canadair regional jet 100/200 - aircraft general · minimum control speed with the critical engine...

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 . . . .��

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

Canadair Regional Jet 100/200 - Aircraft General

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,Controller

CDU . . . . . . 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


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


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


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 GeneratorINST,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 StandardAtmosphere

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


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

�� 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


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


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


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 �� TACAN . . . UHF Tactical Air Navigation Aid TOL . . . . . . ToleranceTAS . . . . . . True Airspeed TRB, TURB TurbulenceTAT . . . . . . Total Air Temperature TRK . . . . . . TrackTCAS . . . . . Traffic Alert and Collision

Avoidance SystemTRM . . . . . . Trim

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

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


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-tions

VLOF . . . . . . . . . . . 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


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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56�� 7�� !" $! "

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)


5� �� (�8�� !" $! $

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


�6�� 9�� !" $! +

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)


�� :�� )�� <MST>

�� !" $! ,

NO. 3 HYDRAULIC SYSTEMACCUMULATOR CHARGINGPOINT AND PRESSURE GAUGE

OVERWING GRAVITYFUEL FILLER (TYP)

FUEL LEVELINDICATOR

PRESSURE REFUEL/DEFUELPANEL AND ADAPTER

OXYGEN SYSTEMCHARGING VALVEAND GAUGE

AC EXTERNALPOWER

BRAKE ACCUMULATORCHARGING POINTSAND INTERPHONE

FUEL LEVELINDICATORS

FUEL 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)


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


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


�� 0�� <MST>

�� !" $! #

WEATHERRADAR

GLIDESLOPE

VOR ANDLOCALIZER(BOTH SIDES)

EMERGENCYLOCATORTRANSMITTER

UNDERWATERLOCATORBEACONS(CVR AND FDR)

MARKER BEACON 1MARKER BEACON 2

VHF 2

ATC 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>


(�8�� 9�� (� <MST>

�� !" $! -

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

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


�� Airplanes 7002 to 7451, <MST>

�� !" +! "

<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 to

pencil 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


�� Airplanes 7452 and Subsequent, <MST>

�� !" +! "


Effectivity:Airplanes 7452 and subsequent.

LEGEND

11

11

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

pencil holder and map light).6. Sun visor.7. HGS combiner <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


�� 3��;�� <��;4 Airplanes 7002 to 7451, <MST>

�� !" +! $

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>




�� 3��;�� <��;4 Airplanes 7452 and Subsequent, <MST>

�� !" +! $

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>


�� 3�� <��;4 <MST>

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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

HAT CLIPHAT 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 NOTE

Escape roperepositioned.

9


)��=� �� !" +! ,


FLIGHT BAGCOMPARTMENT

NOSE WHEELSTEERING TILLER

OXYGEN MASKREGULATORSTORAGECOMPARTMENT

AIRCONDITIONINGSYSTEMOUTLET

ENGINEOIL LEVELPANEL SOURCE

SELECTOR/ISOLATIONVALVES 12

RHSTOP/STARTLH

16

20

9

SELECTOR

VALVE CLOSED

MACHTRANSDUCER

PITOT

SELECTOR

VALVE CLOSED

MACHTRANSDUCER

STATIC

NORMAL NORMAL

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS

AIR CONDITIONINGSYSTEM INTAKE

5

MICHDPH


)��=� �� )�� Airplanes 7002 to 7672,<MST>

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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 control

panel.

1

2

3

4

7

6

9

NORM

PFD 1 EICAS

STALL

PTCTPUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF

NAV

SOURCE

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

RA TESTTGT VSPDS

SET

SET

NAV

SOURCE

FORMAT RANGE


12

215

12 1812 18 17

11

16

8


)��=� �� )�� Airplanes 7673 and Subsequent, <MST>

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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 control

panel.

1

2

3

4

7

6

9

NORM

PFD 1 EICAS

STALL

PTCTPUSHER

FAST

SLOW

WIPER

OFF

ON

PARKOFF

NAV

SOURCE

FORMAT RANGE

N/W STRGARMED

OFF

8

5



OFF

ON

FLOOR

<0040>

BARO

HPA/INMDADH

SPEED REFS

SEL

RA TESTTGT VSPDS

SET

SET

NAV

SOURCE

FORMAT RANGE

RST

SEL

ET

MODE

CHR

INT

CHR


215

12 1812 18

12

17

11

16

8


)��=� *�� )�� <MST>

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FLIGHTDIRECTOR / AUTOPILOTMODE ANNUNCIATOR

ALTIMETER

ATTITUDEDIRECTORINDICATOR

AIRSPEEDLIMITSPLACARD(TYPICAL)

PRIMARYFLIGHTDISPLAY

AIRSPEEDINDICATOR

NAVIGATIONANNUNCIATORS

COCKPITVOICERECORDER

HORIZONTALSITUATIONINDICATOR

VERTICAL SPEEDINDICATORAND TCASRESOLUTIONADVISORY

<0015>

10

10

MULTIFUNCTIONDISPLAY

HSI MODENAVAID SECTORMAPPRESENTPOSITION MAP<0024><0050>

PLAN MAP<0024><0050>

TCAS TRAFFICWEATHERRADAR12

12

18

1812

5 12

18

18

<0024>

<0049, 0050>

FMS 2

FMS


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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 Display

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

202

1311

16

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

615

1113

7

8

2

Placards apply onlyto aircraft with enginesmixed 3A1/3B1

KNOTS

mb/hPa In Hg

180 200 220 250

IAS


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<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.

F

A

CKPT CABIN

COLDHOT

OFF

FAN

N

FAIL

BOTTLE

APU

<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

STROBEWING

INSP

<0020>

<0091>

MISC LTS

OFF

ON

DIM

STBY

COMP

OFF

DOME

LIGHT

ON

OFF

STERILE

ON

PASS SIGNS

APU

OFF

ON

OFF

ON

OFF

ON

NAV BEACON STROBEWING

EXTERNAL LTS

INSP

OFF

ON

AUTOOFF OFF

ON

AUTOOFF

ON

AUTO

1 3A 3B 2

ON

HYDRAULIC

AIR--CONDITIONING

WING

OFFON

TEST

PROBESLH RH

LOWHI

LOWHI

OFF/RESET

LH

MISC LTSOVHD

DIM BRT

OFF

ON

DIM

STBY

COMP

OFF

DOME

LIGHT

PWR

FUEL

START

FAILSOVFAILPUMP

ON

INOP INOP

ON

FAIL FAIL

ONON

OPEN

L R

L BOOSTPUMP

R BOOSTPUMP

F

U

E

L

BLEED AIR14TH STAGE

10TH STAGEL ISOL R

L APU LCV ISOL R

CLOSED CLOSED

CLOSED CLOSEDOPENOPEN

OPEN

DUCTFAIL

DUCTFAIL

DUCTFAIL

DUCTFAILFAIL

TESTNORM

LOOP A

LOOP B

DUCTMON

XFLOW

GRAVITY

FAIL

XFLOW

AUTO OVERRIDE

FIREX MONITOR

FIRE DETECTION

FAIL

BOTTLEENGINE BOTTLE

LH APU RH TESTWARNJETENG

A

BOTH

B

JET ENG

NORM

TEST

NORM

TEST

1 APU2

ANTI--ICE

RHWSHLDOFF/RESET

START/STOP

AVAIL

ON

PASS OXY

STANDBY COMPASS WITH ALL RADIOS ON SWUNG BY

TO FLY

STEER

N 45 E 135 S 225 W 315

EMER LTSNO

SMKGSEATBLTS

ON

OFF

AUTO

ON

OFF

ARMOFF

ELT

ON

ARM/

RESET

FOR AVIATIONEMER USE ONLY

ELT

ON

NORM

TEST 1

TEST 2

BOTTLE

CARGO

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


�� <MST>

�� !" +! %

RIGHT GLARESHIELD

LEFT GLARESHIELD

CENTER GLARESHIELD

1 2 3 4 5 6

7

9 6

5

12

34

8

7 7

<0040>


<0040>

LEGEND

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

Switch/Light.PULL UP / GND PROX GlideslopeSwitch/Light. <0040>

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

112

211

18

1010

310

18


�� )�� 31��4 <MST>

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<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

MSGDIR

INTC

PREV

PAGEFPLN

NEXT

PAGE

EXECMDCU

MENULEGS

HOLD

VNAV

DEP

ARR

SEC

FPLN

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

2

OFF

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

16

16

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

MSGDIR

INTC

PREV

PAGEFPLN

NEXT

PAGE

EXECMDCU

MENULEGS

HOLD

VNAV

DEP

ARR

SEC

FPLN

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


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8

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6

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9

2

5

7

<0029>

Option removesGround ProximityWarning System/FlapOverride Switch

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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


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1

3

4

5

7

89

10

3

16

14

2

1315 16

17

18

19

6

3

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ACT

STBY

ELV

G/S

FAULT CLR BRT + DIM --

1 2 3

4 5 6

7 8 9

ENTER 0 TEST

HGS

CARGOARMED

CARGO FIREX

STANDBYNORMAL

SMOKE

PUSH

BOTTLE

PUSH TODISCH

CARGOARMEDSMOKE

PUSH

BOTTLE

PUSH TODISCH

6

20<0026>

<0012>

PA

<0060>

12

16A<0025>

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<0008><0011> <0014>

PA

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FMS 2

FMS

FLIGHTDIRECTOR / AUTOPILOTMODE ANNUNCIATOR

ATTITUDEDIRECTORINDICATOR

AIRSPEED LIMITSPLACARD (TYPICAL)

PRIMARYFLIGHTDISPLAY

AIRSPEEDINDICATOR

NAVIGATIONANNUNCIATORS

HORIZONTALSITUATIONINDICATOR

VERTICAL SPEEDINDICATORAND TCASRESOLUTIONADVISORY

18

1812

1812

123

12

ALTIMETER

MULTIFUNCTIONDISPLAY

HSI MODENAVAID SECTORMAPPRESENTPOSITION MAP<0024><0050>

PLAN MAP<0024><0050>

TCAS TRAFFICWEATHER RADAR

18

10

10

11


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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

RA TESTTGT VSPDS

SET

SET

NAVSOURCE

FORMAT RANGE

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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

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1 2

4 5

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6

7

8

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WIPER

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ON

PARKOFF



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FLOOR

NORM

PFD 1 EICAS

NAVSOURCE

FORMAT RANGE

BARO

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SPEED REFS

SEL

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SET

RST

SEL

ET

MODE

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INT

CHR

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FORMAT RANGE

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9

16

208

12

132013

18

13



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AIRCONDITIONINGSYSTEMOUTLET

AUDIO WARNING

FLIGHT BAGCOMPARTMENT

SOURCESELECTOR/ISOLATIONVALVES

SELECTORVALVE CLOSED

MACHTRANSDUCER

PITOT

SELECTORVALVE CLOSED

MACHTRANSDUCER

STATICNORMAL NORMAL

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS

HDPHMIC

<0019>

AUDIO WARNING

DATACONCENTRATORUNITAUDIO WARNINGDISABLE SWITCHES

OXYGEN MASKREGULATORSTORAGECOMPARTMENT

COPILOTHAT HOOK

AA

B

B

C

C


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OBSERVER’SHEADSETHOOK

OBSERVER’S STATIONRIGHT HAND SIDE

OBSERVER’SSEAT

OBSERVER’S STATIONLEFT HAND SIDE

OBSERVER’SJACK PANEL

OBSERVER’SOXYGENMASK/REGULATORSTORAGEUNIT


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STABILIZER TRIMDISCONNECTSWITCH (RED)

INTERCOM/RADIO TRANSMITSWITCH (BLACK)

STABILIZER TRIMLEVER SWITCHES(BLACK)

AUTOPILOT/STICKPUSHER DISCONNECTSWITCH (RED)

FLIGHT DIRECTORSYNC CONTROLSWITCH (BLACK)

PILOT’S CONTROL WHEEL(COPILOT’S OPPOSITE)

REAR VIEW

TOP VIEW

B

A

B

A


1. �� <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:

� Slide latch

� Deadbolt assembly

� Two quick--release hinge pins

� Viewer

� Decompression panel and latch

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

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

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

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

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

A. Emergency Operation

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

(1) Unlock and lift the lower hinge pin

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

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

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


CAUTION

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

NOTE

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


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HINGE ASSEMBLY

COCKPIT DOOR

HINGE ASSEMBLY

UPPERDECOMPRESSIONPANEL

SLIDELATCH

DEADBOLTASSEMBLY

VIEWER(PEEPHOLEASSEMBLY)

POCKETENCLOSURE

A

AB


9�� 7�� !" +! "- �� $

B

PRESSURERELEASELATCH

UPPER HINGEHANDLE

RETRACTABLEBOLTS

SLIDELATCH

DEADBOLT

NAMEPLATE

STRAPHANDLE

STRAPHANDLE

UPPER HINGEHANDLE


canadair regional jet 100/200 - aircraft general · minimum control speed with the critical engine...

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