//**********************************PLEASE DO NOT REMOVE*********************************** //* Model PZL Okecie 104 Wilga (c) by Tibor Kókai * //* * //* FSX Conversion by Henk Schuitemaker * //* Texture conversion by MAIW - Martin Gossmann * //* * //* Repaints by Tibor Kókai & Michael Schulze * //* * //* Requires fx_f16_navgrem effect by Henry Tomkiewicz and Mike MacIntyre * //* Requires fx_f16_navredm effect by Henry Tomkiewicz and Mike MacIntyre * //**********************************PLEASE DO NOT REMOVE*********************************** [fltsim.0] title=AI_WILGA SEK sim=TKAI_Wilga_AI_ONLY model= texture=sek ui_manufacturer=PZL ui_type=104 Wilga atc_id=HA-SEK ui_variation=Malév Aero Club description=Repaint by Tibor Kókai atc_parking_types=RAMP atc_parking_codes=104W atc_airline=Aero ui_createdby=MAIW & Tibor Kókai ui_typerole=Military AI [fltsim.1] title=AI_WILGA SEM sim=TKAI_Wilga_AI_ONLY model= texture=sem ui_manufacturer=PZL ui_type=104 Wilga atc_id=HA-SEM ui_variation=Malév Aero Club 2 description=Repaint by Tibor Kókai atc_parking_types=RAMP atc_parking_codes=104W atc_airline=Aero ui_createdby=MAIW & Tibor Kókai ui_typerole=Military AI [fltsim.2] title=AI WILGA VPS sim=TKAI_Wilga_AI_ONLY model= texture=VPS ui_manufacturer=PZL atc_parking_types=RAMP atc_parking_codes=104W ui_type=104 Wilga atc_id=Y4VPS ui_variation=DDR-VPS description=Repaint by Michael Schulze atc_airline=VOPO ui_createdby=MAIW & Tibor Kókai ui_typerole=Military AI [fltsim.3] title=AI WILGA VPT sim=TKAI_Wilga_AI_ONLY model= texture=VPT ui_manufacturer=PZL ui_type=104 Wilga atc_id=Y4VPT atc_parking_types=RAMP atc_parking_codes=104W ui_variation=DDR-VPT description=Repaint by Michael Schulze atc_airline=VOPO ui_createdby=MAIW & Tibor Kókai ui_typerole=Military AI [General] atc_type=SILENT atc_model=PZ04 editable=0 performance=FOR AI USE ONLY Category=airplane [weight_and_balance] max_gross_weight=1500 empty_weight=2275 reference_datum_position=0.0, 0, 0 empty_weight_CG_position=-2.0, 0, 0 empty_weight_pitch_MOI=5400 empty_weight_roll_MOI=3200 empty_weight_yaw_MOI=4350 empty_weight_coupled_MOI=0 max_number_of_stations=0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=7, -17.90, 0, 4.95, fx_beacon //light.3 = 4, -0.68, 0, 1.51, fx_vclight [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [GeneralEngineData] engine_type = 0 // 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=6.4, 0.0, -1.0 fuel_flow_scalar= 0.88 // Fuel flow scalar min_throttle_limit = 0.0 // Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar=1.00 cylinder_displacement=90.0 compression_ratio=8.5 number_of_cylinders=4 max_rated_rpm=2400 max_rated_hp=400 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.3 turbocharged=0 max_design_mp=0 min_design_mp=0 critical_altitude=0 emergency_boost_type=0 emergency_boost_mp_offset=0 emergency_boost_gain_offset=0 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.0 [propeller] thrust_scalar=1.0 // Propeller thrust scalar propeller_type=1 // 0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.3 // Propeller Diameter, (feet) propeller_blades=2 // Number of propeller blades propeller_moi=5.0 // Propeller moment of inertia beta_max=0 // Maximum blade pitch angle for constant speed prop, (degrees) beta_min=0 // Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=0 // Miminum governed RPM prop_tc=0 // Prop time-constant gear_reduction_ratio=1.0 // Propeller gear reduction ratio fixed_pitch_beta=20 // Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 // Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 // Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=0 // Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 // Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 // Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 // Minimum RPM for prop feathering beta_feather=0 // Feathering pitch angle (degrees) power_absorbed_cf=0 // Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 // Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 // Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 // Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 // Minimum pitch angle in reverse, (degrees) [Reference Speeds] flaps_up_stall_speed = 65 // Knots True (KTAS) full_flaps_stall_speed = 60 // Knots True (KTAS) cruise_speed = 107 // Knots True (KTAS) max_indicated_speed = 127 // Red line (KIAS) [fuel] Center=0, 0, 50, 0 fuel_type = 1 // Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [contact_points] static_pitch=7.0 static_cg_height=6.2 gear_system_type=4 tailwheel_lock=0 max_number_of_points=3 point.0=1, -7.000, 0.00, -5.43, 1500, 0, 0.3527, 170, 0.1, 2.5, 0.75, 0, 0, 0, 0, 0 point.1=1, 1.000, -4.50, -6.53, 2500, 1, 0.8842, 0, 0.2, 2.5, 0.75, 0, 0, 2, 0, 0 point.2=1, 1.000, 4.50, -6.53, 2500, 2, 0.8842, 0, 0.2, 2.5, 0.75, 0, 0, 3, 0, 0 [keyboard_response] elevator=200, 1000 aileron=200, 1000 rudder=200, 1000 [airplane_geometry] wing_area = 174.0 // Square feet wing_span = 36.1 // Feet wing_root_chord = 4.9 // Feet wing_dihedral = 1.7 // Degrees wing_incidence = 1.5 // Degrees wing_twist = -3.0 // Degrees oswald_efficiency_factor= 0.68 // Measure of lift effeciency of wing wing_winglets_flag = 0 // Are winglets available? wing_sweep = 0 // Degrees, wing leading edge wing_pos_apex_lon = -2.4 // Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 // Feet, vertical distance from reference point, positive going up htail_area = 39.0 // Square feet htail_span = 11.7 // Feet htail_pos_lon = -18.3 // Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 // Feet, vertical distance from reference point, positive going up htail_incidence = 3.2 // Degrees htail_sweep = 10.0 // Degrees, horizontal tail leading edge vtail_area = 18.0 // Square feet vtail_span = 5.8 // Feet, tip to body vtail_sweep = 20.0 // Degrees, vertical tail leading edge vtail_pos_lon = -21.6 // Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 1.5 // Feet, vertical distance from reference point, positive going up elevator_area = 16.6 // Square feet aileron_area = 18.3 // Square feet rudder_area = 8.0 // Square feet elevator_up_limit = 28.0 // Degrees elevator_down_limit = 21.0 // Degrees aileron_up_limit = 20.0 // Degrees aileron_down_limit = 15.0 // Degrees rudder_limit = 30.0 // Degrees elevator_trim_limit = 19.5 // Degrees spoiler_limit = 0.0 // Degrees spoilerons_available = 0 // Spoilerons Available? aileron_to_spoileron_gain = 0 // Aileron to spoileron gain min_ailerons_for_spoilerons = 0 // Degrees min_flaps_for_spoilerons = 0 // Minimum flap handle posit auto_spoiler_available=0 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 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=2.5 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=0.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 p_factor_on_yaw=0.1 torque_on_roll=0.1 hi_alpha_on_roll=1.0 hi_alpha_on_yaw=1.0 gyro_precession_on_roll=1.0 gyro_precession_on_yaw=1.0 [autopilot] autopilot_available=0 flight_director_available=0 yaw_damper_gain=0 default_vertical_speed=1000 default_pitch_mode=0 default_bank_mode=0 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90 max_throttle_rate=0.1 pitch_takeoff_ga=8 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 use_no_default_bank=1 use_no_default_pitch=1 yaw_slip_control_gain=0.000000 yaw_control_uses_trim=0.000000 [hydraulic_system] normal_pressure=1000 engine_map=1 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=100.0 avionics_bus=0, 5 , 9.5 avionics=1, 5 , 9.5 additional_system=0, 2 , 9.5 marker_beacon=1, 2 , 9.0 fuel_pump=0, 5 , 9.0 [brakes] parking_brake=1 toe_brakes_scale=0.3 auto_brakes=0 [Views] eyepoint=-0.51, -0.89, 0.83 // (feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 7 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 12.7 // degrees flaps-position.2 = 25.3 // degrees flaps-position.3 = 38 // degrees damaging-speed = 120 // KIAS blowout-speed = 150 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type = 0 // 0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [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 [direction_indicators] direction_indicator.0=1,0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,1 // Turn AND Bank [airspeed_indicators] airspeed_indicator.0=1.3, -24.0 [stall_warning] type=2 stick_shaker=0 [pitot_static] vertical_speed_time_constant=1.0 pitot_heat=1.0 [vacuum_system] max_pressure=6.0 vacuum_type=1 engine_map=1 [pneumatic_system] max_pressure=0.000000 [deice_system] structural_deice_type=0