[fltsim.0] title=Boeing 777-200ER MJ Singapore sim=Boeing777-200-MR-MKIII model= panel= sound= texture= ui_manufacturer=Boeing ui_type=777-200ER ui_variation=Singapore Airlines atc_id=9V-SNL atc_airline=SINGAPORE atc_flight_number=516 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 AIRCRAFT atc_model=B772 editable=1 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. [GROUND_REACTION] MAX_STEERING_ANGLE=70 main_gear_static_compression=0.3 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.25 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=1.0 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [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 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.2 induced_drag_scalar = 1.2 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.1 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [jet_engine] thrust_scalar = 1.0 [WEIGHT_AND_BALANCE] //WHEN RECONFIGURING WEIGHT WITH PSS LOAD EDIT, MANUALLY RE-ENTER THE POSITIONS AS SHOWN BELOW! //THIS WEIGHT CONFIG REPRESENTS A REASONABLY FULL LOAD OF 270 PASS (FC=18, BC=46, EC=206) WITH BAGGAGE (16239 LBS) AND CARGO (20398 LBS) //MAX FUEL IS 225219 LBS AT TAKE OFF (96% WING TANKS-9195 GALS EACH,59% MAIN-15228 GALS, 33618 GALS TOTAL) //IT IS RECOMMENDED THAT YOU USE A DIFFERENT CONFIG FILE WHEN USING PSS LOADEDIT AND MANUALLY ENTER THE WEIGHT VALUES HERE empty_weight = 303864.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 //WEIGHT, POSITION FORE-AFT, PORT-STARBORD, ABOVE-BELOW REFERENCE DATUM station_load.0 = 450.000, 98.000, 0.000, 2.000 station_load.1 = 3000.000, 29.000, 0.000, -5.000 station_load.2 = 16239.000, -31.000, 0.000, -5.000 station_load.3 = 20398.000, 55.000, 0.000, -5.000 station_load.4 = 4320.000, 65.000, 0.000, 2.000 station_load.5 = 11040.000, 15.000, 0.000, 2.000 station_load.6 = 49440.000, -35.000, 0.000, 2.000 //TOTAL ZFW = 405301 empty_weight_roll_MOI= 18250000.000 empty_weight_pitch_MOI= 29000000.000 empty_weight_yaw_MOI= 10500000.000 empty_weight_coupled_MOI= 100.000 max_gross_weight= 711992.991 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [GeneralEngineData] engine_type = 1 Engine.0 = 24.000, -31.550, -9.500 Engine.1 = 24.000, 31.550, -9.500 fuel_flow_scalar = 0.950 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 120.000 rated_N2_rpm = 29920.000 static_thrust = 84000.000 afterburner_available = 0 reverser_available = 1 prop_anim_ratio=-1.76 [airplane_geometry] wing_area = 4605.000 wing_span = 198.250 wing_root_chord = 28.667 wing_dihedral = 5.999 wing_incidence = 1.000 wing_twist = -0.494 oswald_efficiency_factor= 0.611 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = 32.500 wing_pos_apex_vert = -3.500 htail_area = 1089.000 htail_span = 70.000 htail_pos_lon = -90.500 htail_pos_vert = 4.600 htail_incidence = 0.000 htail_sweep = 0.000 vtail_area = 572.000 vtail_span = 27.269 vtail_sweep = 0.000 vtail_pos_lon = -80.300 vtail_pos_vert = 10.800 elevator_area = 70.000 aileron_area = 26.800 rudder_area = 56.200 elevator_up_limit = 26.001 elevator_down_limit = 26.001 aileron_up_limit = 30.000 aileron_down_limit = 30.000 rudder_limit = 30.000 elevator_trim_limit = 30.000 spoiler_limit = 59.989 spoilerons_available = 1 aileron_to_spoileron_gain = 3.000 min_ailerons_for_spoilerons = 10.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 180.000 full_flaps_stall_speed = 120.000 cruise_speed = 560.000 [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= 1.000, 85.420, 0.000, -17.500, 1181.100, 0.000, 3.500, 70.000, 1.000, 2.500, 0.720, 15.000, 15.000, 0.000, 220.000, 472.656 point.1= 1.000, -5.500, -18.000, -19.000, 1574.800, 1.000, 4.167, 20.000, 1.000, 2.500, 0.750, 15.000, 15.000, 2.000, 220.000, 472.656 point.2= 1.000, -5.500, 18.000, -19.000, 1574.800, 2.000, 4.167, 20.000, 1.000, 2.500, 0.750, 15.000, 15.000, 3.000, 220.000, 472.656 point.3= 2.000, -31.170, -99.330, 5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -31.170, 99.330, 5.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -101.280, 0.000, 2.350, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 104.000, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch = 0.000 static_cg_height = 17.560 [electrical] //BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 pitot_heat = 0, 15, 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 starter3 = 0, 20, 17.0 starter4 = 0, 20, 17.0 auto_brakes = 0, 15, 17.0 hydraulic_pump = 0, 2, 17.0 fuel_transfer_pump = 0, 5, 17.0 max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 60.0 electric_always_available = 0 [pitot_static] vertical_speed_time_constant=99 [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 [Views] eyepoint =97.5, -2.00, 2.25 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3,-102.70, 0.00, 6.50, fx_navwhih , //aft fuselage nav light light.1 = 2,-102.70, 0.00, 6.50, fx_strobeh , //aft fuselage strobe light.2 = 1, 39.00, 0.00, 10.50, fx_beaconh , //upper beacon light.3 = 1, 20.25, 0.00, -11.50, fx_beaconb , //lower beacon light.4 = 4, 96.30, 0.00, 3.00, fx_vclighth , //cockpit light splash light.5 = 5, 53.25, -9.65, -3.55, fx_navwhih , //wing-engine light located on fuselage ls light.6 = 5, 53.25, 9.65, -3.55, fx_navwhih , //wing-engine light located on fuselage rs light.7 = 5, 40.55, 23.60, -7.50, fx_fxwing.fx, //wing and engine light splash effect rs light.8 = 5, 40.50, -23.50, -7.50, fx_fxwing.fx, //wing and engine light splash effect ls light.9 = 3, -88.00, -15.00, 5.40, fx_navwhi , //simulated tail light mounted on left horizontal stabilizer light.10 = 3, -88.00, 15.00, 5.40, fx_navwhi , //simulated tail light mounted on right horizontal stabilizer light.11 = 6, 97.0, 0.00, -10.0, MJ772TL , //nose gear light splash [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 [fuel] Center1 = 0.000, 0.000, -3.000, 26100.000, 3.000 LeftMain = 2.000, -35.000, 0.000, 9580.000, 2.400 RightMain = 2.000, 35.000, 0.000, 9580.000, 2.400 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=1200.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=99 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8.0 use_no_default_pitch=1 use_no_default_bank=1 [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, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 28.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 0.500 flaps-position.0= 0.000, 0.000 flaps-position.1= 6.665, 0.000 flaps-position.2= 13.331, 0.000 flaps-position.3= 19.996, 0.000 flaps-position.4= 26.662, 0.000 flaps-position.5= 33.327, 0.000 flaps-position.6= 39.992, 0.000 [Flaps.1] type= 1 span-outboard= 0.500 extending-time= 28.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 0.500 flaps-position.0= 0.000, 0.000 flaps-position.1= 6.665, 0.000 flaps-position.2= 13.331, 0.000 flaps-position.3= 19.996, 0.000 flaps-position.4= 26.662, 0.000 flaps-position.5= 33.327, 0.000 flaps-position.6= 39.992, 0.000 [Flaps.2] type= 2 span-outboard= 0.500 extending-time= 5.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 0.200 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000