[fltsim.0]
title=KZ-2-SPORT
sim=KZ-2-SPORT
model=
panel=
sound=
texture=
kb_checklists=
description=KZ-2-SPORT made by Kramme & Zeutenfirst flown o 10 october 1938. 16 were bildt including 4 for royal danish navy. Only 1 is remaining is belonging to Danmarks Tekniske Museum and its loan aut to danich veteran museum at  Stavning Airport not longer flyable
ui_manufacturer=S.A.I.
ui_type=KZ-2-SPORT
ui_variation=OY-DOU
atc_heavy=0
atc_id=OYDOU
atc_airline=KZCLUB
atc_flight_number=

[forcefeedback]
[General]
performance=engine: 105 hp. hirth 504A\nwith 10.20 m\nlengt 7.50 m\nmax celling 5500
atc_type=oydou
atc_model=kz


[weight_and_balance]

// ACM V2.3
max_gross_weight= 2100.000
empty_weight= 1000.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
empty_weight_pitch_MOI= 5230.000
empty_weight_roll_MOI= 3492.000
empty_weight_yaw_MOI= 5931.000
empty_weight_coupled_MOI= 0.000
max_number_of_stations=5

station_load.0=170.000000, 1.300000, -1.000000, 0.000000, Pilot
station_load.1=170.000000, 1.300000, 1.000000, 0.000000, Copilot
CG_forward_limit= 0.000
CG_aft_limit= 1.000



[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type= 0
fuel_flow_scalar= 1.000
engine.0= 6.300, 0.000, 0.000
min_throttle_limit=0.000000

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

[fuel]

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

fuel_type=1
number_of_tank_selectors=1
Center1=0.000, 0.000, 0.000, 0.000, 0.000
LeftMain= 0.000, -7.500, -0.500, 16.000, 1.000

RightMain= 0.000, 7.500, -0.500, 16.000, 1.000

electric_pump=1


[contact_points]
static_pitch= 10.748
static_cg_height= 4.200
max_number_of_points=7

point.0= 1.000, -13.373, 0.000, -1.000, 1181.100, 0.000, 0.335, 33.600, 0.180, 2.500, 0.724, 3.500, 3.500, 0.000, 0.000, 0.000
point.1= 1.000, 1.480, -3.480, -4.140, 1574.800, 1.000, 0.523, 0.000, 0.380, 2.500, 0.678, 12.700, 17.700, 2.000, 0.000, 0.000
point.2= 1.000, 1.480, 3.480, -4.140, 1574.800, 2.000, 0.523, 0.000, 0.380, 2.500, 0.678, 15.200, 20.200, 3.000, 0.000, 0.000

//Scrape
point.3= 2.000, 0.700, -17.800, 0.140, 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, 0.700, 17.800, 0.140, 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, -15.100, 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, 6.100, 0.000, -2.400, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

gear_system_type=3   // 3 = manual, Pumphebel, 1 = hydraulic
tailwheel_lock=1
  

[gear_warning_system]
gear_warning_available=1    //Normal
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=0.0     //Flap angle that activates warning at idle
flap_limit_power=35.0     //Flap angle that activates warning at above idle


[keyboard_response]
elevator=350.000000, 500.000000
aileron=450.000000, 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=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[airplane_geometry]
wing_area= 176.530
wing_span= 34.830
wing_root_chord= 4.130
wing_dihedral= 5.500
wing_incidence= 0.198
wing_twist= 0.000
oswald_efficiency_factor= 0.730
wing_winglets_flag= 0
wing_sweep= 6.000
wing_pos_apex_lon= 2.160
wing_pos_apex_vert= -1.460
htail_area= 34.000
htail_span= 10.660
htail_pos_lon= -14.700
htail_pos_vert= 1.750
htail_incidence= -1.300
htail_sweep= 0.000
vtail_area= 15.000
vtail_span= 4.410
vtail_sweep= 0.000
vtail_pos_lon= -16.000
vtail_pos_vert= 1.100
elevator_area= 12.260
aileron_area= 13.900
rudder_area= 8.230
elevator_up_limit= 25.500
elevator_down_limit= 22.150
aileron_up_limit= 19.000
aileron_down_limit= 17.000
rudder_limit= 25.700
elevator_trim_limit= 20.000
spoiler_limit= 12.000
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
spoilerons_available= 0

[pitot_static]
vertical_speed_time_constant=0.48  //Increasing this value will cause a more instantaneous reaction in the VSI

[electrical]
max_battery_voltage=25
           
generator_alternator_voltage=28
max_generator_alternator_amps=60
electric_always_available=0
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

avionics_bus=0, 3 , 17.0
avionics=1, 3 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 1 , 17.0
fuel_pump=0, 3 , 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=4, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 2 , 17.0

[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
p_factor_on_yaw=0.3
torque_on_roll=1.0
gyro_precession_on_yaw=1.0
gyro_precession_on_pitch=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 

[autopilot]
autopilot_available=0
       
flight_director_available=0default_vertical_speed=700.0 
autothrottle_available=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=1.0
pitch_takeoff_ga=8.000000 

[Views]
eyepoint=-3.4130,-0.0,2.4851

[folding_wings]
wing_fold_system_type=4
fold_rates=1.040,1.039

[exits]
number_of_exits=3
exit_rate.0=0.4
exit_rate.1=0.4


[piston_engine]
// Argus As10C 8 Zylinder 240 PS max, 200 Dauerleistung
power_scalar=1.000
cylinder_displacement= 96.410
compression_ratio= 5.900
number_of_cylinders= 4
max_rated_rpm= 2000.000
max_rated_hp= 105.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.095
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=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar=1.000
propeller_type= 1
propeller_diameter= 7.700
propeller_blades= 2
propeller_moi= 8.500
beta_max= 34.000
beta_min= 15.000
min_gov_rpm= 1100.000
prop_tc= 0.030
gear_reduction_ratio= 1.000
fixed_pitch_beta= 14.000
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

[brakes]
// Differntialbremsen neu 18.05.04
toe_brakes_scale=0.6
parking_brake=1
differential_braking_scale=0.8        //Delta on the amount of brake when the rudder pedals deflected



[Reference Speeds]
flaps_up_stall_speed= 56.000
full_flaps_stall_speed= 48.000
cruise_speed= 165.000
max_indicated_speed=173.0          // entspricht 320 km/h

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=660.0

[stall_warning]
type=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=1,0 

[Flaps.0]
type= 0
span-outboard= 0.500
extending-time= 5.000
system_type= 3
damaging-speed= 115.000
blowout-speed= 125.000
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= 35.000, 0.000
flaps-position.3= 50.000, 0.000