[fltsim.0] title=Eurocopter AS 350 Ecureuil sim=AS 350 model= panel= sound= texture=pdrm kb_checklists= kb_reference= ui_manufacturer=Aerospatiale ui_type=AS 350 ui_variation=PDRM Choper prop_anim_ratio=-1.86 atc_id=PDRM description=The AS.350 was developed by Aerospatiale in the early 1970s, an Avco Lycoming powered prototype first flying on 27 June 1974, followed by a Turbomeca Arriel version on 14 February 1975. Customer deliveries of the Ecureuil (Squirrel) began in April 1978.\nThe Ecureuil was intended to replace the Alouette, and to compete with the Bell 206. The type represents one of Europe's most successful civil helicopter designs, and has found numerous overseas markets. It was also produced as the AS.550 Fennec military helicopter.\n atc_heavy=0 atc_airline=EAGLE atc_flight_number= [General] performance=AS-350 - One 546kW (732shp) Turboméca Arriel 1D1 turboshaft driving a three blade main rotor and two blade tail rotor.\nMax speed 287km\/h (155kt), cruise speed 242km\/h (131kt). Max rate of climb 1752ft\/min. Hovering ceiling out of ground effect 8360ft. Range with max fuel 772km (448nm). \n atc_model=AS350 atc_type=Helicopter editable=1 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0 =176.000000, 5.905000, 1.312000, -1.476000, Pilot station_load.1 =176.000000, 5.905000, -1.312000, -1.476000, Co-pilot station_load.2 =0.000000, 3.280000, 1.968000, 0.000000, Passenger1 station_load.3 =0.000000, 3.280000, 0.984000, 0.000000, Passenger2 station_load.4 =0.000000, 3.280000, -0.984000, 0.000000, Passenger3 station_load.5 =0.000000, 3.280000, -1.968000, 0.000000, Passenger4 station_load.6 =0.000000, 0.000000, 1.640000, -1.320000, Baggage1 station_load.7 =0.000000, 0.000000, -1.640000, -1.320000, Baggage2 station_load.8 =0.000000, -3.280000, 0.000000, -1.312000, Baggage3 empty_weight= 2650.000 empty_weight_roll_MOI= 8000.000 empty_weight_pitch_MOI= 8000.000 empty_weight_yaw_MOI= 11000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 4960.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.980, 0.000, 1.140, 143.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=2, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=4, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=2, 2 , 17.0 fuel_pump=0, 5 , 17.0 hydraulic_pump=0, 2, 17.0 starter1=0, 20, 17.0 light_nav=4, 5 , 17.0 light_beacon=4, 5 , 17.0 light_landing=4, 5 , 17.0 light_strobe=4, 5 , 17.0 light_panel=0, 5 , 17.0 light_cabin=0, 5, 17.0 max_battery_voltage=32.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [pitot_static] vertical_speed_time_constant=99 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=cabin light.0 = 3, -15.74, -4.25, 0.04, fx_navred , light.1 = 3, -15.74, 4.25, 0.04, fx_navgre , light.2 = 3, -23.62, 0.00, 0.49, fx_navwhi , light.3 = 1, -23.95, 0.00, 5.24, fx_beacon , light.4 = 5, 5.50, 1.16, -3.75, fx_landing , light.5 = 5, 5.50, -1.16, -3.75, fx_landing , light.6 = 4, 6.23, 0.00, 0.50, fx_vclighth , light.7 = 10, 3.28, 0.00, 0.50, fx_vclight , light.8 = 2, -15.74, -4.25, 0.04, fx_strobe , light.9 = 2, -15.74, 4.25, 0.04, fx_strobe , light.10 = 2, -23.62, 0.00, 0.49, fx_strobe , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt landrotorwas=fx_rtr_lnd waterrotorwash=fx_rtr_wt [exits] number_of_exits=2 exit_rate.0=0.4 exit_rate.1=0.4 [GeneralEngineData] engine_type= 1 Engine.0= -1.968, 0.000, 1.640 fuel_flow_scalar= 3.500 min_throttle_limit=0.000000 master_ignition_switch=1 max_contrail_temperature=-40.0 [propeller] thrust_scalar = 1.6 [Reference Speeds] cruise_speed=131.000000 max_indicated_speed=155.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=0000.000000 autothrottle_available=0 pitch_takeoff_ga=0.000000 [direction_indicators] direction_indicator.0=3,0 [Views] eyepoint=6.230, 1.200, 0.940 [brakes] toe_brakes_scale=0 parking_brake=0 [hydraulic_system] normal_pressure=507.632000 engine_map=1,0,0,0 electric_pumps=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0=1,7 [contact_points] static_pitch = 0.200 static_cg_height = 6.000 point.0= 3.000, 5.570, 3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.280, 2.500, 0.680, 0.000, 0.000, 7.000, 0.000, 0.000 point.1= 3.000, 5.570, -3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.280, 2.500, 0.680, 0.000, 0.000, 7.000, 0.000, 0.000 point.2= 3.000, -4.590, 3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.390, 2.500, 0.700, 0.000, 0.000, 8.000, 0.000, 0.000 point.3= 3.000, -4.590, -3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.390, 2.500, 0.700, 0.000, 0.000, 8.000, 0.000, 0.000 point.4= 2.000, 0.000, -16.730, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5= 2.000, 0.000, 16.730, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.6= 2.000, -24.270, 0.000, 4.920, 300.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.7= 2.000, 16.730, 0.000, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8= 2.000, 11.480, 0.000, -1.960, 300.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.9= 2.000, -24.270, 0.000, -2.620, 500.000, 0.000, 0.000, 0.000, 0.250, 1.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 [MainRotor] Position=0.000, 0.000, 4.429 Radius=17.535 RatedRmp=390 Number_of_blades=3.000000 Weight_per_blade=30.000000 Weight_to_moi_factor=0.600000 inflow_vel_reference=0.400000 max_disc_angle=5.000000 [SecondaryRotor] TailRotor=1 Position=-19.684, 0.000, 0.656 Radius=6.725 Number_of_blades=2.000000 Weight_per_blade=5.000000 Weight_to_moi_factor=0.000000 inflow_vel_reference=0.000000 [Helicopter] reference_length=42.450000 reference_frontal_area=35.198000 reference_side_area=22.388000 side_aero_center=0.000000 right_trim_scalar=1.000000 correlator_available=1.000000 governed_pct_rpm_ref=1.000000 rotor_brake_scalar=1.500000 torque_scalar=1.000000 cyclic_roll_control_scalar=1.000000 cyclic_pitch_control_scalar=1.000000 pedal_control_scalar=1.000000 collective_on_rotor_torque_scalar=1.000000 [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 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 6.011 rated_N2_rpm= 41.586 static_thrust= 1700.000 afterburner_available= 0 reverser_available= 0.000