[fltsim.0] title=Boeing 737-400 Dolphin Air Promotion Tour 2003 sim=Boeing737-400 model= panel= sound= texture=dlppromo kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_id= atc_id_enable=0 atc_airline=Dolphin Air atc_flight_number=2003 ui_manufacturer=Boeing ui_type=737-400 ui_variation=Dolphin Air Promotion Tour 2003 description=Der Erstflug dieses Musters fand am 9. April 1967 statt. Seitdem ist die Boeing 737 in mittlerweile acht verschiedenen Versionen mit über 3.500 Bestellungen das meistverkaufte Passagierflugzeug der Welt. Die Version -400 ist seit Ende 1993 im Einsatz. Dolphin Air setzt die Boeing 737-400 seit Ende 1998 in der Passage auf vielen innerdeutschen und europäischen Kurzstrecken, aber auch für Umläufe der CARGO Sektion ein. Diese Maschine, der Dolphin Air "PromoJet", wird anlesslich des fuenften Betriebsjahrs der Airline fuer die FS Community freigegeben. [General] atc_type=BOEING atc_model=B734 editable=0 performance=Cruise Speed \n477 kts 550 mph 885 km\/h\n\nEngines \nCFM56-3C1\n\nMaximum Range \n2,059 nm 2,370 mi 3,810 km\n\nService Ceiling \n36, 089 ft 11,000 m\n\nFuel Capacity \n5,311 U.S. gal 20,104 L\n\nEmpty Weight-Standard \n76,180 lb 34,550 kg\n\nMaximum Takeoff Weight\n138,500 lb 62,800 kg\n\nLength \n120 ft 36.45 m\n\nWingspan \n94 ft, 9 in 25.9 m\n\nHeight \n36.5 ft 11.13 m\n\nSeating \nSeats 147 to 168\n\nCargo Capacity \n1,373 ft3 38.93 m3\n\n [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight=138325 // (pounds) empty_weight=102640 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI=3500000 empty_weight_roll_MOI=2262183 empty_weight_yaw_MOI=837024 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar=0.70 parasite_drag_scalar=0.20 induced_drag_scalar=1.10 ELEVATOR_EFFECTIVENESS=3.5 // ADJUST THIS VALUE TO MEET PITCHCRITERIA AILERON_EFFECTIVENESS=6.5 // ADJUST THIS VALUE TO MEET ROLLCRITERIA rudder_effectiveness=3.0 pitch_stability=2.0 roll_stability=1.5 yaw_stability=0.7 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=4.75, -16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=4.75, 16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.59 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=22000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=0.95 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0=1, 48.00, 0.00, -8.10, 1181.1, 0, 1.442, 90.99, 0.8, 2.5, 0.9, 5.0, 5.3, 0, 230.0, 320.0 // ADJUST THE 90.99 VALUE TO ALTER GROUNDSTEERING point.1=1, -7.75, -8.58, -8.68, 1574.8, 1, 1.442, 4.00, 1.0, 2.5, 0.9, 6.0, 8.3, 2, 230.0, 320.0 point.2=1, -7.75, 8.58, -8.68, 1574.8, 2, 1.442, 4.00, 1.0, 2.5, 0.9, 5.7, 8.1, 3, 230.0, 320.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 max_number_of_points=21 static_pitch=0.62 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.66 //feet, altitude of CG when at rest on the ground [Views] eyepoint=43.7, -1.31, 4 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=14 // seconds flaps-position.0=0 // degrees flaps-position.1=1 // degrees flaps-position.2=2 // degrees flaps-position.3=5 // degrees flaps-position.4=10 // degrees flaps-position.5=15 // degrees flaps-position.6=25 // degrees flaps-position.7=30 // degrees flaps-position.8=40 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=1.70 drag_scalar=-1.15 pitch_scalar=1.0 system_type=1 // Hydraulic [flaps.1] // Flaps 15 adjustment type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=10 // seconds flaps-position.3=0.0 // flaps-position.5=1.0 // flaps-position.7=0.0 // flaps-position.8=0.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=-6.00 drag_scalar=0.00 pitch_scalar=1.0 system_type=1 // Hydraulic [flaps.2] // Flaps 30 adjustment type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=3 // seconds flaps-position.3=0.0 // flaps-position.5=0.0 // flaps-position.7=1.0 // flaps-position.8=1.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=-15.00 drag_scalar=14.00 pitch_scalar=1.0 system_type=1 // Hydraulic [flaps.3] // Flaps 40 adjustment type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=3 // seconds flaps-position.3=0.0 // flaps-position.5=0.0 // flaps-position.7=0.0 // flaps-position.8=1.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=-2.00 drag_scalar=14.00 pitch_scalar=1.0 system_type=1 // Hydraulic [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 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -19.14, -47.24, 1.38, fx_navredm , light.1=3, -19.14, 47.24, 1.38, fx_navgrem , light.2=3, -64.32, 0.00, 4.92, fx_navwhih , light.3=2, -18.22, -47.08, 1.38, fx_strobeh , light.4=2, -18.22, 47.08, 1.38, fx_strobeh , light.5=2, -2.65, 0.00, -4.60, fx_beaconb , light.6=1, 2.20, 0.00, 8.30, fx_beaconh , light.7=4, 44.41, 0.00, 3.50, fx_vclight , [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 [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 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 use_no_default_bank=1 use_no_default_pitch=1 default_vertical_speed=800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=94 autothrottle_takeoff_ga=1 pitch_takeoff_ga=15; [fuel] Center1=0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-3, 19, 0, 1500, 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 [airplane_geometry] wing_area=1137.0 //Square feet wing_span=94.75 //Feet wing_root_chord=18.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=-0.5 //Degrees oswald_efficiency_factor=0.75 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=25.0 //Degrees, wing leading edge wing_pos_apex_lon=8.0 //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=338.0 //Square feet htail_span=41.7 //Feet htail_pos_lon=-35.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=224.0 //Square feet vtail_span=20.0 //Feet, tip to body vtail_sweep=35.0 //Degrees, vertical tail leading edge vtail_pos_lon=-35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=5.8 //Feet, vertical distance from reference point, positive going up elevator_area=70.5 //Square feet aileron_area=26.9 //Square feet rudder_area=56.2 //Square feet elevator_up_limit=22.5 //Degrees elevator_down_limit=11.5 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=20.0 //Degrees rudder_limit=26.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=7.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=156.0 //Knots True (KTAS) full_flaps_stall_speed=110.0 //Knots True (KTAS) cruise_speed=477.0 //Knots True (KTAS) [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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
