[fltsim.0]
title=De Havilland Hornet Moth
sim=DH Hornet Moth
model=
panel=
sound=
texture=
kb_checklists=

atc_id=G-ADNE
ui_manufacturer=De Havilland
ui_type=DH87 Hornet Moth
ui_variation=G-ADNE
atc_heavy=0
atc_airline=
atc_flight_number=
description=Two seat Touring Aircraft

[General]
atc_type=De Havilland
atc_model=DH87
editable=1
performance=Maximum Speed\n165 mph    144 kts\t137 km\/hr\nEngine\nDe Havilland Gypsy Major 130-hp air cooled\n\n




[WEIGHT_AND_BALANCE]
max_gross_weight = 2820.000
empty_weight = 1880.000

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 =170.000000, -3.250000, 0.000000, 0.000000, Pilot       //W 
station_load.1 =0.000000, -0.750000, 0.000000, 0.000000, Passenger   //W 
station_load.2 =20.000000, -4.400000, 0.000000, 0.000000, Baggage     //W 
;Moments of Inertia
empty_weight_pitch_MOI  = 1400.000
empty_weight_roll_MOI   = 1137.000
empty_weight_yaw_MOI    = 2360.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000




[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
p_factor_on_yaw          = 0.3
torque_on_roll           = 0.3
gyro_precession_on_yaw   = 0.3
gyro_precession_on_pitch = 0.3



[GeneralEngineData]
engine_type = 0
Engine.0 = 2.800, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser



[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 92.750
compression_ratio= 8.500
number_of_cylinders= 4
max_rated_rpm= 2900.000
max_rated_hp= 165.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
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



[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 1
propeller_diameter= 6.000
propeller_blades= 2
propeller_moi= 3.780
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 0.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 13.750
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0 
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000


        //0  Class
        //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




[contact_points]
point.0= 1.000, -16.600, 0.000, -1.590, 1200.000, 0.000, 0.238, 60.000, 0.300, 2.500, 0.200, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 1.240, -3.000, -5.400, 1600.000, 1.000, 0.728, 0.000, 0.540, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 1.240, 3.000, -5.400, 1600.000, 2.000, 0.728, 0.000, 0.540, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -1.000, -18.700, 1.800, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -1.000, 18.700, 1.800, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -16.400, 0.000, 4.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 5.400, 0.000, -2.200, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = 12.300
static_cg_height = 3.900



[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.5  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected



[hydraulic_system]
normal_pressure = 0.0    //PSI



[Views]
eyepoint =-0.894, -0.710, 1.180


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0 = 3,  -1.08, -16.11, 2.85, fx_navred
light.1 = 3,  -1.08,  16.11, 2.85, fx_navgre
light.2 = 4,  -2.27,   0.00, 1.45, fx_vclight


[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.
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=1,0



[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 =1,1



[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_cub
touchdown=fx_tchdwn_s, 1



[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




[fuel]
LeftMain  = -3.900, -2.100, 2.500, 26.500, 0.000
RightMain = -3.900, 2.100, 2.500, 26.500, 0.000
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1




[airplane_geometry]
wing_area               = 178.500
wing_span               = 32.200
wing_root_chord         = 5.250
wing_dihedral           = 1.100
wing_incidence          = 2.500
wing_twist              = -1.000
oswald_efficiency_factor= 0.680
wing_winglets_flag      = 0
wing_sweep              = 0.000
wing_pos_apex_lon       = 1.310
wing_pos_apex_vert      = 2.100

htail_area              = 18.200
htail_span              = 9.600
htail_pos_lon           = -13.400
htail_pos_vert          = 1.300
htail_incidence         = -0.800
htail_sweep             = 30.000

vtail_area              = 13.000
vtail_span              = 4.440
vtail_sweep             = 38.000
vtail_pos_lon           = -13.500
vtail_pos_vert          = 1.600

elevator_area           = 10.640
aileron_area            = 9.600
rudder_area             = 6.550
elevator_up_limit       = 30.000
elevator_down_limit     = 20.000
aileron_up_limit        = 20.000
aileron_down_limit      = 15.000
rudder_limit            = 28.000
elevator_trim_limit     = 10.000
spoiler_limit           = 0.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000


[Reference Speeds]
flaps_up_stall_speed    = 53.000
full_flaps_stall_speed  = 43.000
cruise_speed            = 105.000
max_indicated_speed     = 166                   //Red line (KIAS)



[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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



[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=3500000                 ; in microseconds



[stall_warning]
type=1


[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 4.000
system_type= 0
damaging-speed= 160.000
blowout-speed= 180.000
lift_scalar= 0.500
drag_scalar= 1.200
pitch_scalar= 0.400
flaps-position.0= 0.000, 0.000
flaps-position.1= 80.000, 0.000