[fltsim.0]
title=kz_7_rdaf
sim=kz_7_rdaf
model=
panel=
sound=
texture=
kb_checklists=
description=BORN 30\/7-48. sn nr:62623. Former RDAF O-623. entert service at Royal danick navy training school at avno. Transfort to RDAF in 1950.When Skydstrup Airforse Base started in 1953 the aircraft was transfort to Skydstrup, and are in 1976 belonging to Skydstrup Airforse Base Glider club It can be seen olmost every weekend taiking up gliders.
ui_manufacturer=S.A.I.
ui_type=KZ
ui_variation=ATJ
atc_heavy=0
atc_id=atj
atc_airline=rdaf
atc_flight_number=

[forcefeedback]

[General]
performance=Skandinaisk Aero Industri KZ-7 U10.LAEKE.\nengine:  Continental 145 hp c-145.\nspan  9,60 m\nlength 6,48 m\nheight 2,10 m\nweight empty 482 kg\nweight loaded 860 kg\nmax speed 200 km\/t\nnr bildt 56
atc_type=kz7
atc_model=kz

[WEIGHT_AND_BALANCE]
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=180.000000, 1.544000, 0.910000, -0.600000, Pilot
station_load.1=180.000000, 1.544000, -0.910000, -0.600000, Front Passenger

station_load.2=150.000000, 3.290000, 0.910000, -0.600000, Rear Passenger
station_load.3=150.000000, 3.290000, -0.910000, -0.600000, Rear Passenger
empty_weight= 1063.000
empty_weight_roll_MOI= 3000.000
empty_weight_pitch_MOI= 6250.000
empty_weight_yaw_MOI= 4250.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 2111.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[fuel]
LeftMain= -1.500, -4.700, 2.500, 39.600, 0.000
RightMain= -1.500, 4.700, 2.500, 39.600, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area= 139.900
wing_span= 31.000
wing_root_chord= 4.917
wing_dihedral= 1.736
wing_incidence= 1.500
wing_twist= -2.999
oswald_efficiency_factor= 0.818
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.229
wing_pos_apex_vert= 0.000
htail_area= 39.000
htail_span= 11.667
htail_pos_lon= -14.667
htail_pos_vert= 0.000
htail_incidence= 3.246
htail_sweep= 3.000
vtail_area= 18.000
vtail_span= 4.837
vtail_sweep= 10.000
vtail_pos_lon= -12.583
vtail_pos_vert= 1.500
elevator_area= 12.000
aileron_area= 16.800
rudder_area= 7.500
elevator_up_limit= 25.000
elevator_down_limit= 23.000
aileron_up_limit= 20.000
aileron_down_limit= 15.000
rudder_limit= 24.000
elevator_trim_limit= 20.500
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

[GeneralEngineData]
engine_type= 0
Engine.0= 4.500, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement= 87.000
compression_ratio= 8.500
number_of_cylinders= 6
max_rated_rpm= 2000.000
max_rated_hp= 145.000
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
fuel_flow_scalar=1.000
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
power_scalar=1.000

[propeller]
propeller_type= 1
propeller_diameter= 6.380
propeller_blades= 2
propeller_moi= 5.700
beta_max= 39.000
beta_min= 11.000
min_gov_rpm= 1400.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 20.000
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
thrust_scalar=1.000

[Reference Speeds]
flaps_up_stall_speed= 54.000
full_flaps_stall_speed= 43.200
cruise_speed= 133.831
max_indicated_speed=170.000000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=-1.681289,-0.973999,1.230315

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

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

[exits]

number_of_exits=3

[folding_wings]
wing_fold_system_type=4
                      
fold_rates=1.040,1.039
          

[contact_points]
point.0= 1.000, -15.503, 0.000, -1.388, 3500.000, 0.000, 0.519, 42.900, 0.191, 2.500, 1.082, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 1.151, -4.000, -5.055, 3500.000, 1.000, 0.519, 0.000, 0.569, 2.500, 0.626, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 1.151, 4.000, -5.055, 3500.000, 2.000, 0.519, 0.000, 0.569, 2.500, 0.626, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 1.083, -18.000, 3.667, 1573.938, 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, 1.083, 18.000, 3.667, 1573.938, 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, -18.333, 0.000, 0.167, 1573.938, 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, 7.250, 0.000, -1.667, 1573.938, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 8.370
static_cg_height= 5.055

[brakes]
toe_brakes_scale=0.671407
parking_brake=1

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 180.000
blowout-speed= 230.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.500, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 40.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.500
extending-time= 0.100
system_type= 4
damaging-speed= 180.000
blowout-speed= 230.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 0.000, 0.000