//Original work by:
//Barry Blaisdell
//Pavel Toman
//Bob May
//DAY Motor Glider ver 1.7 Copyright (c) 2004
//Premier Aircraft Design
//Day Flyer
[fltsim.0]
title=Katana HK36 OE-KHK
sim=HK36_TTC
model=
panel=
sound=
texture=OE-KHK
kb_checklists=HK36_check
kb_reference=HK36_ref
ui_manufacturer=Diamond Aircraft
ui_type=HK36
ui_variation=HK36 Dimona Day Flyer OE-KHK

description=Diamond Katana HK36TTC 115 Super Dimona\n2 Seat Motor Glider\nVisit us at Premier Aircraft Design\nwww.flightsimnetwork.com/premaircraft\nCopyright 2004.
atc_heavy=0
atc_id=OE-KHK
atc_airline=
atc_flight_number=

[fltsim.1]
title=Katana HK36 OK-ANU
sim=HK36_TTC
model=ANU
panel=
sound=
texture=OK-ANU
kb_checklists=HK36_check
kb_reference=HK36_ref
ui_manufacturer=Diamond Aircraft
ui_type=HK36
ui_variation=HK36 Dimona Day Flyer OK-ANU_tow hook_mirror

description=Diamond Katana HK36TTC 115 Super Dimona\n2 Seat Motor Glider\nVisit us at Premier Aircraft Design\nwww.flightsimnetwork.com/premaircraft\nCopyright 2004.

atc_heavy=0
atc_id=OK-ANU
atc_airline=
atc_flight_number=

[General]
performance=Length: 23ft - 6in\nWing Span: 54ft - 6in\nHeight: 5ft -  9in\nWeight: 1189lbs Empty\nPower: Bombardier Rotax 914 F3, 115 HP\n4 Cyl, Turbo charged\nModel & Master Textures by Pavel Toman\nTech Assist - Panels/VC - Check/Ref lists,\nFlight Dynamics by Barry Blaisdell.
atc_type=KATANA 
atc_model= 
editable=1 
visual_damage=0

[Views]
eyepoint=0.014, -0.80, 1.26   //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]
max_gross_weight = 1698
empty_weight = 1189
reference_datum_position = 0, 0, 0
//Moments of Inertia
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 2750
empty_weight_roll_MOI = 2300
empty_weight_yaw_MOI = 2500
empty_weight_coupled_MOI = 0
station_load.0= 170.000, 0.000, 0.000, 0.000

max_number_of_stations =3

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.1
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.1
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=1,  -14.85, 0.00,  3.85, fx_HK36beacon ,

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar =1.000000
engine.0 = 94.966667,0.000000,0.000000
min_throttle_limit=0.02000


[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
Center1 = 0, 0, 0, 22, 0
electric_pump=1

        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)
[contact_points]
static_pitch = -1.000
static_cg_height = 3.000
max_number_of_points = 10

point.0 = 1.000, 4.083, 0.000, -3.450, 1181.102, 0.000, 0.509, 35.940, 0.123, 2.500, 0.683, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.417, -4.500, -3.800, 1574.803, 1.000, 0.509, 0.000, 0.334, 2.500, 0.835, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, -1.417, 4.500, -3.800, 1574.803, 2.000, 0.509, 0.000, 0.334, 2.500, 0.835, 0.000, 0.000, 3.000, 0.000, 0.000
point.3 = 2.00,0.00,-17.916667,2.083333,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.4 = 2.00,0.00,17.916667,2.083333,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00
point.5 = 2.00,-16.333333,0.00,0.833333,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.6 = 2.00,2.416667,0.00,-2.166667,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.7 = 2.00,-16.333333,0.00,6.833333,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,7.00,0.00,0.00
point.8 = 2.00,-1.00,0.00,-1.833333,787.401575,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,8.00,0.00,0.00

[keyboard_response]
elevator = 100.000000, 180.000000
aileron = 200.000000, 1000.000000
rudder = 200.000000, 1000.000000

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
wing_area = 165.000000
wing_span = 54.500000
wing_root_chord =4.900
wing_dihedral = 1.735840
wing_incidence = .906372
wing_twist = -2.999268
oswald_efficiency_factor = 0.699632
wing_winglets_flag = 1
wing_sweep = 0.000000
wing_pos_apex_lon = 0.000000
wing_pos_apex_vert = 0.000000
htail_area = 39.000000
htail_span = 11.666667
htail_pos_lon = -6.333333
htail_pos_vert = 0.000000
htail_incidence = 3.246460
htail_sweep = 0.000000
vtail_area = 18.000000
vtail_span = 4.837355
vtail_sweep = 0.000000
vtail_pos_lon = -12.583333
vtail_pos_vert = 1.500000
elevator_area = 16.610000
aileron_area = 18.300000
rudder_area = 6.650000
elevator_up_limit = 28.000447
elevator_down_limit = 20.998903
aileron_up_limit = 19.996227
aileron_down_limit = 15.000035
rudder_limit = 23.995472
elevator_trim_limit = 20.497754
spoiler_limit           = 70.0                  //Degrees
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0

[electrical]
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
autopilot          = 0, 5 , 1.0
avionics_bus       = 0, 10, 10.0
avionics           = 1, 5 , 10.0
fuel_pump          = 0, 5 , 1.0
light_nav          = 0, 5 , 1.0
light_beacon       = 0, 5 , 1.0
light_landing      = 0, 5 , 7.0
light_strobe       = 0, 5 ,1.0
light_panel        = 0, 5 , 1.0
pitot_heat         = 0, 15, 1.0
additional_system  = 0, 20, 1.0
starter1           = 0, 20, 1.0
hydraulic_pump     = 0, 2,  1.0
fuel_transfer_pump = 0, 5,  1.0
max_battery_voltage=36.0
generator_alternator_voltage=36.0
max_generator_alternator_amps=160.0
electric_always_available=0


[Flaps.0]
type=1
span-outboard=0.000000
extending-time=0.000000
system_type=0
flaps-position.0=0.000000,0.000000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.00000 
idle_rpm_friction_scalar=1.000
cylinder_displacement=84.000000 
compression_ratio=8.500000 
number_of_cylinders=4
max_rated_rpm=2400.000000 
max_rated_hp=115.000000 
fuel_metering_type=0 
cooling_type=1 
normalized_starter_torque=0.380000 
turbocharged=1
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=18000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=1
auto_ignition=0

[propeller]
propeller_type=0 
propeller_diameter=6.900
propeller_blades=2 
propeller_moi=6.668472 
beta_max=35.00000
beta_min=10.000000 
min_gov_rpm=1400.000000 
prop_tc=0.100000 
gear_reduction_ratio=1.000000 
fixed_pitch_beta=20.000000 
low_speed_theory_limit=80.000000 
prop_sync_available=0 
prop_deice_available=0 
prop_feathering_available=1
prop_auto_feathering_available=0 
min_rpm_for_feather=500.000000 
beta_feather=3.000000 
power_absorbed_cf=0.000000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0.000000 
minimum_reverse_beta=0.000000 

[Reference Speeds]
flaps_up_stall_speed=35.000000 
full_flaps_stall_speed=35.00000
cruise_speed=106.516643 
max_indicated_speed=141.000000

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.000000 
autothrottle_available=0 
use_no_default_bank=1
use_no_default_pitch=1
pitch_takeoff_ga=8.000000 
default_pitch_mode=0
default_bank_mode=0
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

[direction_indicators]
direction_indicator.0=1,0 

[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

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=15.996982
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0