[fltsim.0] JABIndex=1 title=ATR42-300 sim=atr42 300 model= panel= sound= texture= checklists= kb_checklists=checklist description=ATR42-300 Inter Candian, late 90's ui_manufacturer=Avions de Transport Regional (ATR) ui_type=42-300 ui_variation=Inter Canadian atc_heavy=0 atc_id= atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, -10.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight= 25888.000 empty_weight_roll_MOI= 205716.000 empty_weight_pitch_MOI= 200000.000 empty_weight_yaw_MOI= 350944.000 empty_weight_coupled_MOI= 1300.000 max_gross_weight= 31475.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain= 0.000, -14.500, 12.000, 758.000, 0.000 RightMain= 0.000, 14.500, 12.000, 758.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 870.000 wing_span= 88.750 wing_root_chord= 8.830 wing_dihedral= 1.500 wing_incidence= 1.500 wing_twist= -1.500 oswald_efficiency_factor= 0.800 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -1.500 wing_pos_apex_vert= 5.280 htail_area= 120.000 htail_span= 23.917 htail_pos_lon= -36.000 htail_pos_vert= 12.000 htail_incidence= 0.500 htail_sweep= 0.000 vtail_area= 150.000 vtail_span= 14.000 vtail_sweep= 5.000 vtail_pos_lon= -36.000 vtail_pos_vert= 12.000 elevator_area= 40.000 aileron_area= 35.920 rudder_area= 69.530 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 33.491 elevator_trim_limit= 5.000 spoiler_limit= 59.989 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 10.000 min_flaps_for_spoilerons= 0.000 //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, 35.000, 0.000, -13.600, 1574.803, 0.000, 0.518, 78.000, 0.250, 1.500, 0.900, 8.000, 8.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.667, -7.200, -13.700, 1574.803, 1.000, 0.718, 0.000, 0.283, 1.500, 0.970, 9.000, 9.000, 2.000, 0.000, 0.000 point.2= 1.000, -2.667, 7.200, -13.700, 1574.803, 2.000, 0.718, 0.000, 0.283, 1.500, 0.970, 10.000, 10.000, 3.000, 0.000, 0.000 point.3= 2.000, -0.500, -42.667, 3.833, 1574.803, 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, -0.500, 42.667, 3.833, 1574.803, 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, -20.333, 0.000, -5.833, 1574.803, 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, 24.083, 0.000, -10.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 13.400 [GeneralEngineData] engine_type= 5 Engine.0= 5.900, -13.000, 4.000 Engine.1= 5.900, 13.000, 4.000 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 21400.000 static_thrust= 195.000 afterburner_available= 0 [propeller] propeller_type= 0 propeller_diameter= 13.700 propeller_blades= 4 propeller_moi= 280.000 beta_max= 45.000 beta_min= 12.000 min_gov_rpm= 16000.000 prop_tc= 0.000 gear_reduction_ratio= 17.600 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 0.000 beta_feather= 86.000 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 thrust_scalar=1.208 [turboprop_engine] maximum_torque= 8639.000 power_scalar=1.000 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 [Reference Speeds] flaps_up_stall_speed= 102.000 full_flaps_stall_speed= 81.600 cruise_speed= 304.798 [keyboard_response] elevator=30.000, 50.000 aileron=60.000, 250.000 rudder=70.000, 100.000 [Views] eyepoint=30, -1.5, -5 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 5.30, -38.98, -1.00, fx_navred , light.1=3, 5.30, 38.98, -1.00, fx_navgre , light.2=3, -37.30, 0.00, -4.00, fx_navwhi , light.3=2, 5.25, -38.98, -1.00, fx_strobe , light.4=2, 5.25, 38.98, -1.00, fx_strobe , light.5=1, -32.50, 0.00, 11.80, fx_beacon , light.6=1, 7.00, 0.00, -12.00, fx_beacon , light.7=4, 15, 0.00, 2, fx_vclight, light.8=4, 31.5, -2.0, -5.5, fx_vclight, light.9=4, 31.5, 2.0, -5.5, fx_vclight, [General] performance=Wing span 24.57 m \nOverall length 22.70 m \nTotal height 7.59 m \nMax. T\/O weight 16700 kg \nMax. range 900 km \nMax. fuel weight 4500 kg \nCruising altitude 2000 - 7600 m \nCapacity payload 4400 kg \nCruising speed 465 km.\/h \nEngines (2) PW 121 \nMax. Power\/Eng. 2386 hp \n atc_type=ATR atc_model=ATR42 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 vertical_speed_hold_available=1 [direction_indicators] direction_indicator.0=3,0 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=0.858 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=0.4 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [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 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 10.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 0.200 flaps-position.0= 0.000, 0.000 flaps-position.1= 9.998, 0.000 flaps-position.2= 19.996, 0.000 flaps-position.3= 29.994, 0.000 flaps-position.4= 39.992, 0.000
