[fltsim.0] title=EMB120 British Airways sim=aia_emb_120 model=no_refl panel= sound= texture=BAW atc_id= atc_airline=British atc_flight_number=1258 ui_manufacturer=AI ui_type=Embraer EMB-120 ui_variation=British Airways atc_id_color=0000000000 visual_damage=0 [fltsim.1] title=EMB120 KLM sim=aia_emb_120 model=no_refl panel= sound= texture=KLM atc_id= atc_airline=KLM atc_flight_number=2151 ui_manufacturer=AI ui_type=Embraer EMB-120 ui_variation=KLM atc_id_color=0000000000 visual_damage=0 [General] atc_type=EMBRAER atc_model=C120 editable=0 performance="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] // ACM V2.3 max_gross_weight = 15000 empty_weight = 9090 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 3, 0, -.5 empty_weight_pitch_MOI = 50000 empty_weight_roll_MOI = 36200 empty_weight_yaw_MOI = 36500 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = 0, 10.4, -2, 0 station_load.1 = "170, 5.0, 2.0, 0.0, Co-Pilot" station_load.2 = "170, -2.1, -2.0, 0.0, Passenger" station_load.3 = "170, -2.1, 2.0, 0.0, Passenger" station_load.4 = "170, -5.3, -2.0, 0.0, Passenger" station_load.5 = "170, -5.3, 2.0, 0.0, Passenger" [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 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 1.0 engine.0 = 5.77, -10.81, 1.19, engine.1 = 5.77, 10.81, 1.19, min_throttle_limit=-0.150000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 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 electric_pump=0 [contact_points] static_pitch = -0.6 static_cg_height = 5.35 max_number_of_points = 7 point.0 = 1, 25.6686, 0, -5.3755, 1181, 0, 0.596, 39.9, 0.296, 2.5, 0.9516, 4.8, 4.8, 0, 184, 184 point.1 = 1, -0.6458, -11, -5.6547, 1574, 1, 0.596, 0, 0.3, 2.5, 0.8152, 4.5, 5.2, 2, 184, 184 point.2 = 1, -0.6458, 11, -5.6547, 1574, 2, 0.596, 0, 0.3, 2.5, 0.8152, 4.8, 4.9, 3, 184, 184 point.3 = 2, -0.6559, -32.4787, 2.4014, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -0.6559, 32.4787, 2.4014, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -30.1391, 0, 3.9616, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 29.9752, 0, -0.3843, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 9000 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 27000 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,1.6459,0.9685,0.9685,0.0168,1.5805,1.9371,1.9371 //ACM_AREAW2// 0.0337,1.5151,2.9056,2.9056,0.0507,1.4496,3.8743,3.8743,0.0675,1.3842 //ACM_AREAW3// 4.8428,4.8428,0.0844,1.3188,5.8115,5.8115,0.1014,1.2534,6.7800,6.7800 //ACM_AREAW4// 0.1182,1.1880,7.7486,7.7486,0.1351,1.1227,8.7172,8.7172,0.1520,1.0573 //ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1059,1.7661,0.5824,0.5824 //ACM_AREAH2// 0.2119,1.7847,0.8737,0.8737,0.3179,1.8034,1.1649,1.1649,0.4239,1.8220 //ACM_AREAH3// 1.4562,1.4562,0.5299,1.8406,1.7474,1.7474,0.6359,1.8593,2.0387,2.0387 //ACM_AREAH4// 0.7419,1.8779,2.3299,2.3299,0.8479,1.8964,2.6212,2.6212,0.9539,1.9151 //ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.2101,2.2853,0.5012,0.5012 //ACM_AREAV2// 0.4205,2.3152,0.7518,0.7518,0.6308,2.3450,1.0024,1.0024,0.8410,2.3749 //ACM_AREAV3// 1.2530,1.2530,1.0513,2.4047,1.5036,1.5036,1.2617,2.4346,1.7541,1.7541 //ACM_AREAV4// 1.4720,2.4644,2.0048,2.0048,1.6822,2.4942,2.2555,2.2555,1.8926,2.5241 //ACM_CAREAW1// 4.3586,4.3586,0.8989,1.2281,4.8428,4.8428,0.9074,1.2201,5.3271,5.3271 //ACM_CAREAW2// 0.9158,1.2122,5.8115,5.8115,0.9243,1.2042,6.2958,6.2958,0.9327,1.1962 //ACM_CAREAW3// 6.7800,6.7800,0.9412,1.1880,7.2644,7.2644,0.9496,1.1800,7.7486,7.7486 //ACM_CAREAW4// 0.9581,1.1720,8.2328,8.2328,0.9666,1.1641,8.7172,8.7172,0.9750,1.1561 //ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,0.9797,1.8098,0.5824,0.5824 //ACM_CAREAH2// 1.0857,1.8720,0.8737,0.8737,1.1916,1.9343,1.1649,1.1649,1.2977,1.9967 //ACM_CAREAH3// 1.4562,1.4562,1.4036,2.0590,1.7474,1.7474,1.5097,2.1214,2.0387,2.0387 //ACM_CAREAH4// 1.6158,2.1837,2.3299,2.3299,1.7217,2.2460,2.6212,2.6212,1.8278,2.3083 //ACM_CAREAV1// 0,0,0.5637,1.6915,0.2506,0.2506,0.7741,1.8116,0.5012,0.5012 //ACM_CAREAV2// 0.9843,1.9316,0.7518,0.7518,1.1947,2.0518,1.0024,1.0024,1.4049,2.1719 //ACM_CAREAV3// 1.2530,1.2530,1.6153,2.2918,1.5036,1.5036,1.8256,2.4119,1.7541,1.7541 //ACM_CAREAV4// 2.0359,2.5320,2.0048,2.0048,2.2460,2.6521,2.2555,2.2555,2.4563,2.7722 wing_area = 310.0 wing_span = 57.2 wing_root_chord = 5.4 wing_dihedral = 6.0 wing_incidence = 1.0 wing_twist = -1.5 oswald_efficiency_factor = 0.7 wing_winglets_flag = 1 wing_sweep = 1.0 wing_pos_apex_lon = 2.1 wing_pos_apex_vert = 0.0 htail_area = 67.0 htail_span = 17.2 htail_pos_lon = -22.6 htail_pos_vert = 0.0 htail_incidence = 0.5 htail_sweep = 20.0 vtail_area = 42.0 vtail_span = 7.4 vtail_sweep = 40.0 vtail_pos_lon = -20.5 vtail_pos_vert = 4.1 elevator_area = 17.0 aileron_area = 13.5 rudder_area = 7.3 elevator_up_limit = 17.0 elevator_down_limit = 15.5 aileron_up_limit = 18.0 aileron_down_limit = 18.0 rudder_limit = 30.0 elevator_trim_limit = 15.0 spoiler_limit = 60.0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [flight_tuning] cruise_lift_scalar=.8 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 [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=3270 //Maximum torque available (ft-lbs) [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.5 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [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 [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 [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [Reference Speeds] flaps_up_stall_speed=106.0 //Knots True (KTAS) full_flaps_stall_speed=96.8 //Knots True (KTAS) cruise_speed=300.0 //Knots True (KTAS) max_mach = 0.58 max_indicated_speed = 263 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [stall_warning] type=2