[fltsim.0] title=Z526F_v3HA sim=z526fb model= panel= sound= texture= kb_checklists= description=Zlin Z526F is Czechoslovak sports and training plane. It's intended for basic and for advanced training, for aerobatics training and also for glider's towage.\nAuthor: Tibor Kókai - March 2004\nclidey@freemail.hu\nCreated in FSDS v2.24 \nModel version 3.0 atc_id_color=0000000000 visual_damage=0 ui_manufacturer=Zlin ui_type=Z526F atc_id=HA-TRA ui_variation=Trener9 [General] performance=Wingspan: 10,596 m \nLengt: 8,0 m \nHeight: 2,06 m \nWing Area: 15,451 m2 \nEngine power ( M137 A ): 180 Hp \nFuel: 2x60l + 2x50l \nMax. Take-off Weight: 975 kg \nWeight Empty: 675 kg \nMax. Speed: 304 km\/h \nCruising Speed: 197 km\/h \nClimb rate: 6,0 m\/s \nG-load: +6,0-3,0 \nCeiling: 5000 m \nRange: 960km\FDm: GCs editable=1 atc_type=Zlin atc_model=Z526F [SMOKESYSTEM] //vertical(useless), longitudinal, lateral from ref datum in feet smoke.0= 0, 0, .70, fx_smoke_w [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 1800 empty_weight = 1349 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.5, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 2 station_load.0 = 180, 0, 0, 1 station_load.1 = 0, 0, 0, 0 empty_weight_pitch_MOI = 947 empty_weight_roll_MOI = 1500 empty_weight_yaw_MOI = 2600 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 [GeneralEngineData] engine_type = 0 Engine.0 = 3, 0, 0 fuel_flow_scalar = 1.330 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.000 cylinder_displacement= 90.300 compression_ratio= 8.500 number_of_cylinders= 6 max_rated_rpm= 2640.000 max_rated_hp= 180.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 1.200 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 12000.000 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=1.180 idle_rpm_friction_scalar=0.800 [propeller] thrust_scalar=1.000 propeller_type=0 propeller_diameter=6.300 propeller_blades=2 propeller_moi=2.400 beta_max=28.000 beta_min=13.000 min_gov_rpm=800.000 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 [Flaps.0] type= 1 span-outboard=0.000 extending-time=8.000 system_type=0 damaging-speed=108.000 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=15.000, 0.000 flaps-position.2=45.000, 0.000 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 44.0 //Flap angle that activates warning at idle flap_limit_power = 44.0 //Flap angle that activates warning at above idle [folding_wings] wing_fold_system_type = 1 fold_rates = 0.4, 0.4 [TailHook] tailhook_length = 0 tailhook_position = 0, 0, 0 cable_force_adjust = 1 [contact_points] point.0 = 1, 0.889, 3, -4.6, 1600, 2, 0.709, 0, 0.323, 2.1, 0.8, 5, 5, 0, 0, 0 point.1 = 1, -14, 0, -1.7, 1200, 0, 0.5, 60, 0.123, 2.5, 0.8, 5, 5, 2, 0, 0 point.2 = 1, 0.889, -3, -4.6, 1600, 1, 0.709, 0, 0.323, 2.1, 0.8, 5, 5, 3, 0, 0 point.3 = 2, 10, 0, -0.9, 10000, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.4 = 2, 0, 15, -2.2, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.5 = 2, 0, -15, -2.2, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.6 = 2, -13, 0, 6, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 0 static_pitch= 13 static_cg_height= 4 tailwheel_lock = 0 gear_system_type=1 [Views] eyepoint= -3.5, 0, 2.2 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 [LIGHTS] light.0 = 4, -3.2, 0.0, 2.0, fx_vclight [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 exit_rate.1 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [autopilot] autopilot_available = 0 flight_director_available = 0 [fuel] LeftMain = 0, 3, 2, 20, 0 RightMain = 0, -3, 2, 20, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 169 wing_span = 32 wing_root_chord = 5.28125 wing_dihedral = 1.5 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.877074014215385 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.8203125 wing_pos_apex_vert = 0 htail_area = 21.1 htail_span = 12.2 htail_pos_lon = -13.4 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 12.5 vtail_span = 5.7 vtail_sweep = 0 vtail_pos_lon = -13.7 vtail_pos_vert = 0 elevator_area = 11.7 aileron_area = 12.2 rudder_area = 8 elevator_up_limit = 30 elevator_down_limit = 30 aileron_up_limit = 20 aileron_down_limit = 20 rudder_limit = 30 elevator_trim_limit = 15 spoiler_limit = 70 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 46.1 full_flaps_stall_speed = 45.0 cruise_speed = 128 max_indicated_speed=180.000000 [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 [brakes] toe_brakes_scale=0.4 parking_brake=1 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0