[fltsim.0]title=EMB120 Delta Connectionsim=EMB120model=panel=sound=texture=daldxtkb_checklists=description=Embraer EMB120 model by Erick Cantu. Paint by Steve Drabekui_manufacturer=Embraer-Cantuui_type=EMB120ui_variation=Delta Connectionatc_airline=atc_id=atc_flight_number=atc_heavy=0atc_id_color=0x00000000atc_id_font=Verdana,-11,1,600,0visual_damage=1atc_parking_types=RAMP[fltsim.1]title=EMB120 embraer_housesim=EMB120model=panel=sound=texture=embraer_housekb_checklists=description=Embraer EMB120 model by Erick Cantu. Paint by Daniel Halpernui_manufacturer=Embraer-Cantuui_type=EMB120ui_variation=embraer_houseatc_airline=atc_id=atc_flight_number=atc_heavy=0atc_id_color=0x00000000atc_id_font=Verdana,-11,1,600,0visual_damage=1atc_parking_types=RAMP[General]atc_type=Embraeratc_model=editable=0performance="Cruise Speed\t\n315 kts 363 mph 583 km\/h\n\nEngines\t\nPratt & Whitney PT6A-60A 1,050 shp\n\nMaximum Range\t\n1,765 nm 2,031 m\t 3,269 km\n\nService Ceiling\t\n35,000 ft 10,668 m\n\nFuel Capacity\t\n539 U.S. gal 2,040 L\n\nMaximum Takeoff Weight \n15,000 lb\t 6,818 kg\n\nLength\t\n46.7 ft\t 14.23 m\n\nWingspan\t\n57.9 ft\t 17.65 m\n\nHeight\t\n14.3 ft\t 4.36 m\n\nSeating\t\nUp to 11\n\nUseful Load\t\n5,910 lb\t 2,681 kg"[WEIGHT_AND_BALANCE]max_gross_weight = 15000 // (pounds)empty_weight = 9090 // (pounds)reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations = 50station_load.0 = "170, 5.0, -2.0, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.1 = "170, 5.0, 2.0, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.2 = "170, -2.1, -2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.3 = "170, -2.1, 2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.4 = "170, -5.3, -2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.5 = "170, -5.3, 2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet);Moments of Inertiaempty_weight_pitch_MOI = 30000empty_weight_roll_MOI = 18200empty_weight_yaw_MOI = 36500empty_weight_coupled_MOI= 0.0[flight_tuning]cruise_lift_scalar = 1.0parasite_drag_scalar = 1.0induced_drag_scalar = 1.0elevator_effectiveness = 1.0aileron_effectiveness = 1.0rudder_effectiveness = 1.0pitch_stability = 1.0roll_stability = 1.0yaw_stability = 1.0elevator_trim_effectiveness = 1.0aileron_trim_effectiveness = 1.0rudder_trim_effectiveness = 1.0[GeneralEngineData]engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0 = -8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.1 = -8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar = 1.0 //Scalar for fuel flow efficiencymin_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser[propeller]thrust_scalar = 1.0 //Propeller thrust scalarpropeller_type = 0 //0=Constant Speed, 1=Fixed Pitchpropeller_diameter = 8.8 //Propeller Diameter, (feet)propeller_blades = 4 //Number of propeller bladespropeller_moi = 24 //Propeller moment of inertiabeta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)beta_min = 15.2 //Minimum blade pitch angle for constant speed prop, (degrees)min_gov_rpm = 25520 //Miminum governed RPMprop_tc = 0.004 //Prop time-constantgear_reduction_ratio = 17.6 //Propeller gear reduction ratiofixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees)low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUEprop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUEprop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUEprop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUEmin_rpm_for_feather = 700 //Minimum RPM for prop featheringbeta_feather = 79.3 //Feathering pitch angle (degrees)power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propellerdefeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUEminimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees)minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees)[TurbineEngineData]fuel_flow_gain = 0.011 //Gain on fuel flowinlet_area = 1.0 //Square Feet, engine nacelle inlet arearated_N2_rpm = 29920 //RPM, second stage compressor rated valuestatic_thrust = 158 //Lbs, max rated static thrust at Sea Level[turboprop_engine]power_scalar = 1.0 //Scalar on Turboprop powermaximum_torque = 3270 //Maximum torque available (ft-lbs)[electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)flap_motor = 0, 5 , 17.0gear_motor = 0, 5 , 17.0autopilot = 0, 5 , 17.0avionics_bus = 0, 5 , 17.0avionics = 1, 5 , 17.0pitot_heat = 0, 2 , 17.0additional_system = 0, 2 , 17.0marker_beacon = 1, 2 , 17.0gear_warning = 0, 2 , 17.0fuel_pump = 0, 5 , 17.0starter1 = 0, 20, 17.0light_nav = 0, 5 , 17.0light_beacon = 0, 5 , 17.0light_landing = 0, 5 , 17.0light_taxi = 0, 5 , 17.0light_strobe = 0, 5 , 17.0light_panel = 0, 5 , 17.0 //0 Class //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, 13.00, 0.00, -5.30, 1181, 0, 0.596, 39.9, 0.296, 1.581, 0.9516, 4.8, 4.8, 0, 184.0, 184.0point.1=1, -1.67, -8.58, -5.9, 1574, 1, 0.596, 0.0, 0.642, 1.581, 0.8152, 4.5, 5.2, 2, 184.0, 184.0point.2=1, -1.67, 8.58, -5.9, 1574, 2, 0.596, 0.0, 0.642, 1.581, 0.8152, 4.8, 4.9, 3, 184.0, 184.0point.3=2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0point.4=2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0point.5=2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0point.6=2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0static_pitch = -1.0static_cg_height = 4.3gear_system_type=1 //Hydraulic[gear_warning_system]gear_warning_available = 1 //Normalpct_throttle_limit = 0.1 //Percent throttle that activates warningflap_limit_idle = 15.0 //Flap angle that activates warning at idleflap_limit_power = 30.0 //Flap angle that activates warning at above idle[brakes]parking_brake = 1 //Parking brake availabletoe_brakes_scale = 1.0 //Brake scalar[hydraulic_system]normal_pressure = 3000.0 //PSIelectric_pumps = 0 //no electric pumpsengine_map = 1,1,0,0 //pumps on Eng1,2[Views]eyepoint = 4.54, -1.20, 3.25[flaps.0]type = 1 // 1 - tail, 2 - leadspan-outboard = 0.5 // 0.0 .. 1.0extending-time = 5 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 20 // degreesflaps-position.2 = 40 // degreesdamaging-speed = 250 // KIASblowout-speed = 300 // KIAS[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 0Com.2 = 1, 0Nav.1 = 1, 0, 1Nav.2 = 1, 0, 0Adf.1 = 1Transponder.1 = 1Marker.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, 250aileron = 150, 250rudder = 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 = 4direction_indicator.0=3,0[attitude_indicators]//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyroattitude_indicator.0 = 1 [turn_indicators]//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyroturn_indicator.0=1,0[LIGHTS]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpitlight.0 = 3, 0.90, -32.00, 2.90, fx_navred ,light.1 = 3, 0.90, 32.00, 2.90, fx_navgre ,light.2 = 3, -39.80, 0.00, 16.00, fx_navwhi ,light.3 = 2, 0.70, -32.00, 2.90, fx_strobe ,light.4 = 2, 0.70, 32.00, 2.90, fx_strobe ,light.5 = 1, 0.00, 0.00, 7.0, fx_beacon ,light.6 = 2, -4.55, 0.00, -1.85, fx_strobe ,light.7 = 4, 4.91, 0.00, 1.64, fx_vclight,[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn_s, 1[fuel]LeftMain = 0.0, -14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)LeftAux = 0.0, -6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightMain = 0.0, 14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightAux = 0.0, 6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors = 1 electric_pump=1[airplane_geometry]wing_area = 310.0 //Square feetwing_span = 57.2 //Feetwing_root_chord = 5.4 //Feetwing_dihedral = 6.0 //Degreeswing_incidence = 1.0 //Degreeswing_twist = -1.5 //Degreesoswald_efficiency_factor= 0.7 //Measure of lift effeciency of wingwing_winglets_flag = 1 //Are winglets available?wing_sweep = 1.0 //Degrees, wing leading edgewing_pos_apex_lon = 2.1 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_area = 67.0 //Square feethtail_span = 17.2 //Feethtail_pos_lon = -22.6 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_incidence = 0.5 //Degreeshtail_sweep = 20.0 //Degrees, horizontal tail leading edgevtail_area = 42.0 //Square feetvtail_span = 7.4 //Feet, tip to bodyvtail_sweep = 40.0 //Degrees, vertical tail leading edgevtail_pos_lon = -20.5 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going upelevator_area = 17.0 //Square feetaileron_area = 13.5 //Square feetrudder_area = 7.3 //Square feetelevator_up_limit = 17.0 //Degreeselevator_down_limit = 15.5 //Degreesaileron_up_limit = 18.0 //Degreesaileron_down_limit = 18.0 //Degreesrudder_limit = 30.0 //Degreeselevator_trim_limit = 15.0 //Degreesspoiler_limit = 60.0 //Degreesspoilerons_available = 0 //Spoilerons Available?aileron_to_spoileron_gain = 0 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 0 //Degreesmin_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate[Reference Speeds]flaps_up_stall_speed = 96.0 //Knots True (KTAS)full_flaps_stall_speed = 76.8 //Knots True (KTAS)cruise_speed = 300.0 //Knots True (KTAS)max_mach = 0.58max_indicated_speed = 263 //Red line (KIAS)[autopilot]autopilot_available= 1flight_director_available= 1default_vertical_speed= 1800.0autothrottle_available= 0pitch_takeoff_ga=8.0max_pitch=10.0max_pitch_acceleration=1.0max_pitch_velocity_lo_alt=2.0max_pitch_velocity_hi_alt=1.5max_pitch_velocity_lo_alt_breakpoint=20000.0max_pitch_velocity_hi_alt_breakpoint=28000.0max_bank=25.0max_bank_acceleration=1.8max_bank_velocity=3.00max_throttle_rate=0.10nav_proportional_control=9.00nav_integrator_control=0.25nav_derivative_control=0.00nav_integrator_boundary=2.50nav_derivative_boundary=0.00gs_proportional_control=9.52gs_integrator_control=0.26gs_derivative_control=0.00gs_integrator_boundary=0.70gs_derivative_boundary=0.00yaw_damper_gain = 1.0[forcefeedback]stick_shaker_magnitude=5000 ; 0 - 10000stick_shaker_direction=0 ; 0 - 35999 degreesstick_shaker_period=111111 ; in microsecondsgear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=9000 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=27000 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[stall_warning]type=2[exits]number_of_exits=2exit_rate.0=0.4 ;Percent per secondexit_rate.1=0.4 ;Percent per second[TailHook] //landing lights (normally shift+T)tailhook_length= 4tailhook_position= 0.0, 0.0, 0.0cable_force_adjust= 0.5[folding_wings] //Airstairs (normally shift+F)wing_fold_system_type= 4fold_rates= 0.110,0.110