[fltsim.0] title=Boeing 777-200ER MR MKIII VIIR sim=Boeing777-200-MR-MKIII model= panel= sound= texture= ui_manufacturer=Boeing ui_type=777-200ER ui_variation=British Airways "Benyhone Tartan" atc_id=G-VIIR atc_airline=Speed Bird atc_flight_number=002 atc_heavy=1 description=MelJet Boeing 777-200ER for FS2002\nVersion 1.0, Release 1 (January 4, 2003)\n\nVisual model and FDE by Melvin Rafi\nhttp:\/\/www.meljet.com [General] atc_type=BOEING atc_model=B772 editable=0 performance=Flight Dynamic file Version 1.0 for FS2002\nEngine Thrust: 95000lbs each\nPowerplants: PW4090, Trent 895, GE90-94B\n\nThis Aircraft and the Flight Dynamic File are freeware and are not to be sold or transfered in any form for which a fee is charged. Free distribution is allowed only after approval from MelJet. [WEIGHT_AND_BALANCE] max_gross_weight = 656000 // (pounds) empty_weight = 301900 // (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 = 130000,0.000000,0.000000,0.000000 // Total Payload (pounds) ;Moments of Inertia empty_weight_pitch_MOI = 18000000 empty_weight_roll_MOI = 5500000 empty_weight_yaw_MOI = 16300000 empty_weight_coupled_MOI= 0.0 [airplane_geometry] wing_area = 4550.0 //Square feet wing_span = 199.9 //Feet wing_root_chord = 23.0 //Feet wing_dihedral = 7.0 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 32.0 //Degrees, wing leading edge wing_pos_apex_lon = 25.0 //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 = 1150.0 //Square feet htail_span = 70.7 //Feet htail_pos_lon = -100.0 //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 = 50.0 //Degrees, horizontal tail leading edge vtail_area = 585.0 //Square feet vtail_span = 34.3 //Feet, tip to body vtail_sweep = 45.0 //Degrees, vertical tail leading edge vtail_pos_lon = -108.3 //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 = 140.0 //Square feet aileron_area = 65.0 //Square feet rudder_area = 225.0 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 30.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 25.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 60.0 //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 = 150.0 //Knots True (KTAS) full_flaps_stall_speed = 120.0 //Knots True (KTAS) cruise_speed = 482.0 //Knots True (KTAS) [flaps.0] //Inboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.2 // 0.0 .. 1.0 extending-time = 25 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 250 // KIAS blowout-speed = 290 // KIAS lift_scalar = 0.65 drag_scalar = 0.60 pitch_scalar= 0.05 system_type = 1 //Hydraulic [flaps.1] //Outboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 25 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 250 // KIAS blowout-speed = 290 // KIAS lift_scalar = 0.40 drag_scalar = 0.40 pitch_scalar= 0.05 system_type = 1 //Hydraulic [flaps.2] //Inboard Leading Edge Slats type = 2 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0.5 // degrees flaps-position.2 = 0.5 // degrees flaps-position.3 = 0.5 // degrees flaps-position.4 = 0.5 // degrees flaps-position.5 = 1.0 // degrees flaps-position.6 = 1.0 // degrees damaging-speed = 250 // KIAS blowout-speed = 290 // KIAS lift_scalar = 0.10 drag_scalar = 0.05 pitch_scalar= 0.05 system_type = 1 //Hydraulic [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 [fuel] Center1 = 0.0, 0.0, -4.0, 26100.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -7.0, -35.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -7.0, 35.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1500.0 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 1 pitch_takeoff_ga = 8; [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 10.5, -32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 10.5, 32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.80 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 113.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 95000 //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 [Views] eyepoint = 90.0, -2.65, 2.25 [contact_points] //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) point.0=1, 87.42, 0.00, -17.50, 1181.1, 0, 3.500, 70.0, 1.0, 2.5, 0.7200, 15.0, 15.0, 0, 0.0, 0.0 point.1=1, -19.50, -12.00, -19.00, 1574.8, 1, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 2, 0.0, 0.0 point.2=1, -19.50, 12.00, -19.00, 1574.8, 2, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 3, 0.0, 0.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = 0 static_cg_height = 17.56 [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 [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 [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits = 1 exit_rate.0 = 0.1 ;Percent per second [TailHook] tailhook_length=1 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.075,0.075 ;Percent per second [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3,-102.25, 0.00, 6.25, fx_navwhih , light.1=2,-102.25, 0.00, 3.00, fx_strobeh , light.2=1, 39.00, 0.00, 10.50, fx_beaconh , light.3=1, 20.25, 0.00, -11.50, fx_beaconh , light.4=4, 93.50, 0.00, 5.50, fx_vclighth , light.5=5, 33.5, 21.0, -8.0, B777EL, light.6=5, 33.5, -21.0, -8.0, B777EL, //light.7=5, 98.0, 0.00, -11.00, b734_ll, smoke.0=-8.40,-28.00,-76.0, fx_jpv smoke.1=-8.40,-28.00,76.0, fx_jpv [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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [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