[fltsim.0] title=TFS Dash 8-400 OE-LGA sim=TFS_Dash8-400 model= texture=OE-LGA atc_parking_codes=TYR atc_parking_types=RAMP atc_id=OE-LGA atc_airline=TYROLEAN ui_manufacturer=The Fruit Stand ui_type=Dash 8-402Q ui_variation=OE-LGA description=The Fruit Stand Dash 8-400 [General] atc_type=BOMBARDIER atc_model=DH8D editable=0 performance= For AI pilots only! Do not attemp to fly it as UI.You've been warned! [weight_and_balance] // ACM V2.5 max_gross_weight = 48000 empty_weight = 37888 reference_datum_position = 2, 0, 0 empty_weight_CG_position = 5.8, 0, 0 empty_weight_pitch_MOI = 547662 empty_weight_roll_MOI = 185801 empty_weight_yaw_MOI = 508740 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = "170, 42.0, -2.0, 0.0, Pilot" station_load.1 = "170, 42.0, 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, -42.3, -2.0, 0.0, Passenger" station_load.5 = "170, -42.3, 2.0, 0.0, Passenger" [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 3.55, -46.64, 0.35, fx_navred light.1 = 3, 3.55, 46.64, 0.35, fx_navgre light.2 = 2, 4.05, -46.65, 0.35, fx_strobe light.3 = 2, 4.05, 46.65,0.35 , fx_strobe light.4 = 1, 9.25, 0, -9.85, fx_strobe light.5 = 1, 18.51, 0, -1.28, fx_beacon light.6 = 1, -48.5, 0, 13.1, fx_strobe light.7 = 3, -56.3, 0, 12.2, fx_navwhi [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 1.0 min_throttle_limit = -0.35 engine.0 = 10.3, -14.6, 2.5, engine.1 = 10.3, 14.6, 2.5, [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 electric_pump = 1 LeftMain = 3, -14.5, -1, 900, 0 RightMain = 3, 14.5, -1, 900, 0 [contact_points] point.0 = 1, 46, 0, -12.50, 1200, 0, 0.95, 55, 0.296, 2.5, 0.90, 4.8, 4.8, 0, 195.0, 195.0 point.1 = 1, 0, -14.8, -13.82, 1600, 1, 1.30, 0.0, 0.642, 2.6, 0.95, 5.2, 5.2, 2, 195.0, 195.0 point.2 = 1, 0, 14.8, -13.82, 1600, 2, 1.30, 0.0, 0.642, 2.6, 0.95, 4.9, 4.9, 3, 195.0, 195.0 point.3 = 2, 3.6, -46.5, 0.5, 790, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, 3.6, 46.5, 0.5, 790, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -48.51, 0, -4.8, 790, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 50, 0, -9.55, 790, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch = -1.15 static_cg_height = 13.4 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 [keyboard_response] elevator = 150.0, 250.0 aileron = 150.0, 250.0 rudder = 150.0, 250.0 [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 = 9000 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// 0,0,0,1.6459,0.7990,0.7990,0.0137,1.5772,1.5985,1.5985 //ACM_AREAW2// 0.0274,1.5089,2.3977,2.3977,0.0417,1.4407,3.1970,3.1970,0.0557,1.3724 //ACM_AREAW3// 3.9962,3.9962,0.0697,1.3041,4.7954,4.7954,0.0837,1.2358,5.5946,5.5946 //ACM_AREAW4// 0.0974,1.1675,6.3940,6.3940,0.1115,1.0987,7.1932,7.1932,0.1254,1.0305 //ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1058,1.7661,0.5824,0.5824 //ACM_AREAH2// 0.2117,1.7847,0.8737,0.8737,0.3179,1.8034,1.1648,1.1648,0.4239,1.8220 //ACM_AREAH3// 1.4562,1.4562,0.5299,1.8406,1.7474,1.7474,0.6359,1.8593,2.0387,2.0387 //ACM_AREAH4// 0.7419,1.8779,2.3299,2.3299,0.8478,1.8961,2.6212,2.6212,0.9538,1.9148 //ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.2099,2.2853,0.5012,0.5012 //ACM_AREAV2// 0.4205,2.3152,0.7518,0.7518,0.6308,2.3450,1.0024,1.0024,0.8410,2.3749 //ACM_AREAV3// 1.2530,1.2530,1.0513,2.4047,1.5036,1.5036,1.2617,2.4346,1.7539,1.7539 //ACM_AREAV4// 1.4720,2.4644,2.0048,2.0048,1.6821,2.4941,2.2555,2.2555,1.8926,2.5241 //ACM_CAREAW1// 3.5966,3.5966,0.8855,1.2149,3.9962,3.9962,0.8927,1.2051,4.3958,4.3958 //ACM_CAREAW2// 0.8996,1.1957,4.7954,4.7954,0.9064,1.1864,5.1950,5.1950,0.9136,1.1769 //ACM_CAREAW3// 5.5946,5.5946,0.9204,1.1675,5.9944,5.9944,0.9275,1.1576,6.3940,6.3940 //ACM_CAREAW4// 0.9344,1.1483,6.7936,6.7936,0.9415,1.1390,7.1932,7.1932,0.9484,1.1295 //ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,0.9797,1.8098,0.5824,0.5824 //ACM_CAREAH2// 1.0857,1.8717,0.8737,0.8737,1.1914,1.9342,1.1648,1.1648,1.2977,1.9967 //ACM_CAREAH3// 1.4562,1.4562,1.4033,2.0590,1.7474,1.7474,1.5096,2.1214,2.0387,2.0387 //ACM_CAREAH4// 1.6158,2.1837,2.3299,2.3299,1.7216,2.2460,2.6212,2.6212,1.8278,2.3083 //ACM_CAREAV1// 0,0,0.5637,1.6914,0.2506,0.2506,0.7741,1.8114,0.5012,0.5012 //ACM_CAREAV2// 0.9843,1.9313,0.7518,0.7518,1.1947,2.0518,1.0024,1.0024,1.4048,2.1719 //ACM_CAREAV3// 1.2530,1.2530,1.6153,2.2918,1.5036,1.5036,1.8256,2.4119,1.7539,1.7539 //ACM_CAREAV4// 2.0359,2.5320,2.0048,2.0048,2.2460,2.6521,2.2555,2.2555,2.4563,2.7722 wing_area = 649.0 wing_span = 93.3 wing_root_chord = 10.5 wing_dihedral = 2.0 wing_incidence = 1.0 wing_twist = -1.5 oswald_efficiency_factor = 0.7 wing_winglets_flag = 0 wing_sweep = 4.0 wing_pos_apex_lon = 8.1 wing_pos_apex_vert = -1.5 htail_area = 180.0 htail_span = 29.3 htail_pos_lon = -46.8 htail_pos_vert = 12.0 htail_incidence = 0.8 htail_sweep = 8.0 vtail_area = 152.0 vtail_span = 14.9 vtail_sweep = 30.0 vtail_pos_lon = -37.5 vtail_pos_vert = -2.1 elevator_area = 17.0 aileron_area = 13.5 rudder_area = 7.3 elevator_up_limit = 15.0 elevator_down_limit = 17 aileron_up_limit = 18.0 aileron_down_limit = 18.0 rudder_limit = 30.0 elevator_trim_limit = 15.0 spoiler_limit = 50.0 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 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 engine_generator_map = 1,1 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 [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=4.6 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=750 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.6 //Scalar on Turboprop power maximum_torque=5878 //Maximum torque available (ft-lbs) [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=0.9 induced_drag_scalar=0.9 elevator_effectiveness=0.9 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=1.5 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=13.6 //Propeller Diameter, (feet) propeller_blades=6 //Number of propeller blades propeller_moi=54 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=12 //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=17.0 //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) [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 = 0.16 //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=-8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 8 // seconds flaps-position.0 = 0 // degrees, KIAS flaps-position.1 = 5 // degrees, KIAS flaps-position.2 = 10 // degrees, KIAS flaps-position.3 = 15 // degrees, KIAS //flaps-position.4 = 20 // degrees, KIAS //flaps-position.5 = 25 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [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=100.0 //Knots True (KTAS) full_flaps_stall_speed=125.0 //Knots True (KTAS) cruise_speed=350.0 //Knots True (KTAS) max_mach = 0.58 max_indicated_speed = 285 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.0 autothrottle_available=0 pitch_takeoff_ga=5.0 max_pitch=8.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.5 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=1ยด
