[fltsim.0]
title=DH80A Puss Moth Skis Version
sim=DH80
model=ski
panel=silver
sound=
texture=wh
kb_checklists=
atc_id=VH-UQO  
ui_manufacturer=De Havilland
ui_type=DH80 Puss Moth
ui_variation=C-CYBA 
description=Black w/Skis
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[General]
atc_type=De Havilland 
atc_model=DH80 
editable=1 
performance=Maximum Speed\n125 mph    108 kts\t137 km\/hr\nEngine\nDe Havilland Gypsy Major 130-hp air cooled\n\n 
Category=airplane

[weight_and_balance]

// ACM V2.5
max_gross_weight = 2050
empty_weight = 1265
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.5, 0, 0
empty_weight_pitch_MOI = 1400
empty_weight_roll_MOI = 1137
empty_weight_yaw_MOI = 2360
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 3

station_load.0 = 170.000000, 0.0000, 0.000000, 0.000000, Pilot
station_load.1 = 150, -2.4, 0, 0
station_load.2 = 20.000000, -4.400000, 0.000000, 0.000000, Baggage


[lights]

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

light.0 = 3,  -1.88, -18.11, 1.90, fx_navred
light.1 = 3,  -1.88,  18.11, 1.90, fx_navgre
light.2 = 4,  -2.27,   0.00, -1.0, fx_vclight_dh80

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.000
min_throttle_limit = 0.0
engine.0 = 6.338, 0.000, 0.000

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_dh80
windshield_rain_effect_available = 1


[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1


//----- 436 miles tanks -----//

LeftMain = 0, -2.1, 1.5, 26.5, 0
RightMain = 0, 2.1, 1.5, 26.5, 0


//----- 570 miles tanks -----//
//range 285 miles/tank = 570 miles

//LeftMain = 0, -2.1, 1.5, 34.5, 0
//RightMain = 0, 2.1, 1.5, 34.5, 0


//----- 700 miles tanks -----//
//range 350 miles/tank = 700 miles

//LeftMain = 0, -2.1, 1.5, 42.5, 0
//RightMain = 0, 2.1, 1.5, 42.5, 0


//----- 1300 miles tanks -----//
//range 650 miles/tank = 1300 miles

//LeftMain = 0, -2.1, 1.5, 80, 0
//RightMain = 0, 2.1, 1.5, 80, 0


[contact_points]
static_pitch = 10.45
static_cg_height = 3.9
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 8


//If you prefer a steerable tailwheel, remove the // from the next line ... and put a // in front of the next point.0 line.
//point.0 = 1, -16.778, 0, -1.05, 2200, 0, 0.238, 180, 0.2, 3, 0.8, 0, 0, 0, 0, 0  // for castoring tailwheel
point.0 = 1, -16.778, 0, -1.05, 2200, 0, 0.238,  35, 0.2, 3, 0.8, 0, 0, 0, 0, 0    //for stearable tailwheel
point.1 = 2, -5, 0, -2, 600, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.2 = 1, 1.55, -3.53, -4.59, 1600, 1, 0.728, 0, 0.55, 1.5, 0.9, 0, 0, 2, 0, 0
point.3 = 1, 1.55,  3.53, -4.59, 1600, 2, 0.728, 0, 0.55, 1.5, 0.9, 0, 0, 3, 0, 0
point.4 = 2.000, -1.000, -18.250, 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.5 = 2.000, -1.000,  18.250, 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.6 = 2.000, -17.85,  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.7 = 2.000,  6.150, 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


[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000


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

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.6002,0.6222,0.6222,0.0326,1.5528,1.2445,1.2445
//ACM_AREAW2// 0.0652,1.5054,1.8668,1.8668,0.0978,1.4580,2.4891,2.4891,0.1304,1.4106
//ACM_AREAW3// 3.1115,3.1115,0.1630,1.3632,3.7337,3.7337,0.1956,1.3158,4.3561,4.3561
//ACM_AREAW4// 0.2282,1.2684,4.9783,4.9783,0.2609,1.2210,5.6006,5.6006,0.2935,1.1736
//ACM_AREAH1// 0,0,0,0.9753,0.1625,0.1625,0.0938,1.0204,0.3251,0.3251
//ACM_AREAH2// 0.1877,1.0655,0.4876,0.4876,0.2815,1.1106,0.6502,0.6502,0.3754,1.1557
//ACM_AREAH3// 0.8128,0.8128,0.4692,1.2007,0.9753,0.9753,0.5631,1.2458,1.1379,1.1379
//ACM_AREAH4// 0.6569,1.2909,1.3004,1.3004,0.7508,1.3360,1.4630,1.4630,0.8446,1.3811
//ACM_AREAV1// 0,0,0,1.3533,0.1503,0.1503,0.1174,1.3625,0.3007,0.3007
//ACM_AREAV2// 0.2349,1.3717,0.4511,0.4511,0.3524,1.3809,0.6014,0.6014,0.4699,1.3901
//ACM_AREAV3// 0.7518,0.7518,0.5874,1.3993,0.9022,0.9022,0.7048,1.4086,1.0525,1.0525
//ACM_AREAV4// 0.8223,1.4178,1.2029,1.2029,0.9398,1.4270,1.3533,1.3533,1.0573,1.4362
//ACM_CAREAW1// 2.8003,2.8003,0.9468,1.2669,3.1115,3.1115,0.9631,1.2672,3.4226,3.4226
//ACM_CAREAW2// 0.9794,1.2675,3.7337,3.7337,0.9957,1.2678,4.0449,4.0449,1.0120,1.2681
//ACM_CAREAW3// 4.3561,4.3561,1.0283,1.2684,4.6672,4.6672,1.0447,1.2687,4.9783,4.9783
//ACM_CAREAW4// 1.0610,1.2690,5.2895,5.2895,1.0773,1.2693,5.6006,5.6006,1.0936,1.2696
//ACM_CAREAH1// 0,0,0.4876,0.9753,0.1625,0.1625,0.5815,1.0448,0.3251,0.3251
//ACM_CAREAH2// 0.6753,1.1143,0.4876,0.4876,0.7692,1.1837,0.6502,0.6502,0.8630,1.2532
//ACM_CAREAH3// 0.8128,0.8128,0.9569,1.3227,0.9753,0.9753,1.0508,1.3921,1.1379,1.1379
//ACM_CAREAH4// 1.1446,1.4616,1.3004,1.3004,1.2385,1.5311,1.4630,1.4630,1.3323,1.6005
//ACM_CAREAV1// 0,0,0.3383,1.0149,0.1503,0.1503,0.4558,1.0783,0.3007,0.3007
//ACM_CAREAV2// 0.5732,1.1416,0.4511,0.4511,0.6907,1.2050,0.6014,0.6014,0.8082,1.2683
//ACM_CAREAV3// 0.7518,0.7518,0.9257,1.3317,0.9022,0.9022,1.0432,1.3950,1.0525,1.0525
//ACM_CAREAV4// 1.1606,1.4584,1.2029,1.2029,1.2781,1.5217,1.3533,1.3533,1.3956,1.5851
wing_area = 222
wing_span = 36.75
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 = 3.000
wing_pos_apex_lon = 1.95
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 = 12.8
aileron_area = 27.0
rudder_area = 7.30
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 = 15.000
spoiler_limit = 180.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[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=0.5  //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          = 0.0  //0.3
torque_on_roll           = 0.3
gyro_precession_on_yaw   = 0.3
gyro_precession_on_pitch = 0.3

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=92.750 
compression_ratio=5.25 
number_of_cylinders=4 
max_rated_rpm=2350 
max_rated_hp=130.000 
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=3000 
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 
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=23.750 
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 
rotation = -1
        //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

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.3  //Brake scalar - If you use a castoring tailwheel, you may want to increase this to .6
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=-0.500, 0.000, 1.18 

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

[folding_wings]
wing_fold_system_type = 1
fold_rates = 0.12, 0.11


[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
[Reference Speeds]
flaps_up_stall_speed=43.000 
full_flaps_stall_speed=43.000 
cruise_speed=108.000 
max_indicated_speed     = 128                   //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

[stall_warning]
type=1
stick_shaker=0
[Flaps.0]
type= 1
span-outboard= 0.5
extending-time= 2.000
damaging-speed= 160.000
blowout-speed= 180.000
lift_scalar= -0.0
drag_scalar= 1.0  ////Changed
pitch_scalar= 0.3
//flaps-position.0= 0.000, 0.000
flaps-position.0=0.00
flaps-position.1=35.00
flaps-position.2=55.00
flaps-position.3=85.00
system_type = 3

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0.