[fltsim.0] title=ATR42 TEST sim=ATR42 model= panel= sound= texture= kb_checklists=DH_Dash8_100_check kb_reference=DH_Dash8_100_ref atc_id=N700MS atc_airline=Alitalia atc_flight_number=1123 ui_manufacturer=ATR ui_type=ATR42 ui_variation=Alitalia description= atc_heavy=0 [General] atc_type=ATR atc_model=ATR42 editable=1 performance= [WEIGHT_AND_BALANCE] max_gross_weight= 42523.200 empty_weight= 32500.000 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=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [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=1.500 propeller_type= 0 propeller_diameter= 10.500 propeller_blades= 6 propeller_moi= 48.000 beta_max= 60.000 beta_min= 14.000 min_gov_rpm= 29920.000 prop_tc= 0.004 gear_reduction_ratio= 22.500 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= 1.100 rated_N2_rpm= 29995.000 static_thrust= 225.000 afterburner_available= 0 [turboprop_engine] power_scalar=1.000 maximum_torque= 5500.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [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, -6.600, 1500.000, 0.000, 0.800, 25.000, 0.300, 2.500, 0.700, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -33.000, -6.000, -7.200, 3000.000, 1.000, 1.220, 0.000, 0.675, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -33.000, 6.000, -7.200, 3000.000, 2.000, 1.220, 0.000, 0.675, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000 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 [SMOKESYSTEM] smoke.0=2.70,-35.4,-13.3, fx_smoke_rx smoke.1=2.70,-35.4,13.3, fx_smoke_rx [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [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= 586.000 wing_span= 80.333 wing_root_chord= 7.167 wing_dihedral= 2.000 wing_incidence= 2.999 wing_twist= -0.994 oswald_efficiency_factor= 0.842 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -25.000 wing_pos_apex_vert= 0.000 htail_area= 157.000 htail_span= 30.333 htail_pos_lon= -58.900 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 114.000 vtail_span= 12.174 vtail_sweep= 0.000 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 [SMOKESYSTEM] smoke.0=2.70,-35.4,-13.3, fx_smoke_rx smoke.1=2.70,-35.4,13.3, fx_smoke_rx [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 use_no_default_bank=1 use_no_default_pitch=1 [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, [direction_indicators] direction_indicator.0=3,0 [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