[fltsim.0]
title=EC_Tiger_afs_demo
sim=ecTig_afs
model=d
panel=d
sound=d
texture=d
kb_checklists=Bell_206B_JetRanger_check
kb_reference=Bell_206B_JetRanger_ref
prop_anim_ratio=-1.76
atc_id_color=0xc6eff7ff
atc_id=demo
atc_model=
ui_manufacturer=Eurocopter
ui_typerole=military helicopter
ui_createdby=AFS-design
ui_type="EC-505 Tiger "
ui_variation="Demoversion"
description=


[General]
atc_type=eurocopter
performance="Eurocopter TIGER dates:\n Maximum weight:5,925 kg/13,060 lb\nAlternate gross-weight 6,000 kg/13,230 lb\nCapacity1 pil.+1 gunner Useful load HCP (roof sight) 1,800 kg/3,968\nlb U TIGER (mast sight) 1,650 kg/3,638 lb\nMaximal operational weight with external load 6,000 kg/13,230 lb \n Power plant 2 MTR 390 Take-off power (A.E.O.) 958 kW/1,285 \n shp Maximum continuous power (A.E.O.)873 kW/1,171 shp \nFast cruise speed ( at maximum weight)HCP (roof sight) 280 km/h-150 kts \n U TIGER (mast sight) 260 km/h-140 kts Maximum range with standard tank(s)* 800 km-432 n.m.
atc_model=helicopter
editable=0
Category=Helicopter




[CameraDefinition.0]
Title=WEAPONS
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=look WEAPONS
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-3.3, -1.8, -11
InitialPbh=0, 0, 17
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=GEAR
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Description=look GEAR
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-2.2, -1.2, -7
InitialPbh=0, 0, 13
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=COCKPIT RIGTH 
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=look COCKPIT RIGTH 
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=4.8, 1.6, 0.0
InitialPbh=16, 0, 295
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title=COCKPIT LEFT 
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=look COCKPIT LEFT 
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=-6.8, 0.6, -1.0
InitialPbh=6, 0, 70
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=No
ClipMode=Minimum


[CameraDefinition.4]
Title=TAIL
Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description=look TAIL
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.75
ShowWeather=Yes
InitialXyz=0, 2.0, -15.0
InitialPbh=7, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0

[brakes]
parking_brake=1       //Parking brake available
toe_brakes_scale=1.0  //Brake scalar
auto_brakes=0

[hydraulic_system]
normal_pressure=0.0    //PSI

[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, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[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

[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

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

[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=1   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=5.15   //PSI
engine_map=1

[pneumatic_system]
max_pressure=0.000000

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=0.0    //Scalar on heat effectiveness, 0 = not available

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

[Reference Speeds]
cruise_speed=350.0                 //Knots True (KTAS)
max_indicated_speed=400                  //Red line (KIAS)

[autopilot]
autopilot_available=0
flight_director_available=0

[yaw_string]
yaw_string_available=1

[deice_system]
structural_deice_type=0     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots

[Views]
eyepoint= 10.5, 0.0, -2.0


[LIGHTS]
// Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0 = 3,     1.70,   -9.00,  -4.30, fx_navred
light.1 = 3,     1.70,    9.00,  -4.30, fx_navgre
light.2 = 3,   -36.00,       0,   2.05, fx_navwhi
light.3 = 2,     1.70,   -9.00,  -4.30, fx_strobe
light.4 = 2,     1.70,    9.00,  -4.30, fx_strobe


[contact_points]
point.0=1.00, -24.75,  0.00, -11.180, 2600.80,  0.0,   50.7,   50.0,   0.51, 3.0, 0.50, 5.0, 5.5, 0.0,  240.00,  240.00
point.1=1.00, 5.00,-6.25, -11.340,   3000.80, 1.00,   1.9,  0.00,  0.50,  3.0, 0.60, 5.5, 5.0, 2.0,  240.00,  240.00
point.2=1.00, 5.00, 6.25, -11.340,   3000.80,  2.00,  1.9,  0.00,  0.50,  3.0, 0.60, 6.0, 6.0, 3.0,  240.00,  240.00
point.3=2.000000,-18.083333,-15.583333,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-18.083333,15.583333,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-24.250000,0.000000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,26.750000,0.000000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=5, 0.0, 0.0, 0.0, 0, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 1.0, 1.2, 0, 0.0, 0.0
static_pitch=0
static_cg_height=11.4
gear_system_type=0


[WEIGHT_AND_BALANCE]
max_gross_weight = 1340                          // (pounds)
empty_weight = 726                             // (pounds)

reference_datum_position     =  0.0,  0.0, 0.0   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  0.0,  0.0, 0.0   // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 3

station_load.0="18,   0.0, 0.0,  0.0,  weapon chief"               //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="18,   0.0, 0.0,  0.0,  pilot"                  //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="374,  0.0, 0.0,  0.0,  weapons"                  //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI   =  6000
empty_weight_roll_MOI    =  4000
empty_weight_yaw_MOI     = 10000
empty_weight_coupled_MOI =     0


[fuel]
Center1=0.000,  0.00, 0.000, 30.000,   0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
engine_driven_pump=0


[Helicopter]
reference_length=40.58
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


[fuselage_aerodynamics]
drag_force_cf=0.55
side_drag_force_cf=10.0
pitch_damp_cf=-2.0
roll_damp_cf=-2.0
yaw_damp_cf=-0.1
yaw_stability_cf=0.27

[MainRotor]
Position=0, 0, 0                       //Longitudinal, Lateral, Vertical feet from datum
Radius=18.583                               //feet
max_disc_angle=5.0
RatedRpm=210
Number_of_blades=4
Weight_per_blade=2.0
Weight_to_moi_factor=.5
inflow_vel_reference=34.0


[SecondaryRotor]
Position=-22.8, -0.74, 1.8                    //Longitudinal, Lateral, Vertical feet from datum
TailRotor=1
Radius=3.75       


[GeneralEngineData]
engine_type=0                                 
Engine.0=0.0, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=2                           //Fuel flow scalar
min_throttle_limit=0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 90.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 1685                               //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0                                //Max design manifold pressure, (inHg)
min_design_mp= 0                                //Min design manifold pressure, (inHg)
critical_altitude= 0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction