; Localized 09/12/2006 03:16 AM (GMT) 4:4.2.169 aircraft.cfg [fltsim.0] title=Bombardier CRJ-700 Lufthansa CityLine sim=Bombardier_CRJ_700 model="" panel="" sound="" texture=lufthansa CityLine kb_checklists=BombardierCRJ700_check kb_reference=BombardierCRJ700_ref atc_id=Hansaline100 atc_airline=lufthansa CityLine atc_parking_types=GATE,RAMP ui_manufacturer=Bombardier ui_type=CRJ-700 ui_variation=Lufthansa CityLine ui_typerole=Regionaljet ui_createdby=Microsoft Corporation description=Die CRJ-Familie (Canadair Regional Jet) ist eine Weiterentwicklung des Canadair Challenge-Businessjets, der als LearStar 600 seinen Dienst erstmalig aufnahm. Der Bombardier Canadair CRJ700 wurde 2001 in Betrieb genommen und ist eine längere Version des CRJ100/200-Regionaljets, bei der die Sitzkapazität von 50 auf 70 erhöht wurde. Zusätzlich zu dem verlängerten Rumpf und dem verbesserten Fahrwerk hat der CRJ700 eine größere Tragflächenspannweite und Vorflügel an der Tragflächenvorderseite. Wie die anderen Modelle der CRJ-Familie verfügt der CRJ700 über ein EFIS-Avioniksystem (elektronisches Fluginformationssystem) und "Glascockpit"-Instrumente. [General] atc_type=BOMBARDIER atc_model=CRJ700 editable=0 performance=Reisegeschwindigkeit\n0,78 Mach 515 Meilen pro Stunde 829 km\/h\n\nTriebwerkoptionen\nGeneral Electric CF34-8C1 Mantelstromtriebwerke mit 12.670 Lbs Schub\n\nMaximale Reichweite\n1.702 nm 3.152 km\n\nDienstgipfelhöhe\n41.000 Fuß 12.497 m\n\nTreibstoffmenge\n3.036 Gallonen 11.488 l\n\nLeergewicht\n43.200 Lbs 19.595 kg\n\nMaximales Bruttogewicht \n72.500 Lbs 32.885 kg\n\nLänge\n106 Fuß 8 Zoll 32,5 m\n\nSpannweite\n76 Fuß 3 Zoll 23,2 m\n\nHöhe\n24 Fuß 10 Zoll 7,6 m\n\nSitzplätze\n70\n\nZuladung\n18.800 Lbs 8.527 kg Category=airplane [CameraDefinition.0] Title=Fahrwerk Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description=Ansicht des Fahrwerks und der Innenklappen der linken Tragfläche Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=.52 ShowWeather=Yes InitialXyz=-2.2, -1.2, -7 InitialPbh=0, 0, 13 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title=Heck Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c} Description=Ansicht nach vorn von einer Position hinter dem Luftfahrzeug Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=.75 ShowWeather=Yes InitialXyz=0, 3, -35.0 InitialPbh=5, 0, 0 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.2] Title=Rechte Tragfläche Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59} Description=Ansicht von der rechten Tragflächenspitze in Richtung Cockpit Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.5 ShowWeather=Yes InitialXyz=25.8, 1.6, 0.0 InitialPbh=6, 0, 280 XyzAdjust=TRUE Category=Aircraft MomentumEffect=FALSE ClipMode=Minimum [CameraDefinition.3] Title=Linke Tragfläche Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description=Ansicht von der linken Tragflächenspitze in Richtung Cockpit Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.5 ShowWeather=Yes InitialXyz=-25.8, 1.6, 0.0 InitialPbh=6, 0, 80 XyzAdjust=TRUE Category=Aircraft MomentumEffect=No ClipMode=Minimum [CameraDefinition.001] Title=Rechter Sitz Guid={8ff6c134-098d-409f-baec-caba3f683f98} Origin=Virtual Cockpit MomentumEffect=YES SnapPbhAdjust=Swivel SnapPbhReturn=False PanPbhAdjust=Swivel PanPbhReturn=False Track=None ShowAxis=YES AllowZoom=TRUE InitialZoom=.6 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=1.1, 0.0, 0.0 InitialPbh=2, 0, 0 [CameraDefinition.002] Title=Mittlere Konsole Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin=Virtual Cockpit MomentumEffect=No SnapPbhAdjust=None SnapPbhReturn=False PanPbhAdjust=None PanPbhReturn=False Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.8 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.54, 0.3, -0.05 InitialPbh=75, 0, 0 [CameraDefinition.003] Title=Triebwerkssteuerelemente Guid={a5741a54-ea6d-4580-9709-c99161e38a83} Origin=Virtual Cockpit MomentumEffect=No SnapPbhAdjust=None SnapPbhReturn=False PanPbhAdjust=None PanPbhReturn=False Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=1.0 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.54, 0.0, 0.28 InitialPbh=65.0, 0, 0 [CameraDefinition.004] Title=Oberes Instrumentenbrett Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe} Origin=Virtual Cockpit MomentumEffect=No SnapPbhAdjust=None SnapPbhReturn=False PanPbhAdjust=None PanPbhReturn=False Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.9 SmoothZoomTime=2.0 ZoomPanScalar=1.15 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.55, -0.58, -0.3 InitialPbh=-49.7, 0, 0 [WEIGHT_AND_BALANCE] max_gross_weight=74945.0 // (pounds) empty_weight=43500.0 // (pounds) reference_datum_position=49.7, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position=-50.0, 0, 7 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -8.67, -1.4, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -8.67, 1.4, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=11000, -62.0, 0.0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_name.0=Pilot station_name.1=Kopilot station_name.2=Passagiere ;Moments of Inertia empty_weight_pitch_MOI=413776 empty_weight_roll_MOI=188879 empty_weight_yaw_MOI=578254 empty_weight_coupled_MOI=0.0 [airplane_geometry] wing_area=738.7 //Square feet wing_span=76.25 //Feet wing_root_chord=17.3 //Feet wing_dihedral=0.0 //Degrees wing_incidence=1.5 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.8 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=27.0 //Degrees, wing leading edge wing_pos_apex_lon=-42.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=192.0 //Square feet htail_span=14.4 //Feet htail_pos_lon=-95.9 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=12.7 //Feet, vertical distance from reference point, positive going up htail_incidence=4.0 //Degrees htail_sweep=35.0 //Degrees, horizontal tail leading edge vtail_area=108.0 //Square feet vtail_span=11.6 //Feet, tip to body vtail_sweep=44.0 //Degrees, vertical tail leading edge vtail_pos_lon=-86.7 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=3.7 //Feet, vertical distance from reference point, positive going up elevator_area=42.1 //Square feet aileron_area=22.0 //Square feet rudder_area=21.4 //Square feet elevator_up_limit=28.0 //Degrees elevator_down_limit=20.0 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=18.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=60.0 //Degrees spoiler_extension_time=2.0 //Seconds spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=4.6 //Aileron to spoileron gain min_ailerons_for_spoilerons=5 //Degrees min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=1 positive_g_limit_flaps_up=3.0 //Design G load tolerance (positive, flaps up) positive_g_limit_flaps_down=2.0 //Design G load tolerance (positive, flaps down) negative_g_limit_flaps_up=-2.0 //Design G load tolerance (negative, flaps up) negative_g_limit_flaps_down=-2.0 //Design G load tolerance (negative, flaps down) load_safety_factor=1.5 //Design G load safety factor [Reference Speeds] flaps_up_stall_speed=112.0 //Knots True (KTAS) full_flaps_stall_speed=102.0 //Knots True (KTAS) cruise_speed=473.0 //Knots True (KTAS) max_mach=0.83 max_indicated_speed=335.0 //Red line (KIAS) [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [flaps.0] type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=8 // seconds flaps-position.0=0 // degrees flaps-position.1=20 // degrees flaps-position.2=20 // degrees flaps-position.3=25 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS [flaps.1] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=8 // degrees flaps-position.3=20 // degrees flaps-position.4=30 // degrees flaps-position.5=45 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-74.0, -7.5, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-74.0, 7.5, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain=0.0025 //Gain on fuel flow inlet_area=9.4 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=12670 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [fuel] Center1=-52.7, 0.0, -4.0, 688.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-54.3, -7.7, -3.5, 1118.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-54.3, 7.7, -3.5, 1118.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 ;/0 Class ;/1 Longitudinal Position (feet) ;/2 Lateral Position (feet) ;/3 Vertical Position (feet) ;/4 Impact Damage Threshold (Feet Per Minute) ;/5 Brake Map (0=None, 1=Left, 2=Right) ;/6 Wheel Radius (feet) ;/7 Steer Angle (degrees) ;/8 Static Compression (feet) (0 if rigid) ;/9 Max/Static Compression Ratio ;/10 Damping Ratio (0=Undamped, 1=Critically Damped) ;/11 Extension Time (seconds) ;/12 Retraction Time (seconds) ;/13 Sound Type [contact_points] point.0=1, -8.50, 0.00, -6.70, 1600, 0, 0.5625, 46.8, 0.80, 2.5, 0.55, 10.0, 10.0, 0, 260.0, 260.0 point.1=1, -56.50, -6.76, -8.60, 1600, 1, 1.0, 0.0, 0.90, 2.5, 0.65, 9.0, 9.0, 2, 260.0, 260.0 point.2=1, -56.50, 6.76, -8.60, 1600, 2, 1.0, 0.0, 0.90, 2.5, 0.65, 9.0, 9.0, 3, 260.0, 260.0 point.3=2, -65.00, -39.00, 0.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -65.00, 39.00, 0.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -43.00, 0.00, -3.80, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, -98.00, 0.00, 16.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.7=2, -8.00, 0.00, -2.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.8=2, -80.00, 0.00, -1.50, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=-1.8 static_cg_height=7.3 gear_system_type=1 //Hydraulic emergency_extension_type=2 //None=0,Pump=1,Gravity=2 [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=15.0 //Flap angle that activates warning at idle flap_limit_power=30.0 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=1.2 //Brake scalar auto_brakes=0 hydraulic_system_scalar=1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure [electrical] max_battery_voltage=24.0 generator_alternator_voltage=30.0 max_generator_alternator_amps=400.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 5 , 9.5 avionics=1, 5 , 9.5 additional_system=0, 2 , 9.5 marker_beacon=1, 2 , 9.0 fuel_pump=0, 5 , 9.0 [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=1 //no electric pumps engine_map=1,1,0,0 //pumps on Eng1,2 [vacuum_system] max_pressure=5.15 //PSI vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.0 //Scalar on heat effectiveness, 0 = not available [stall_warning] type=2 stick_shaker=1 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [direction_indicators] ;/1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another ;/2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [attitude_indicators] ;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=2 attitude_indicator.1=2 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [altimeters] altimeter.0=1 altimeter.1=1 [turn_indicators] ;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 turn_indicator.1=0,0 [Radios] ;/ Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=30,15 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=1.0 [Views] //eyepoint = -16.73, -1.65, 4.28 eyepoint=-11.1, -1.65, 4.28 [exits] number_of_exits=3 exit.0=0.4, -16.90, -4.5, 3.9, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.1=0.4, -74.00, -4.5, 0.5, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.2=0.4, -16.50, 4.5, 0.5, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) [LIGHTS] ;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -64.70, -37.00, -0.50, fx_navredm , light.1=3, -64.70, 37.00, -0.50, fx_navgrem , light.2=3, -104.63, 0.00, 14.30, fx_navwhi , light.3=1, -29.00, 0.00, -2.30, fx_beaconb , light.4=2, -104.63, 0.00, 15.00, fx_strobe , light.5=1, -32.50, 0.00, 7.00, fx_beaconh , light.6=4, -10.00, 0.00, 3.90, fx_vclighth, light.7=2, -64.50, -36.50, -0.50, fx_strobe , light.8=2, -64.50, 36.50, -0.50, fx_strobe , [keyboard_response] ;/Breakpoint speeds (knots) on the keyboard increments of control surfaces. ;/Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds