[fltsim.0] title=Zlin 726 Trener Universal sim=z726universal model= panel= sound= texture= kb_checklists= kb_reference= atc_id=SP prop_anim_ratio=1.03 ui_manufacturer=Zlin ui_type=Z726TU ui_variation=Trener Universal description=Zlin 726 Trener Universal [General] atc_type=Zlin atc_model=Z726 editable=0 performance=Designed by Capt.I.D'Attomo. FD by GCs. [WEIGHT_AND_BALANCE] max_gross_weight = 2210 empty_weight = 1550 reference_datum_position = 3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170, -3.0, 0.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "000, 0.0, 0.0, 0.0, Student" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1400.0 empty_weight_roll_MOI = 1137.0 empty_weight_yaw_MOI = 2360.0 empty_weight_coupled_MOI= 0.0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 2.0 aileron_effectiveness = 0.34 rudder_effectiveness = 1.0 pitch_stability = 1.8 roll_stability = 0.3 yaw_stability = 3.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 90.3 //Cubic inches per cylinder compression_ratio= 8.5 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm= 2575 //Max rated RPM max_rated_hp= 180 //Max rated HP fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.5 //Starter torque factor turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 35 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 24000.00 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 1 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.58 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 8.3 //Propeller moment of inertia beta_max= 31.7 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 14.9 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.1 //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) rotation=-1 [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, 0 , 00.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 2 , 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 //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0=1, -16.18, 0.0, -1.64, 9181.1, 0, 0.523, 20.66, 0.296, 1.99, 0.794, 4.0, 4.0, 0, 0.0, 0.0 point.1=1, -1.70, -3.0, -4.10, 4574.8, 1, 0.523, 0.00, 0.286, 2.5, 0.808, 5.0, 5.0, 2, 0.0, 0.0 point.2=1, -1.70, 3.0, -4.10, 4574.8, 2, 0.523, 0.00, 0.286, 2.5, 0.808, 5.5, 5.5, 3, 0.0, 0.0 point.3 = 2, -3.60, -16.0, -1.00, 4574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4 = 2, -3.60, 16.0, -1.00, 4574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5 = 2, -18.00, 0.0, -0.90, 4574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6 = 2, 6.00, 0.0, -2.10, 4574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.7 = 2, -2.93, 0.0, -2.20, 4574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0 point.8 = 2, -4.60, 0.0, -1.00, 4574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8, 0.0, 0.0 max_number_of_points = 21 static_pitch=11.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=4.1 //feet, altitude of CG when at rest on the ground gear_system_type=0 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.68 //Brake scalar [hydraulic_system] normal_pressure = 0.0 //PSI [fuel] //Tanks Position and capacity: //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -3.85, -2.10, 0.00, 22.0, 0.00 RightMain= -3.85, 2.10, 0.00, 22.0, 0.00 //Fuel type: 1 = Avgas, 2 = JetA fuel_type=1 number_of_tank_selectors = 1 electric_pump=1 [Views] eyepoint= -3.0, 0.0, 1.6 //(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 = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 30 // degrees flaps-position.2 = 45 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // 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] // availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Transponder.1 = 1 Marker.1 = 1 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [exits] number_of_exits = 2 exit_rate.0 = 0.5 exit_rate.1 = 0.4 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 100, 180 aileron = 200, 1000 rudder = 200, 1000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=1,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,1 //Turn AND Bank [airspeed_indicators] airspeed_indicator.0 = 1,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area = 128.5 //Square feet wing_span = 34.0 //Feet wing_root_chord = 4.9 //Feet wing_dihedral = 6.3 //Degrees wing_incidence = 1.5 //Degrees wing_twist = -3.0 //Degrees oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //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 = 78.0 //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 = 4.8 //Feet, tip to body vtail_sweep = 40.0 //Degrees, vertical tail leading edge vtail_pos_lon = -16.2 //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 = 6.7 //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 = 18.0 //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 position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 54.0 //Knots True (KTAS) full_flaps_stall_speed = 49.0 //Knots True (KTAS) cruise_speed = 175.0 //Knots True (KTAS) max_indicated_speed = 210 //Red line (KIAS) [autopilot] autopilot_available= 0 flight_director_available= 0 [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 [stall_warning] type=1 [LIGHTS] light.0 = 4, -2.5, 0, 1.3, fx_vclight