[fltsim.0] title=Spin sim=Spin model= panel= sound= texture= kb_checklists= kb_reference= atc_id=PH-AAA ui_manufacturer="Fokker" ui_type="Spin" ui_variation= ui_typerole="Single Engine Prop" ui_createdby="Rien Cornelissen" description="Flight dynamics derived from FSX Piper Cub, adapted by Rien Cornelissen." [General] performance="Cruise Speed\n57 kts \n\nEngine\nArgus AS 1 90 hp\n\nPropeller\n2-blade fixed\n\nFuel tank\n5 gal \n\nMaximum Gross Weight\n800 lb 360 kg\n\nEmpty Weight\n600 lb 270 kg\n\nLength\n12 ft, 9.5 in 3.9 m\n\nWing Span\n33 ft, 6 in 10.6 m\n\nHeight\n11 ft, 8 in 3.57 m\n\nSeating\n1\n\nUseful Load\n160 lb 70 kg" Category = airplane //lateral-vertical-longitudinal, in meters [WEIGHT_AND_BALANCE] max_gross_weight= 800.0 empty_weight = 600.0 reference_datum_position= 0.00, 0.00, 0.00 empty_weight_CG_position= 0.00, 0.00, 0.00 max_number_of_stations =50 station_load.0 = 170.0, -3.25, 0.00, 0.00 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_name.0 = "Pilot" ;Moments of Inertia empty_weight_pitch_MOI = 313.8 empty_weight_roll_MOI = 313.9 empty_weight_yaw_MOI = 642.2 empty_weight_coupled_MOI = 0.0 [flight_tuning] cruise_lift_scalar = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 0 rudder_effectiveness = 1.0 elevator_trim_effectiveness= 0 aileron_trim_effectiveness = 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 = 7.296, 0.0, 1.729 //(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= 50 //Cubic inches per cylinder compression_ratio= 6.0 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm= 2300 //Max rated RPM max_rated_hp= 90 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //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= 0 //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= 0.5 //Scalar on idle RPM friction magneto_order_left_right_both = 1 //sets the order of the magneto switch direction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.0 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 3.78 //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= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 13.75 //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 in feather 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) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) [contact_points] //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 point.0 = 1, -3.75, 0.00, -4.20, 1500, 0, 0, 22.0, 0.25, 2.0, 0.8, 0.0, 0.0, 0 point.1 = 1, 3.5, -3.9, -4.75, 3500, 1, 1.6, 0.0, 0.40, 2.0, 0.8, 0.0, 0.0, 2 point.2 = 1, 3.5, 3.9, -4.75, 3500, 2, 1.6, 0.0, 0.40, 2.0, 0.8, 0.0, 0.0, 3 max_number_of_points=21 static_pitch=3.5 static_cg_height=4.05 [Views] eyepoint=-2.625, 0.0, 4.211 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type=availiable, standby frequency, has glide slope [LIGHTS] Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1= 1.00, 0.00, 1.00, 5.00, 0.00 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 engine_driven_pump=0 [airplane_geometry] wing_area = 178.5 //Square feet wing_span = 35.2 //Feet wing_root_chord = 5.25 //Feet wing_dihedral = 10 //Degrees wing_incidence = 2.5 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.4 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 10 //Degrees, wing leading edge wing_pos_apex_lon = 3.31 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 2.1 //Feet, vertical distance from reference point, positive going up htail_area = 18.2 //Square feet htail_span = 9.6 //Feet htail_pos_lon = -13.4 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 1.3 //Feet, vertical distance from reference point, positive going up htail_incidence = -0.8 //Degrees htail_sweep = 30.0 //Degrees, horizontal tail leading edge vtail_area = 13.0 //Square feet vtail_span = 4.44 //Feet, tip to body vtail_sweep = 38.0 //Degrees, vertical tail leading edge vtail_pos_lon = -13.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 1.6 //Feet, vertical distance from reference point, positive going up elevator_area =10 //Square feet aileron_area = 0 //Square feet rudder_area = 5 //Square feet elevator_up_limit = 20.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 0 //Degrees aileron_down_limit = 0 //Degrees rudder_limit = 28.0 //Degrees elevator_trim_limit = 0 //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 auto_spoiler_available = 0 positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up) positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down) negative_g_limit_flaps_up = -1.5 //Design G load tolerance (negative, flaps up) negative_g_limit_flaps_down= -1.5 //Design G load tolerance (negative, flaps down) load_safety_factor = 1.5 //Design G load safety factor [Reference Speeds] flaps_up_stall_speed = 33.0 //Knots True (KTAS) full_flaps_stall_speed = 33.0 //Knots True (KTAS) cruise_speed = 59.0 //Knots True (KTAS) max_indicated_speed = 106 //Red line (KIAS) [autopilot] autopilot_available= 0 flight_director_available= 0 default_vertical_speed= 700.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 default_pitch_mode=1 default_bank_mode=1 max_pitch=10.0 max_bank=17.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.000000 [Flaps.0] type= 0 [exits] number_of_exits=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 [brakes] toe_brakes_scale=1.0 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type= 0 stick_shaker= 0 [attitude_indicators] attitude_indicator.0=2 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0
