[fltsim.0]
title=Hughes_269C_red
sim=hughes
model=
panel=
sound=
texture=red
prop_anim_ratio=-1.2
atc_id_color=
atc_id=N332DW
ui_manufacturer="Hughes"
ui_type="269C"
ui_variation="Red"
ui_typerole="Rotorcraft"
ui_createdby="Bruce Fitzgerald"
description=

[fltsim.1]
title=Hughes_269C_blue
sim=hughes
model=
panel=
sound=
texture=bu
prop_anim_ratio=-1.2
atc_id_color=
atc_id=N322DW
ui_manufacturer="Hughes"
ui_type="269C"
ui_variation="Blue"
ui_typerole="Rotorcraft"
ui_createdby="Bruce Fitzgerald"
description=

[fltsim.2]
title=Hughes_269C_white
sim=hughes
model=
panel=
sound=
texture=whi
prop_anim_ratio=-1.2
atc_id_color=
atc_id=N233DW
ui_manufacturer="Hughes"
ui_type="269C"
ui_variation="white"
ui_typerole="Rotorcraft"
ui_createdby="Bruce Fitzgerald"
description=

[General]
atc_type=Hughes
atc_model=269C
performance=
editable=1
Category = Helicopter

[CameraDefinition.0]
Title = "Chase"
Guid = {4B3CBC7C-B252-374A-8E16-07927ACFFB52}
Description = Just off the tail looking forward
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 0.0, 3.0, -18.0
InitialPbh = 12, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[Reference Speeds]
flaps_up_stall_speed=54.000000 
full_flaps_stall_speed=43.200000 
cruise_speed=98.000000 
max_indicated_speed=135.000000

[weight_and_balance]
max_gross_weight = 3150
empty_weight = 1900
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 1, 0, 0
empty_weight_pitch_MOI = 9000
empty_weight_roll_MOI = 9000
empty_weight_yaw_MOI = 19000
empty_weight_coupled_MOI = 0
max_number_of_stations = 1
station_load.0 = 0.000, 0.000, 0.000, 0.000

[fuel]
LeftMain  = -2.85, -0.5, 3.0, 16.5, 0.0         //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -2.85,  0.5, 3.0, 16.5, 0.0         //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1
engine_driven_pump=1

[contact_points]
//0  Class
//1  Longitudinal Position 
//2  Lateral Position
//3  Vertical Position 
//4  Impact Damage Threshold
//5  Brake Map (0=None, 1=Left, 2=Right)
//6  Wheel Radius
//7  Steer Angle
//8  Static Compression
//9  Max/Static Compression Ratio
//10 Damping Ratio
//11 Extension Time
//12 Retraction Time
//13 Sound Type
//14 Damage speed
//15 Fail speed
point.0 = 1, -2.06,  -3.7, -4.98, 3000, 1, 0.2, 0, 0.3, 1.5, 0.728, 0, 0, 2, 0, 0
point.1 = 1,       6,  -3.7, -4.98, 3000, 0, 0.2, 0, 0.3, 1.5, 0.728, 0, 0, 7, 0, 0
point.2 = 1,       6,   3.7, -4.98, 3000, 0, 0.2, 0, 0.3, 1.5, 0.728, 0, 0, 7, 0, 0
point.3 = 1, -2.06,   3.7, -4.98, 3000, 2, 0.2, 0, 0.3, 1.5, 0.728, 0, 0, 3, 0, 0
point.4 = 2, -15.7, 0.00, -2.95,      0, 0,    0, 0,    0,    0,       0, 0, 0, 9, 0, 0

static_pitch = 0
static_cg_height = 4.69
max_number_of_points = 6

[brakes]
toe_brakes_scale=2.00
parking_brake=1

[Views]
eyepoint=1.7, 1.0, 1.8 

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,    6.9,  -3.3,  -4.2,  fx_navred
light.1 = 3,    6.9,   3.3,  -4.2,  fx_navgre
light.2 = 3, -15.0,   2.3,   2.1,  fx_navwhi
light.3 = 2,   -7.55,   0.0,   0.7,  fx_beacon
light.4 = 4,    3.6,   0.0,   1.7,  fx_vclightwhi

[smokesystem]
// none

[effects]
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
landrotorwash = fx_rtr_lnd
waterrotorwash = fx_rtr_wtr

[exits]
//(0=Main 1=Cargo 2=Emergency)
number_of_exits = 2
exit.0 = 0.4 
exit.1 = 0.4 // 

[Flight_tuning]
parasite_drag_scalar       = 14.0
induced_drag_scalar        = 5.0

[Helicopter]
low_realism_stability_scale = 1.0, 1.0, 1.0
reference_length=20.000000
reference_frontal_area=50.000000
reference_side_area=70.000000
side_aero_center=-0.000000
lift_aero_center=-0.000000
right_trim_scalar=1.000000
correlator_available=1.000000
governed_pct_rpm_ref=1.000000
rotor_brake_scalar=1.000000
torque_scalar=1.000000
tail_rotor_translating_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      = 0.2
side_drag_force_cf = 1.0
pitch_damp_cf      = -2.0
roll_damp_cf       = -2.0
yaw_damp_cf        = -1.0
yaw_stability_cf   = 0.57
pitch_stability_cf=0.000000

[MainRotor]
number_of_blades=3.000000
weight_per_blade=0.000000
weight_to_moi_factor=0.577000
inflow_vel_reference=0.000000

[SecondaryRotor]
number_of_blades=2.000000
weight_per_blade=0.000000
weight_to_moi_factor=0.577000
inflow_vel_reference=0.000000

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.5, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //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= 2500                             //Max rated RPM
max_rated_hp= 150                               //Max rated HP
fuel_metering_type= 0                           //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= 1                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 1                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 0.8      //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 0.9      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 0.9                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 0.8                  //Scalar on idle RPM friction
magneto_order_left_right_both = 1		//sets the order of the magneto switch direction

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 1

[hydraulic_system]
normal_pressure=0.000000
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[autopilot]
autopilot_available=0 
flight_director_available=0 
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[direction_indicators]
direction_indicator.0=3,0 
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000