[fltsim.0] JABIndex=1 title=Wilga-35 Moving Parts #1 sim=wilga-m2k2 model= panel= sound= texture= checklists= kb_checklists=Wilga-M_CHECK kb_reference=Wilga-M_ref atc_type=PZL atc_id_enable=1 atc_id=M100 atc_id_color=0xff000000 description=Notes: Designed by H.Miersch for FS2002\nsupported from Fliegerclub Langhennersdorf\nhttp:\/\/fly.to\/EDOH\n ui_manufacturer=PZL ui_type=Wilga ui_variation=Yellow atc_airline= atc_flight_number=2002 atc_heavy=0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.90, -17.91, 3.88, fx_navred light.1=3, -0.90, 17.91, 3.88, fx_navgre light.2=3, -18.80, 0.00, -1.25, fx_navwhi light.3=2, -1.13, -17.91, 3.78, fx_strobe light.4=2, -1.13, 17.91, 3.78, fx_strobe light.5=1, -16.52, 0.00, 6.00, fx_beacon light.6=4, -2.24, 0.00, 2.20, fx_vclight [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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 [flight_tuning] cruise_lift_scalar=1.159 induced_drag_scalar=0.956 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=0.956 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=0.900 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [piston_engine] power_scalar=1.059 cylinder_displacement= 90.252 compression_ratio= 8.500 number_of_cylinders= 6 max_rated_rpm= 2400.000 max_rated_hp= 250.000 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 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= 0 propeller_diameter= 6.833 propeller_blades= 2 propeller_moi= 5.700 beta_max= 31.800 beta_min= 17.000 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 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [ground_reaction] main_gear_static_compression=0.3 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.3 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.7 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.7 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 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 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 [General] performance=Length: 8.1 m = 26.5 ft.\nWing span: 11.12 m = 36.5 ft.\nWeight:\nPower: Ai-14 RA 250 PS\nDetails: Built in Poland\nDesigner: orig. Jerry Arzdorf\nDate: May 14, 1996\n atc_type=PZL atc_model=PZL-108 [WEIGHT_AND_BALANCE] reference_datum_position= 0.600, 0.000, 0.000 empty_weight_CG_position= 1.000, 0.000, 0.000 max_number_of_stations=50 station_load.0= 160.000, -1.400, -2.500, 0.000 station_load.1= 160.000, -0.400, 2.300, 0.000 station_load.2= 150.000, -3.400, -2.500, 0.000 station_load.3= 150.000, -3.400, 2.300, 0.000 station_load.4= 60.000, -5.400, 0.000, 0.000 empty_weight= 1980.000 empty_weight_roll_MOI= 1500.000 empty_weight_pitch_MOI= 3500.000 empty_weight_yaw_MOI= 5000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 2532.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain= 0.150, -6.100, 2.500, 46.000, 0.000 RightMain= 0.150, 6.100, 2.500, 46.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 160.000 wing_span= 36.500 wing_root_chord= 4.900 wing_dihedral= 10.000 wing_incidence= 1.200 wing_twist= -1.219 oswald_efficiency_factor= 0.665 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 1.000 wing_pos_apex_vert= 1.000 htail_area= 35.000 htail_span= 12.167 htail_pos_lon= -16.333 htail_pos_vert= 0.000 htail_incidence= 1.000 htail_sweep= 5.000 vtail_area= 24.000 vtail_span= 5.586 vtail_sweep= 40.000 vtail_pos_lon= -16.333 vtail_pos_vert= 5.833 elevator_area= 16.610 aileron_area= 18.300 rudder_area= 6.650 elevator_up_limit= 28.000 elevator_down_limit= 20.999 aileron_up_limit= 19.996 aileron_down_limit= 15.000 rudder_limit= 23.995 elevator_trim_limit= 19.498 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 [contact_points] point.0= 1.000, -19.400, 0.000, -2.670, 1184.322, 0.000, 1.000, 60.000, 0.400, 2.500, 0.600, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 4.000, -4.417, -6.667, 1574.803, 1.000, 0.518, 0.000, 0.400, 2.500, 0.600, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 4.000, 4.417, -6.667, 1574.803, 2.000, 0.518, 0.000, 0.400, 2.500, 0.600, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, 1.317, -18.333, 4.333, 1574.803, 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, 1.317, 18.333, 4.333, 1574.803, 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, -18.100, 0.000, -2.500, 1574.803, 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, 8.900, 0.000, -1.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7= 2.000, -14.933, 0.000, 6.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8= 2.000, 0.400, 0.000, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch= 10.150 static_cg_height= 5.600 [GeneralEngineData] engine_type= 0 Engine.0= 7.483, 0.000, -0.417 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 40.000 full_flaps_stall_speed= 32.000 cruise_speed= 93.658 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=0.60,-0.26,2.52 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 3 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 0.500 drag_scalar= 0.500 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 18.000, 0.000 flaps-position.2= 36.000, 0.000