[fltsim.0] title=FSP KLM 767-300 GE sim=Boeing767-300 model=v2GE panel= sound= texture=klm atc_id=PH-BZM atc_airline=KLM atc_flight_number= atc_heavy=1 ui_manufacturer=AI_Plane ui_type=767-300 GE ui_variation=KLM description=REPAINT:Peefunk(http://qnh2993.hp.infoseek.co.jp/) FD:Hiro [General] visual_damage=0 // 0=off, 1=on atc_type=BOEING atc_model=B763 editable=0 performance=Cruise Speed\tMach .84\nMaximum Range\t5,600 nm\nService Ceiling\t36,400 ft\nMax Takeoff Weight\t580,000 lb\nSeating\t\t368 to 550\nCargo Capacity\t7,552 CU ft\n [WEIGHT_AND_BALANCE] max_gross_weight=660000 // (pounds) empty_weight=281680 // (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=18000000 empty_weight_roll_MOI=5500000 empty_weight_yaw_MOI=16300000 empty_weight_coupled_MOI=0.0 [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 [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=1 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=13.0 //Def=113.0 Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=84000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.00 [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, 87.42, 0.00, -18.00, 1181.1, 0, 4.521, 90.0, 1.63, 2.5, 0.7235, 4.0, 4.0, 0, 0.0, 0.0 point.1=1, -19.50, -12.00, -18.50, 1574.8, 1, 4.521, 0.0, 1.91, 2.5, 0.7470, 6.9, 6.9, 2, 0.0, 0.0 point.2=1, -19.50, 12.00, -18.50, 1574.8, 2, 4.521, 0.0, 1.91, 2.5, 0.7470, 7.1, 7.1, 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=0.10 static_cg_height=17.56 [Views] eyepoint=90.0, -2.65, 8.6 [flaps.0] 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=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.55 drag_scalar=0.55 pitch_scalar=0.55 system_type=1 //Hydraulic [flaps.1] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=23 // 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=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.35 drag_scalar=0.35 pitch_scalar=0.35 system_type=1 //Hydraulic [flaps.2] type=2 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=4 // 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=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.05 drag_scalar=0.05 pitch_scalar=0.05 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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -28.22,-73.62, 0.33, fx_navredh , light.1 = 3, -28.22, 73.62, 0.33, fx_navgreh , light.2 = 3, -28.22,-73.62, 0.33, fx_navwhih , light.3 = 3, -28.22, 73.62, 0.33, fx_navwhih , light.4 = 2, -31.00,-73.60, 0.38, fx_strobeh , light.5 = 2, -31.00, 73.60, 0.38, fx_strobeh , light.6 = 1, 32.00, 0.00, 7.00, fx_beaconb , light.7 = 1, 32.00, 0.00, 7.00, fx_beaconb , light.8 = 1, 8.00, 0.00, -11.00, fx_beaconh , light.9 = 1, 8.00, 0.00, -11.00, fx_beaconh , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] Center1=0.0, 0.0, -4.0, 12400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-7.0, -35.0, 0.0, 16400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-7.0, 35.0, 0.0, 16400.0, 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 [airplane_geometry] wing_area=4605.0 //Square feet wing_span=200.0 //Feet wing_root_chord=23.0 //Feet wing_dihedral=6.2 //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=1090.0 //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=40.0 //Degrees, horizontal tail leading edge vtail_area=573.0 //Square feet vtail_span=27.3 //Feet, tip to body vtail_sweep=35.0 //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=137.0 //Square feet aileron_area=68.0 //Square feet rudder_area=232.0 //Square feet elevator_up_limit=15.0 //Degrees elevator_down_limit=30.0 //Degrees aileron_up_limit=30.0 //Degrees aileron_down_limit=15.0 //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=322.0 //Knots True (KTAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. [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
