[fltsim.0] title=Airwave Airlines Express Dash 8 sim=DH_Dash8_100 model= panel= sound= texture= kb_checklists=DH_Dash8_100_check kb_reference=DH_Dash8_100_ref atc_id=N700MS atc_airline=Airwave atc_flight_number=1123 ui_manufacturer=De Havilland ui_type=Express Prop ui_variation=Airwave Airlines Express description= atc_heavy=0 [General] atc_type=DEHAVILLAND atc_model=DH8A performance= [WEIGHT_AND_BALANCE] max_gross_weight = 34500.000 empty_weight = 22730.000 reference_datum_position = 31.000, 0.000, 0.000 empty_weight_CG_position = -26.000, 0.000, 0.000 max_number_of_stations = 50 station_load.0 = 170.000, -9.800, -1.750, 0.000 station_load.1 = 170.000, -9.800, 1.750, 0.000 station_load.2 = 5660.000, -27.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI = 111701.000 empty_weight_roll_MOI = 61201.000 empty_weight_yaw_MOI = 161691.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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 = 5 Engine.0 = -28.400, -13.300, 2.700 Engine.1 = -28.400, 13.300, 2.700 fuel_flow_scalar = 1.000 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 propeller_diameter = 13.000 propeller_blades = 4 propeller_moi = 77.000 beta_max = 45.000 beta_min = 12.000 min_gov_rpm = 25520.000 prop_tc = 0.004 gear_reduction_ratio = 17.000 fixed_pitch_beta = 0.000 low_speed_theory_limit = 80.000 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather = 700.000 beta_feather = 79.300 power_absorbed_cf = 0.900 defeathering_accumulators_available= 0 prop_reverse_available = 1 minimum_on_ground_beta = 1.000 minimum_reverse_beta = -14.000 [TurbineEngineData] fuel_flow_gain = 0.011 inlet_area = 1.000 rated_N2_rpm = 29920.000 static_thrust = 200.000 afterburner_available= 0 [turboprop_engine] power_scalar = 1.0 //Scalar on Turboprop power maximum_torque = 7878.000 [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 = 1.000, -5.000, 0.000, -7.450, 1500.000, 0.000, 1.617, 25.000, 0.500, 2.500, 0.900, 5.000, 6.000, 0.000, 100.000, 422.014 point.1 = 1.000, -29.000, -12.990, -7.550, 3000.000, 1.000, 0.633, 0.000, 0.675, 2.500, 0.800, 6.000, 7.000, 2.000, 100.000, 422.014 point.2 = 1.000, -29.000, 12.990, -7.550, 3000.000, 2.000, 0.633, 0.000, 0.675, 2.500, 0.800, 6.000, 7.000, 3.000, 100.000, 422.014 point.3 = 2.000, -31.600, -42.500, 5.390, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4 = 2.000, -31.600, 42.500, 5.390, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5 = 2.000, -68.600, 0.000, 1.220, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6 = 2.000, 0.000, 0.000, -3.920, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points = 21 static_pitch = -0.400 static_cg_height = 7.100 [Views] eyepoint= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] LeftMain = -31.100, -9.100, 3.900, 417.500, 0.000 RightMain = -31.100, 9.100, 3.900, 417.500, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 585.000 wing_span = 85.000 wing_root_chord = 7.000 wing_dihedral = 2.500 wing_incidence = 1.000 wing_twist = -3.000 oswald_efficiency_factor= 0.700 wing_winglets_flag = 0 wing_sweep = 3.000 wing_pos_apex_lon = -25.000 wing_pos_apex_vert = 0.000 htail_area = 97.000 htail_span = 26.000 htail_pos_lon = -58.900 htail_pos_vert = 0.000 htail_incidence = 1.000 htail_sweep = 8.000 vtail_area = 106.000 vtail_span = 11.700 vtail_sweep = 30.000 vtail_pos_lon = -54.900 vtail_pos_vert = 3.400 elevator_area = 53.500 aileron_area = 12.100 rudder_area = 46.400 elevator_up_limit = 17.000 elevator_down_limit = 15.500 aileron_up_limit = 18.000 aileron_down_limit = 18.000 rudder_limit = 30.000 elevator_trim_limit = 15.000 spoiler_limit = 60.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 92.000 full_flaps_stall_speed = 72.000 cruise_speed = 265.000 [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= 150.0, 250.0 aileron= 150.0, 250.0 rudder= 150.0, 250.0 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available= 0 pitch_takeoff_ga=8.000000 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -30.1, -42, 5, fx_navred , light.1 = 3, -30.1, 42, 5, fx_navgre , light.2 = 2, -29.9, 41.7, 5, fx_strobe , light.3 = 2, -29.9, -41.7, 5, fx_strobe , light.4 = 1, -65.0, 0.00, 18.4, fx_beacon , light.5 = 4, -7.91, 0.00, 2.64, fx_vclight, [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 5.000 system_type= 0 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 30.000, 0.000 flaps-position.3= 40.000, 0.000