[fltsim.0] title=AIA EMB120 Big Sky sim=aia_emb_120 visual_damage=1 model=reflective panel= sound= texture=bigsky kb_checklists= kb_reference= atc_id=N285AS atc_airline=Big Sky atc_flight_number=118 ui_manufacturer=Embraer ui_type=EMB-120 ui_variation=Big Sky description=AI Aardvark EMB-120 Big Sky atc_id_color=0000000000 visual_damage=0 [General] atc_type=EMBRAER atc_model=E120 editable=0 performance=Max Cruise Speed\t315 kts\nMaximum Range\t1,894 nm\nService Ceiling\t35,000 ft\nMax Gross Weight\t15,000 lb\nSeating\t\tUp to 11\nUseful Load\t5,810 lb\n [weight_and_balance] // ACM V1.0 pl4 max_gross_weight = 12000 empty_weight = 9090 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 30000 empty_weight_roll_MOI = 18200 empty_weight_yaw_MOI = 36500 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = 170, 5.0, -2.0, 0.0 station_load.1 = 170, 5.0, 2.0, 0.0 station_load.2 = 170, -2.1, -2.0, 0.0 station_load.3 = 170, -2.1, 2.0, 0.0 station_load.4 = 170, -5.3, -2.0, 0.0 station_load.5 = 170, -5.3, 2.0, 0.0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.8 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=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.8 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=24 //Propeller moment of inertia beta_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 RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.6 //Propeller gear reduction ratio fixed_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=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=79.3 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_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 flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=158 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=2570 //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 , 17.0 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] static_pitch = 0.5 static_cg_height = 5.9 max_number_of_points = 7 point.0 = 1, 22.9279, 0, -5.2, 1181, 0, 0.596, 60, 0.2, 2.5, 0.9516, 4.8, 4.8, 0, 0, 0 point.1 = 1, -1.67, -8.58, -5.9, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 0.0, 0.0 point.2 = 1, -1.67, 8.58, -5.9, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 0.0, 0.0 point.3 = 2, -1.3214, -32.1767, 2.3511, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -1.3214, 32.1767, 2.3511, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -30.7277, 0, 4.3792, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 30.1408, 0, -0.3859, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [Views] eyepoint=4.54, -1.20, 3.25 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=20 // degrees flaps-position.2=40 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.90 drag_scalar=0.70 pitch_scalar=0.70 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 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, 2.7, -31.48, 2.48, fx_navred light.1 = 3, 2.70, 31.48, 2.48, fx_navgre light.2 = 3, -34.67, 0.01, 14.01, fx_navwhi light.3 = 2, 2.86, -31.29, 2.46, fx_strobe light.4 = 2, 2.86, 31.29, 2.46, fx_strobe light.5 = 1, -0.03, 0.01, 6.27, fx_beacon light.6 = 1, 2.98, 0, -1.91, fx_beacon [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 LeftMain = 0, -14.5, -1, 190, 0 LeftAux = 0, -6, -1.5, 79.5, 0 RightMain = 0, 14.5, -1, 190, 0 RightAux = 0, 6, -1.5, 79.5, 0 [airplane_geometry] wing_area=310.0 //Square feet wing_span=57.2 //Feet wing_root_chord=5.4 //Feet wing_dihedral=6.0 //Degrees wing_incidence=1.0 //Degrees wing_twist=-1.5 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=1.0 //Degrees, wing leading edge wing_pos_apex_lon=2.1 //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=67.0 //Square feet htail_span=17.2 //Feet htail_pos_lon=-22.6 //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=0.5 //Degrees htail_sweep=20.0 //Degrees, horizontal tail leading edge vtail_area=42.0 //Square feet vtail_span=7.4 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-20.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=4.1 //Feet, vertical distance from reference point, positive going up elevator_area=17.0 //Square feet aileron_area=13.5 //Square feet rudder_area=7.3 //Square feet elevator_up_limit=17.0 //Degrees elevator_down_limit=15.5 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=18.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=00.0 //Degrees 60 spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=92.0 //Knots True (KTAS) full_flaps_stall_speed=72.0 //Knots True (KTAS) cruise_speed=265.0 //Knots True (KTAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 pitch_takeoff_ga=8.000000 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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
