGHTDISPLAY

AIRSPEEDINDICATOR

NAVIGATIONANNUNCIATORS

HORIZONTALSITUATIONINDICATOR

VERTICAL SPEEDINDICATORAND TCASRESOLUTIONADVISORY

18

1812

1812

123

12

ALTIMETER

MULTIFUNCTIONDISPLAYHSI MODENAVAID SECTORMAPPRESENTPOSITION MAP<0024><0050>PLAN MAP<0024><0050>TCAS TRAFFICWEATHER RADAR

18

10

10

11

01--30--17Vol. 1



MASTER

Copilot�s Side Panel Airplanes 7002 to 7672, <MST>Figure 01---30---14

1 2

4 5

3

6

7

8

STALLPTCT

PUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF



OFF

ON

FLOOR

NORM

PFD 1 EICAS

NAVSOURCE

FORMAT RANGE

BARO

HPA/INMDADH

SPEED REFS

SEL

RATESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE

<0040>


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

13


REV 56, Jan 31/03



Copilot�s Side Panel Airplanes 7673 and Subsequent, <MST>Figure 01---30---14

1 2

4 5

3

6

7

8

STALLPTCT

PUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF



OFF

ON

FLOOR

NORM

PFD 1 EICAS

NAVSOURCE

FORMAT RANGE

BARO

HPA/INMDADH

SPEED REFS

SEL

RATESTTGT VSPDS

SET

SET

RST

SEL

ET

MODE

CHR

INT

CHR

NAVSOURCE

FORMAT RANGE

<0040>


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

13


01--30--19Vol. 1



MASTER

Copilot�s Side Console <MST>Figure 01---30---15


AIRCONDITIONINGSYSTEMOUTLET

AUDIO WARNING

FLIGHT BAGCOMPARTMENT

SOURCESELECTOR/ISOLATIONVALVES


MACHTRANSDUCER

PITOT


MACHTRANSDUCER

STATICNORMAL NORMAL

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS

HDPHMIC

<0019>

AUDIO WARNING

DATACONCENTRATORUNITAUDIO WARNINGDISABLE SWITCHES

OXYGEN MASKREGULATORSTORAGECOMPARTMENT

COPILOTHAT HOOK

AA

B

B

C

C

REV 56, Jan 31/03



Fwd Attendant/Observer PositionFigure 01---30---16

OBSERVER’SHEADSETHOOK

OBSERVER’S STATIONRIGHT HAND SIDE

OBSERVER’SSEAT

OBSERVER’S STATIONLEFT HAND SIDE

OBSERVER’SJACK PANEL

OBSERVER’SOXYGENMASK/REGULATORSTORAGEUNIT

01--30--21Vol. 1



MASTER

Control WheelsFigure 01---30---17

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

REV 56, Jan 31/03



1. REINFORCED FLIGHT COMPARTMENT DOOR <0093><FAA>

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:

S Slide latch

S Deadbolt assembly

S Two quick--release hinge pins

S Viewer

S 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.

01--30--23Vol. 1



MASTER

CAUTION

The lower hingepinmust be releasedbefore 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.

REV 56, Jan 31/03



Reinforced Cockpit DoorFigure 01---30---18 Sheet 1

HINGE ASSEMBLY

COCKPIT DOOR

HINGE ASSEMBLY

UPPERDECOMPRESSIONPANEL

SLIDELATCH

DEADBOLTASSEMBLY

VIEWER(PEEPHOLEASSEMBLY)

POCKETENCLOSURE

A

AB

01--30--25Vol. 1



MASTER

Reinforced Cockpit DoorFigure 01---30---18 Sheet 2

B

PRESSURERELEASELATCH

UPPER HINGEHANDLE

RETRACTABLEBOLTS

SLIDELATCH

DEADBOLT

NAMEPLATE

STRAPHANDLE

STRAPHANDLE

UPPER HINGEHANDLE

REV 56, Jan 31/03



THIS PAGE INTENTIONALLY LEFT BLANK

Documents

CHAPTER 1 --- AIRPLANE GENERAL - SmartCockpit · Vol. 1 01--00--1 REV56,Jan31/03 AIRPLANE GENERAL Table of Contents Flight Crew Operating Manual CSP A--013 MASTER CHAPTER 1 --- …