[fltsim.0] title=ATR42 sim=ATR42 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=D4-CBF atc_airline=TCV atc_flight_number=vr412 ui_manufacturer=ATR ui_type=ATR42 ui_variation=CABO VERDE AIRLINES atc_heavy=0 description=ATR 42-300 AVIAO REGIONAL ADQUIRIDO PELO TACV EM 1996 Model by Alberto La Greca Repainted with TACV CABO VERDE AIRLINES colors by Antonio Luiz Delgado, flight dynamic configured configured by José Antonio Neves Ramos [General] atc_type=ATR atc_model=ATR42 performance=Max Take-off weight 16692 kg \/ 36722 lb Max Landing Weight 16397 kg \/ 36073 lb \nMax Empty Weight 10285 kg \/ 22627 lb\nMax Payload 4915 kg \/ 10813 lb \nSeating Standard 42-50 \nRange 1185km (48 pax @ 95kg)\nMax Cruise Speed 270 kt mach .49 @FL200 \nEngine PW121 \nPropeller HS 14SF, 4 blade\n\n\n\n\n [WEIGHT_AND_BALANCE] max_gross_weight= 36475.000 empty_weight= 25888.000 reference_datum_position= 0.000, 0.000, 6.800 empty_weight_CG_position= 0.000, 0.000, -10.000 max_number_of_stations= 50 ;Moments of Inertia empty_weight_pitch_MOI= 200000.000 empty_weight_roll_MOI= 205716.000 empty_weight_yaw_MOI= 350944.000 empty_weight_coupled_MOI= 1300.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.0= 0.000, 0.000, 0.000, 0.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=0.856 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=0.502 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 5 Engine.0= 5.900, -13.000, 2.800 Engine.1= 5.900, 13.000, 2.800 fuel_flow_scalar= 1.000 [propeller] thrust_scalar=1.000 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= 0.004 gear_reduction_ratio= 17.600 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= 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 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 21400.000 static_thrust= 195.000 afterburner_available= 0 [turboprop_engine] power_scalar=1.000 maximum_torque= 8639.000 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, 35.000, 0.000, -13.400, 1500.000, 0.000, 1.600, 80.000, 0.400, 2.500, 0.900, 5.000, 6.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.000, -7.200, -13.600, 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, -2.000, 7.200, -13.600, 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, -0.500, -42.667, 3.833, 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, -0.500, 42.667, 3.833, 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, -20.333, 0.000, -5.833, 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, 24.083, 0.000, -10.833, 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= 0.000, -14.500, 12.000, 758.000, 0.000 RightMain= 0.000, 14.500, 12.000, 758.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA 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= 7.500 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 [Reference Speeds] flaps_up_stall_speed= 102.000 full_flaps_stall_speed= 81.600 cruise_speed= 304.798 [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=1 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 [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, 2.00, -38.98, 5.10, fx_navred , light.1=3, 2.00, 38.98, 5.10, fx_navgre , light.2=3, -41.80, 0.00, 2.00, fx_navwhi , light.3=2, 1.95, -38.98, 5.10, fx_strobe , light.4=2, 1.95, 38.98, 5.10, fx_strobe , light.5=1, -35.20, 0.00, 17.00, fx_beacon , light.6=1, 1.00, 0.00, -4.80, 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, [direction_indicators] direction_indicator.0=3,0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 0, 1 Nav.2=1, 0, 1 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= 15.000, 0.000 flaps-position.2= 30.000, 0.000 flaps-position.3= 45.000, 0.000
