[fltsim.0]
title=AS 350 Ecureuil AirStar
sim=AS 350
model=
panel=
sound=
texture=AirStar
kb_checklists=
kb_reference=
ui_manufacturer=Aerospatiale
ui_type=AS 350
ui_variation=AirStar
prop_anim_ratio=-1.86
atc_id=AS3
description=This is the AS350 Ecureuil with the AirStar Helicopters Livery, serving passenger scenic rides at the Grand Canyon. Repaint by Christian Haensel.
atc_heavy=0
atc_airline=AirStar
atc_flight_number=350
[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=1
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
