//Version 6_2
[fltsim.0]
title=de Havilland DH104 Sea Devon
sim=DH104_BW6_2
model=
panel=
sound=
texture=XJ348
kb_checklists=DH104_check
kb_reference=DH104_ref_2
ui_manufacturer=de Havilland
ui_type=DH-104 Dove
ui_variation=Sea Devon C.Mk 20
atc_heavy=0
atc_id=XJ348
atc_airline=NAVY
atc_flight_number=348
description=Sea Devon C.20 XJ348 c/n 04406, 781 Royal Naval Air Squadron.

[fltsim.1]
title=de Havilland DH104 British Eagle
sim=DH104_BW6_2
model=1
panel=
sound=
texture=BE
kb_checklists=DH104_check
kb_reference=DH104_ref_2
ui_manufacturer=de Havilland
ui_type=DH-104 Dove
ui_variation=DH-104 Dove British Eagle
atc_heavy=0
atc_id=G-AROI
atc_airline=British Eagle
atc_flight_number=GAROI
description=c/n 04474,  G-AROI British Eagle


[fltsim.2]
title=de Havilland DH104 Channel Airways
sim=DH104_BW6_2
model=2
panel=
sound=
texture=CA
kb_checklists=DH104_check
kb_reference=DH104_ref_2
ui_manufacturer=de Havilland
ui_type=DH-104 Dove
ui_variation=DH-104 Dove Channel Airways
atc_heavy=0
atc_id=G-ANVU
atc_airline=Channel
atc_flight_number=GANVU
description=G-ANVU Channel Airways


[General]
atc_type=DeHavilland
atc_model=Dove
performance=Cruise Speed\n160 kts  296 km/hr\n\nEngine\nde Havilland Gypsy Queen 70-2 380 hp\n\nPropeller\nThree-bladed de Havilland constant-speed, variable pitch\n\nMaximum Range\n1000 mls      \n\nService Ceiling\n20,000 ft \n\nFuel Capacity\n202 US gal\n\nMaximum Gross Weight\n8,800 lb          3,995 kg\n\nLength\n29 ft, 10 in 9.09 m\n\nWingspan\n37 ft, 10 in 11.53 m\n\nHeight\n9 ft, 9 in              2.97 m\n\nSeating  Up to 10\n\nUseful Load\n1,860 lb   844 kg
prop_anim_ratio=.50


[WEIGHT_AND_BALANCE]
max_gross_weight = 8800.000
empty_weight = 5725.000

reference_datum_position     =  0.0, 0.0, 0.0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -1.5, 0.0, 0.0

max_number_of_stations = 11
station_load.0 = 170, 4.18, -1.04, 1.06, Pilot
station_load.1 = 170, 4.18, 1.04, 1.06, Co-pilot
station_load.2 = 170, 1.2, -1.2, 1.06, Passenger
station_load.3 = 170, 1.2, 1.2, 1.06, Passenger
station_load.4 = 170, -1.3, -1.2, 1.06, Passenger
station_load.5 = 170, -1.3, 1.2, 1.06, Passenger
station_load.6 = 170, -3.5, -1.2, 1.06, Passenger
station_load.7 = 170, -3.5, 1.2, 1.06, Passenger
station_load.8 = 0, -5.8, -1.2, 1.06, Passenger
station_load.9 = 0, -5.8, -1.2, 1.06, Passenger
station_load.10 = 140, -8, 0, 0, Baggage

;Moments of Inertia
empty_weight_pitch_MOI = 7958
empty_weight_roll_MOI = 9131
empty_weight_yaw_MOI = 15900
empty_weight_coupled_MOI = 0

CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 0
Engine.0 = 6.800, -6.470, 0.000
Engine.1 = 6.800, 6.470, 0.000
fuel_flow_scalar= 1.1
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]           //Based on Gypsy Queen 70-2
power_scalar =1.000
cylinder_displacement= 103.67
compression_ratio= 6.500
number_of_cylinders= 6
max_rated_rpm= 2980.000
max_rated_hp= 380.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.295
turbocharged= 1
max_design_mp= 45.000
min_design_mp= 7.000
critical_altitude= 4400.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 1
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
rotation= -1,-1
thrust_scalar =1.000
propeller_type= 0
propeller_diameter= 7.5
propeller_blades= 3
propeller_moi=6.1
beta_max= 65.0
beta_min= 18.6    
min_gov_rpm= 600
prop_tc= 0.006
gear_reduction_ratio= 1.4
fixed_pitch_beta= 25.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 88.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0 
prop_reverse_available= 0.000
minimum_on_ground_beta= 1.000
minimum_reverse_beta= 0.000

[contact_points]
//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
        //14 Airspeed limit for retraction (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1.000, 11.2129, 0.000, -5.15, 1600.000, 0.000, 0.8, 60.000, 0.08, 2.500, 0.850, 3.000, 3.000, 0.0, 152.000, 180.000
point.1 = 1.000, -2.1117, -6.789, -4.98, 1600.000, 1.000, 1.080, 0.000, 0.20, 2.500, 0.850, 4.100, 4.300, 2.0, 152.000, 200.000
point.2 = 1.000, -2.1117, 6.789, -4.98, 1600.000, 2.000, 1.080, 0.000, 0.20, 2.500, 0.850, 4.300, 4.100, 3.0, 152.000, 200.000
//SCRAPES
point.3 = 2, -26.443, -0.009,  1.362, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.4 = 2, 12.718, 0.000,  -1.421, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.5 = 2, -1.370, -28.053,  0.769, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.6 = 2, -1.370, 28.053,  0.769, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
static_pitch     = 0.99         //degrees (pitch when loaded on ground)
static_cg_height=5.01         //feet, altitude of CG when at rest on the ground
gear_system_type=1             //Hydraulic//Pneumatic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  10.0     //Flap angle that activates warning at idle
flap_limit_power   = 31.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.45  //Brake scalar
differential_braking_scale = 0.8  //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 475.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[electrical]
max_battery_voltage = 24.0
engine_generator_map=1,1
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
electric_always_available = 0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 10, 17.0
pitot_heat         = 0, 5 , 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
starter2           = 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
light_cabin        = 0, 5 , 17.0

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI

[exits]
number_of_exits = 1
exit_rate.0 = 0.4                               ;Percent per second

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Com.2         = 0, 0
Nav.1         = 1, 0, 1
Nav.2         = 1, 0, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[Views]
eyepoint = 4.3, -0.86, 3.35    //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 1, -0.69, 0.00, -2.4, fx_beacon,
light.2 = 1, -9.35, 0.00, 3.8, fx_beacon,
light.3 = 4, 4.3, 0.0, 2.5, fx_vclight,
light.4 = 4, 0.0, 0.0, 3.0, fx_vclight,
light.5 = 4, -4.0, 0.0, 3.0, fx_vclight,
light.6 = 4, -9.0, 0.0, 2.8, fx_vclight, 

[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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 = 2 

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

[fuel]
LeftMain = -0.4,-4,-1,101.05,2.4
RightMain = -0.4, 4,-1,101.05,2.4
fuel_type =  1
number_of_tank_selectors = 2
electric_pump=1

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

[airplane_geometry]
wing_area               = 335.000
wing_span               = 57.000
wing_root_chord         = 8.660
wing_dihedral           = 6.000
wing_incidence          = 0
wing_twist              = 0
oswald_efficiency_factor= 0.8776
wing_winglets_flag      = 0
wing_sweep              = 0.0
wing_pos_apex_lon       = 2.165
wing_pos_apex_vert      = 1.41
htail_area              = 37.6
htail_span              = 17.66
htail_pos_lon           = -20.480
htail_pos_vert          = 1.760
htail_incidence         = 0.000
htail_sweep             = 0
vtail_area              = 19.03
vtail_span              = 8.600
vtail_sweep             = 0
vtail_pos_lon           = -22.0
vtail_pos_vert          = 3.450
elevator_area           = 25.190
aileron_area            = 22.46
rudder_area             = 16.990
elevator_up_limit       = 27.000
elevator_down_limit     = 14.000
aileron_up_limit        = 21.200
aileron_down_limit      = 18.800
rudder_limit            = 25.000
elevator_trim_limit     = 20.000
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    = 65.0
full_flaps_stall_speed  = 55.0
cruise_speed            = 160.0
max_indicated_speed     = 206.0      //Red line (KIAS)
max_mach = 0.51

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 900.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0

[stall_warning]
type=2

[Flaps.0]
type= 1
span-outboard= 0.550
extending-time= 7.000
system_type= 1
damaging-speed= 152.000
blowout-speed= 182.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 60.000, 0.000

[folding_wings]
wing_fold_system_type =  4
fold_rates =  0.12, 0.11

[TailHook]
tailhook_length = 4
tailhook_position = -15, 0, -1
cable_force_adjust = 1

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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=2500000                 ; in microseconds