[fltsim.0] title=777-200 sim=Boeing777 model=200 panel= sound= texture=200_domestic ui_manufacturer=Lynx Airways Worldwide ui_type=777-200 Passenger ui_variation=Domestic/International atc_id=L0183D atc_airline=Lynx Airways atc_flight_number=LYX atc_heavy=1 description=MelJet Boeing 777-200LR model and FDE by Melvin Rafi http:www.meljet.com. Repaint was completed by our very own Media Division Officer, Yoshi. Lynx Airways Worldwide has been given permission by MelJet to repaint their aircraft. We at Lynx thank MelJet, their staff, and designers for the oportunity to fly their aircraft as part of our fleet. [fltsim.1] title=777-300 sim=Boeing777 model=300 panel= sound= texture=300_domestic ui_manufacturer=Lynx Airways Worldwide ui_type=777-300 Passenger ui_variation=Domestic/International atc_id=L05113D atc_airline=Lynx Airways atc_flight_number=LYX atc_heavy=1 description=MelJet Boeing 777-300LR model and FDE by Melvin Rafi http:www.meljet.com. Repaint was completed by our very own Media Division Officer, Yoshi. Lynx Airways Worldwide has been given permission by MelJet to repaint their aircraft. We at Lynx thank MelJet, their staff, and designers for the oportunity to fly their aircraft as part of our fleet. [General] atc_type=BOEING atc_model=B772 editable=0 performance=Flight Dynamic file Version 1.5 for FS2002\nEngine Thrust: 110100lbs each\nPowerplant: GE90-110B1\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 = 766000 // (pounds) empty_weight = 320000 // (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 = 100000,0.000000,0.000000,0.000000 // 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 = 4600.0 //Square feet wing_span = 212.9 //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 = 1 //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] //This configuration will give 51590 US Gallons (approximately 345653lbs) of 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, 12745.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -7.0, 35.0, 0.0, 12745.0, 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 = 0.75 //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 = 110100 //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 = 2 exit_rate.0 = 0.1 ;Percent per second exit_rate.1 = 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 , [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