//Original by FSpainter/Florian LAROYE © //___________________________________________________________________________ [fltsim.0] title="AS 350BA Ecureuil FSpainter" sim=AS350BA model= panel= sound= texture= kb_checklists="AS 350BA\AS350BA_check" kb_reference="AS 350BA\AS350BA_ref" atc_id="F-HUYT" atc_id_color="0x000000" atc_airline="" atc_flight_number="" prop_anim_ratio="1.41" ui_manufacturer="Eurocopter" ui_type="AS 350BA Ecureuil" ui_variation="FSpainter" description="Successeur de l'Alouette II, l'Ecureil fut conçu comme un appareil à bon marché ne nécessitant pas une maintenance importante et présentant un niveau de vibration et de bruit peu important. Le prototype de cet appareil effectua son vol initial en avril 1974, et les machines suivantes furent dotées d'un Turbomeca Arriel ou d'un Lycoming LTS101 de 615 ch. Ce dernier équipe les versions AS 350C et AS 350D Astar, destinées au marché nord-américain, alors que le premier propulse la variante AS 350B, conçue pour le marché mondial. Un modèle bimoteur, mis au point sous la désignation d'AS 355 (Twinstar en Amérique et Ecureil 2 dabs le reste du monde), a donné naissance à deux sous-versions : l'AS 355E et l'AS 355F, avec un fuselage renforcé, des pales de rotor différentes et un systme de transmission modifié." //___________________________________________________________________________ //___________________________________________________________________________ //___________________________________________________________________________ [General] atc_type="Eurocopter" atc_model="AS 350BA" atc_heavy="0" editable="0" performance="Vitesse à ne jamais dépasser\t\t155 kts\nVitesse de croisière\t138 kts\nTaux de montée\t1 700 ft/min\nEndurance\t4h42\nPlafond pratique\t16000 ft" Category=helicopter //___________________________________________________________________________ [WEIGHT_AND_BALANCE] max_gross_weight = 4960 empty_weight = 2167 reference_datum_position= 1.2, 0.0, 0.0 empty_weight_CG_position= 1.2, 0.0, 0.0 max_number_of_stations=50 empty_weight_pitch_MOI = 5200 empty_weight_roll_MOI = 4900 empty_weight_yaw_MOI = 6000 empty_weight_coupled_MOI = 0 station_load.0 = "170, 4.90, 1.35, 3.45, Pilote" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "0, 4.90,-1.35, 3.45, Co-Pilote" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "0, 2.90,-1.80, 3.45, Passager 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "0, 2.90, 1.80, 3.45, Passager 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "0, 2.90,-0.90, 3.45, Passager 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "0, 2.90, 0.90, 3.45, Passager 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "0, -1.50, 0.00, 1.00, Baggages" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //4.90,1.35,3.45 //___________________________________________________________________________ [FLIGHT_TUNING] cruise_lift_scalar=1.307 parasite_drag_scalar=2.700 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.600 roll_stability=1.000 yaw_stability=1.00 elevator_trim_effectiveness=0.512 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 //___________________________________________________________________________ [turboprop_engine] power_scalar=1.0 //___________________________________________________________________________ [propeller] thrust_scalar=1.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=2 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 //___________________________________________________________________________ [Helicopter] reference_length = 21.58 reference_frontal_area = 17.7 reference_side_area = 44.5 side_aero_center = -12.5 right_trim_scalar = 1.0 correlator_available = 1 governed_pct_rpm_ref = 1.04 governor_pid = 0.4, 0, 0.1, 0, 0.2 rotor_brake_scalar = 1.0 torque_scalar = 1.0 cyclic_roll_control_scalar =1.0 cyclic_pitch_control_scalar =1.0 pedal_control_scalar =1.0 collective_on_rotor_torque_scalar = 1.0 //___________________________________________________________________________ [electrical] //BusType, MaxAmpLoad, MinVoltage //BusTypes : 0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage= 32 generator_alternator_voltage = 28.5 max_generator_alternator_amps = 70 flap_motor = 2, 5 , 17.0 gear_motor = 2, 5 , 17.0 autopilot = 2, 5 , 17.0 avionics_bus = 2, 5 , 17.0 avionics = 1, 5 , 17.0 pitot_heat = 2, 2 , 17.0 additional_system = 2, 2 , 17.0 marker_beacon = 1, 2 , 17.0 fuel_pump = 2, 5 , 17.0 starter1 = 4, 20, 17.0 light_nav = 2, 5 , 17.0 light_beacon = 2, 5 , 17.0 light_landing = 2, 5 , 17.0 light_taxi = 2, 5 , 17.0 light_strobe = 2, 5 , 17.0 light_panel = 2, 5 , 17.0 //___________________________________________________________________________ [contact_points] static_pitch = 0 static_cg_height = 2.67 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 13 point.0 = 3, 4.43, 2.70, -2.80, 3000.000, 0, 0.519, 0.000, 0.120, 2.500, 0.985, 0.000, 0.000, 0.000, 0.000, 0.000 point.1 = 3, -3.07, -2.70, -2.80, 3000.000, 0, 0.519, 0.000, 0.150, 2.500, 0.998, 0.000, 0.000, 0.000, 0.000, 0.000 point.2 = 3, -3.07, 2.70, -2.80, 3000.000, 0, 0.519, 0.000, 0.150, 2.500, 0.998, 0.000, 0.000, 0.000, 0.000, 0.000 point.3 = 3, 4.43, -2.70, -2.80, 3000.000, 0, 0.519, 0.000, 0.120, 2.500, 0.985, 0.000, 0.000, 0.000, 0.000, 0.000 point.4 = 2, 0.00, -16.67, 9.00, 00.00, 0, 0.0000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0 point.5 = 2, 0.00, 16.67, 9.00, 00.00, 0, 0.0000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0 point.6 = 2, -20.50, 0.00, -0.75, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.7 = 2, 0.00, 9.08, 2.58, 787.4, 0, 0.0000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0 point.8 = 1, 0.0, 0.0, 0.0, 3574.8, 0, 0.5187, 0.0, 0.2, 10.4, 0.50, 0.0, 0.0, 2.0, 0.0, 0.0 point.9 = 4, 4.43, 2.70, -1.70, 3000.000, 0, 0.519, 0.000, 0.120, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 point.10 = 4, -3.07, -2.70, -1.70, 3000.000, 0, 0.519, 0.000, 0.150, 2.500, 0.728, 0.000, 0.000, 0.000, 0.000, 0.000 point.11 = 4, -3.07, 2.70, -1.70, 3000.000, 0, 0.519, 0.000, 0.150, 2.500, 0.728, 0.000, 0.000, 0.000, 0.000, 0.000 point.12 = 4, 4.43, -2.70, -1.70, 3000.000, 0, 0.519, 0.000, 0.120, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 //___________________________________________________________________________ [Views] eyepoint=4.90,1.35,3.45 //___________________________________________________________________________ [exits] number_of_exits=2 exit_rate.0=1.0 exit_rate.1=0.7 //___________________________________________________________________________ [Radios] Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 //___________________________________________________________________________ [keyboard_response] elevator=100, 180 aileron=200, 1000 rudder=200, 1000 //___________________________________________________________________________ [direction_indicators] direction_indicator.0=3,0 //___________________________________________________________________________ [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -16.50, -5.00, 2.70, fx_navred , light.1=3, -16.50, 4.85, 2.70, fx_navgre , light.2=3, -24.95, -0.12, 3.30, fx_navwhi , light.3=1, -24.90, -0.12, 7.90, fx_beacon , light.4=4, 5.00, 0.20, 1.50, fx_vclight , light.5=4, 2.75, 0.00, 2.80, fx_vclight , //___________________________________________________________________________ [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt //___________________________________________________________________________ [fuel] LeftMain =-1.2, 0.0, 0.0, 142.651,6, 0.0 fuel_type=2 number_of_tank_selectors=1 electric_pump=1 //___________________________________________________________________________ [GeneralEngineData] engine_type=1 Engine.0=8.3, 0.0, 0.4 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 //___________________________________________________________________________ [Reference Speeds] flaps_up_stall_speed = 0.00 //Knots True (KTAS) full_flaps_stall_speed = 0.00 //Knots True (KTAS) cruise_speed = 138.0 //Knots True (KTAS) max_indicated_speed = 155.0 //Red line (KIAS) //___________________________________________________________________________ [brakes] toe_brakes_scale=1.915586 parking_brake=1 //___________________________________________________________________________ [hydraulic_system] normal_pressure=75.000000 engine_map=1,0,0,0 //___________________________________________________________________________ [attitude_indicators] attitude_indicator.0=1 //___________________________________________________________________________ [turn_indicators] turn_indicator.0=1,0 //___________________________________________________________________________ [MainRotor] Position = 0, 0, 4.91 Radius = 12.583 max_disc_angle = 5.0 RatedRpm = 510 Number_of_blades = 6 Weight_per_blade = 26.0 Weight_to_moi_factor = 0.58 inflow_vel_reference = 34.0 //___________________________________________________________________________ [SecondaryRotor] Position = -22.8, -0.74, 1.8 TailRotor = 1 Radius = 1.75 //___________________________________________________________________________ [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 //___________________________________________________________________________ [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 [fuselage_aerodynamics] drag_force_cf=0.000000 side_drag_force_cf=0.000000 pitch_damp_cf=0.000000 roll_damp_cf=0.000000 yaw_damp_cf=0.000000 yaw_stability_cf=0.000000 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=5.150000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0
