[fltsim.0]
title=EC135 ICARO Reach N36RX
sim=EC135
model=us_med1
panel=glass_half
sound=pw
texture=N36RX
kb_checklists=
ui_manufacturer=Eurocopter
ui_type=EC 135 ICARO
ui_variation=Reach N36RX
description=Created by ICARO Group Development Team
atc_heavy=0
atc_airline=
atc_flight_number=N36RX
prop_anim_ratio=0.41
atc_id=N36RX
atc_id_color=0000000000
visual_damage=0


[General]
atc_type=Eurocopter
atc_model=EC35
performance=2 x Pratt & Whitney PW 206 B\tje 546 kw/ 732 PS\nRotordurchmesser:\t10,20 m\nRumpflдnge:\t10,16 m\nLeermasse:\t1420 kg\nmax. Abflugmasse:\t2900 kg\nDienstgipfelhцhe:\t3900 m\nReichweite:\t720 km\nGeschwindigkeit:\tmax. 287 km/h, Reise 261 km/h 
editable=1 

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi

//light.0 = 1, -21.27, -0.26, 6.84, fx_beacon
//light.1 = 6, 11.50, 0, -0.84, fx_shockwave_landing_light
//light.2 = 5, 8.90, -1.18, -3.88, fx_shockwave_landing_light_light
//light.3 = 5, 7.92, -1.16, -3.28, fx_shockwave_landing_light_narrow_down_22
//light.4 = 2, -2.59, 2.66, 0.10, fx_shockwave_strobe_l
//light.5 = 2, -2.59, -2.68, 0.10, fx_shockwave_strobe_l
//light.6 = 3, -14.39, -4.42, 0.52, fx_navred
//light.7 = 3, -14.40, 4.44, 0.52, fx_navgre
//light.8 = 3, -23.46, -0.36, 6.51, fx_shockwave_navwhi
//light.9 = 4, 3.78, 0, -0.36, fx_vclight
//light.10= 4, 7.43, 0, -0.35, fx_vclight

light.0 = 1, 	-21.27, -0.26, 6.84, 	fx_beacon
light.1 = 5, 	8.45, 1.21, -3.10, 	fx_landing_light
light.2 = 5, 	6.87, 1.26, -3.47, 	fx_landing_light
light.3 = 2, 	-2.58, 2.66, 0.10, 	fx_strobe
light.4 = 2, 	-2.55, -2.68, 0.10, 	fx_strobe
light.5 = 3, 	-14.23, -4.55, 0.55, 	fx_navred
light.6 = 3, 	-14.23, 4.57, 0.55, 	fx_navgre
light.7 = 3, 	-23.51, -0.36, 6.51, 	fx_navwhi
light.8 = 4, 	3.78, 0, -0.36, 	fx_vclight
light.9 = 4, 	7.43, 0, -0.35, 	fx_vclight


[smokesystem]
smoke.0 = 2.77, -9.77, 2.45, fx_Heatshimmer5
smoke.1 = 2.77, -9.79, -2.5, fx_Heatshimmer5


[contact_points]
static_pitch = 0.198
static_cg_height = 5.80
max_number_of_points = 8
        //0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
        //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)



//    	 	 1	2	3	4		5	6	7	8     9   	10	11 12 13 14 15
point.0 = 3, 5.92, 	3.60, 	-5.85, 	1574.8, 	1, 	0.519, 	0, 0.286975, 2.5, 	0.605, 	0, 0, 7, 0, 0
point.1 = 3, -1.50, -3.60, 	-5.75, 	1574.8, 	2, 	0.519,	0, 0.396299, 2.5, 	0.728, 	0, 0, 7, 0, 0
point.2 = 3, -1.50, 3.60, 	-5.75, 	1574.8, 	0, 	0.519, 	0, 0.396299, 2.5, 	0.728, 	0, 0, 7, 0, 0
point.3 = 3, 5.92, 	-3.60, 	-5.85, 	1574.8, 	0, 	0.519, 	0, 0.286975, 2.5, 	0.605, 	0, 0, 7, 0, 0
point.4 = 2, 0, 	-17.53, 4.73, 	0, 0, 0, 	0, 	0, 		0, 0, 	0, 		0, 0, 0, 0, 0, 0
point.5 = 2, 0, 	17.53, 	4.73, 	0, 0, 0, 	0, 	0, 		0, 0, 	0, 		0, 0, 0, 0, 0, 0
point.6 = 2, -18.94, 0, 	-2.5902, 787.4, 	1, 	0, 		0, 0, 	0, 		0, 0, 0, 9, 0, 0
point.7 = 2, 9.2402, 0, 	-3.32, 	787.400, 	2, 	0, 		0, 0, 	0, 		0, 0, 0, 4, 0, 0


[Views]
;            z    x   y
eyepoint= 5.60, 1.40, 1.60      //(feet) longitudinal, lateral, vertical distance from reference datum



[fuel]
RightMain= -0.000, 0.000, 0.000, 14.503, 0.694
external1= 2.000, 0.000, 0.000, 148.148, 1.123
LeftMain= -0.000, 0.000, 0.000, 14.503, 0.694
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[GeneralEngineData]
engine_type = 5
Engine.0 = 5.000, 0.000, 2.600
fuel_flow_scalar=90.000000
min_throttle_limit=0.000000

[TurbineEngineData]
fuel_flow_gain=0.2000
inlet_area=10.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=1700.000000
static_thrust=300                   //Fuel Flow
afterburner_available=0

[turboprop_engine]
power_scalar = 1.0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=2.000
parasite_drag_scalar=0.010
induced_drag_scalar=0.010
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000


[WEIGHT_AND_BALANCE]
max_gross_weight = 6250.000
empty_weight = 4100.000

reference_datum_position     =  0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50

station_load.0 = 198.000000, 5.931,1.345,-1.000000 ,Pilot        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 198.000000, 5.931,-1.345,-1.000000 ,HEMS-CrewMember        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 000.000000, -0.506,-1.345,-1.396  ,Patient       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 190.000000, 1.993,1.238,-1.396  ,Doc        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 000.000000, 3.993, -1.238,-1.396  ,HEMS-Hinten       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 266.000000,0.000000,0.000000,0.000000  ,Medical Equipment    //   Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI   = 4000.000
empty_weight_roll_MOI    = 4000.000
empty_weight_yaw_MOI     = 6000.000
empty_weight_coupled_MOI = 10.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[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]
low_realism_stability_scale = 1.0, 1.0, 1.0             //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24.0           //Battery Voltage - fully charged
generator_alternator_voltage = 28.0  //Alternator/Aenerator Voltage
max_generator_alternator_amps = 100.0

autopilot          = 1, 1 , 17.0
avionics_bus       = 0, 1,  17.0
avionics           = 0, 10 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 3, 17.0
marker_beacon      = 0, 2 , 17.0
gear_warning       = 0, 0 , 17.0
fuel_pump          = 0, 3 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 1 , 17.0
light_beacon       = 0, 1 , 17.0
light_landing      = 0, 3 , 17.0
light_taxi         = 0, 2 , 17.0
light_strobe       = 0, 1 , 17.0
light_panel        = 0, 4 , 17.0

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 1
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[Reference Speeds]
flaps_up_stall_speed    = 0.0                   //Knots True (KTAS)
full_flaps_stall_speed  = 0.0                   //Knots True (KTAS)
cruise_speed            = 135.0                 //Knots True (KTAS)
max_indicated_speed=1000.000000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks

[exits]
number_of_exits=4
exit_rate.0=0.4
exit_rate.1=0.4
exit_rate.2=0.4
exit_rate.3=0.4


[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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0.001
autothrottle_available=1
pitch_takeoff_ga=0.000000
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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

[airplane_geometry]
wing_area=170.000000
wing_span=35.000000
wing_root_chord=5.000000
wing_dihedral=6.998291
wing_incidence=1.499634
wing_twist=-0.999756
oswald_efficiency_factor=0.781155
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.215000
wing_pos_apex_vert=0.000000
htail_area=32.000000
htail_span=12.833333
htail_pos_lon=-13.000000
htail_pos_vert=0.000000
htail_incidence=2.999268
htail_sweep=0.000000
vtail_area=16.000000
vtail_span=4.560702
vtail_sweep=0.000000
vtail_pos_lon=-12.166667
vtail_pos_vert=2.500000
elevator_area=32.000000
aileron_area=12.800000
rudder_area=3.500000
elevator_up_limit=10.999988
elevator_down_limit=6.999997
aileron_up_limit=30.000070
aileron_down_limit=12.501939
rudder_limit=26.997771
elevator_trim_limit=12.000028
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
tailhook_rate=0.002

[brakes]
toe_brakes_scale=1.000000
parking_brake=0

[hydraulic_system]
normal_pressure=0.000000


[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=2
attitude_indicator.1=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0