[fltsim.0]
title=Eurocopter AS 350 Ecureuil - Policia Militar de São Paulo
sim=AS 350
model=
panel=
sound=
texture=pm_sp
kb_checklists=
kb_reference=
ui_manufacturer=Aerospatiale
ui_type=AS 350 
ui_variation=Águia 4 - PM SP
prop_anim_ratio=-1.86
atc_id=PP-EOX
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
Category=helicopter

[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
pitot_heat=1.000000

[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
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
