[fltsim.0] title=SF 28 A Tandemfalke sim=SF28 model= panel= sound= texture= kb_checklists=sf28_check kb_reference=sf28_ref description="Scheibe SF 28 A Tandem-Falke" ui_manufacturer="Scheibe" ui_type="SF 28 A Tandemfalke" ui_typerole="Motorglider" ui_createdby"Wolfgang Piper" ui_variation= visual_damage=1 atc_heavy=0 atc_id=FCEYS atc_airline= atc_flight_number= prop_anim_ratio=0.5 [General] performance=Länge:8.15 m \nSpannweite: 16.3m \nGewicht: 580 kg max, 380 kg leer\nDesigner: Wolfgang Piper, 07/2006 Category=airplane [CameraDefinition.0] Title = "Tail" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c} Description = Looking forward from behind the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .75 ShowWeather = Yes InitialXyz = 0, 3.1, -20.0 InitialPbh = 10, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 12.5, 1.9, 0.0 InitialPbh = 9, 0, 270 XyzAdjust = TRUE Category=Aircraft MomentumEffect = TRUE ClipMode=Minimum [CameraDefinition.2] Title = "Left Wing" Guid = {33320004-b71a-4f9f-9105-1eb674ab7f3c} Description = View from the left wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -12.5, 1.9, 0.0 InitialPbh = 9, 0, 90 XyzAdjust = TRUE Category=Aircraft MomentumEffect = TRUE ClipMode=Minimum [CameraDefinition.001] Title = "Rear Seat" Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = .7 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=30 HeadingPanRate=75 PanAcceleratorTime=0 InitialXyz=0.0, 0.0, -1.15 InitialPbh=0, 0, 0 [WEIGHT_AND_BALANCE] max_gross_weight=1385.000000 empty_weight=885.000000 reference_datum_position=0.0000, 0.0000, 0.0000 empty_weight_CG_position=-3.90000,0.000000,0.000000 station_load.0=170,2.00000,0.000000,0.000000 // Pilot station_load.1=170,-1.00000,0.000000,0.000000 // Guest station_load.2=10,-16.00000,0.000000,0.000000 // CG- Korrektur empty_weight_roll_MOI=900.000000 empty_weight_pitch_MOI=2300.000000 empty_weight_yaw_MOI=700.000000 empty_weight_coupled_MOI=0.000000 [GeneralEngineData] engine_type=0 Engine.0=6.5, 0.0, 0.00 fuel_flow_scalar=0.88 min_throttle_limit=0.00000 [Electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 33 [piston_engine] power_scalar=1.00 cylinder_displacement=60.0 compression_ratio=7.5 number_of_cylinders=2 max_rated_rpm=3420 max_rated_hp=220 fuel_metering_type=1 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=1.45 idle_rpm_mechanical_efficiency_scalar=1.45 max_rpm_friction_scalar=1.10 idle_rpm_friction_scalar=1.10 [propeller] thrust_scalar = 0.6 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 5.0 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 3 //Propeller moment of inertia beta_max= 45.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 15.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1100.0 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 0.95 //Propeller gear reduction ratio fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.0 //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= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering beta_feather= 50.5 //Feathering pitch angle (degrees) power_absorbed_cf= 0.9 //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= 15.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees) [airplane_geometry] wing_area=285.000000 wing_span=53.500000 wing_root_chord=5.3 wing_dihedral=3 wing_incidence=1.5 wing_twist=-0.999756 oswald_efficiency_factor=0.7 wing_winglets_flag=0 wing_sweep=3.000000 wing_pos_apex_lon=0.80000000 wing_pos_apex_vert=-1.000000 htail_area=24.000000 htail_span=9.3 htail_pos_lon=-14 htail_pos_vert=1.2 htail_incidence=0 htail_sweep=0.000000 vtail_area=16.000000 vtail_span=4.6 vtail_sweep=0.000000 vtail_pos_lon=-16.000000 vtail_pos_vert=2.5 elevator_area=12.4 aileron_area=11.900000 rudder_area=10.5 elevator_up_limit=20 elevator_down_limit=30 aileron_up_limit=18 aileron_down_limit=15 rudder_limit=25 elevator_trim_limit=20 spoiler_limit=40 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 spoiler_extension_time=0.800000 positive_g_limit_flaps_up=5.500000 positive_g_limit_flaps_down=5.500000 negative_g_limit_flaps_up=-3.500000 negative_g_limit_flaps_down=-3.500000 load_safety_factor=1.5 [flight_tuning] cruise_lift_scalar=1.34 parasite_drag_scalar=0.8 induced_drag_scalar=0.84 elevator_effectiveness=0.6 aileron_effectiveness=0.6 rudder_effectiveness=0.8 pitch_stability=1.0 roll_stability=1.1 yaw_stability=0.8 elevator_trim_effectiveness=1.3 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=0.8 p_factor_on_yaw=-1.0 //dreht nach rechts torque_on_roll=-1.0 //dreht nach rechts [fuel] Center1 = 4.5, 0.000, 1.000, 10.600, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [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 // Lang. Breit. Vert. // Pos. Pos. Pos. // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 //-------------------------------------------------------------------------------------------------------------------------------- point.0=1, -14.76, 0, -0.8, 1800, 0, 0.5, 20, 0.25, 2.5, 0.7, 0, 0, 0, 0, 0 // Gear Tail point.1=1, 1.0, -0.1, -3.1, 2500, 1, 0.5, 0, 0.3, 2.5, 0.7, 0, 0, 2, 0, 0 // Gear Main point.2=1, 1.0, 0.1, -3.1, 2500, 2, 0.5, 0, 0.3, 2.5, 0.7, 0, 0, 3, 0, 0 // Gear Main point.3=1, -0.9, -8.6, -2.6, 2500, 0, 0.4, 0, 0.3, 2.5, 0.7, 0, 0, 2, 0, 0 // Gear Left point.4=1, -0.9, 8.60, -2.6, 2500, 0, 0.4, 0, 0.3, 2.5, 0.7, 0, 0, 3, 0, 0 // Gear Right point.5=2, 0, -21.0, 1.1, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip point.6=2, 0, 21.0, 1.1, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip point.7=2, -14.76, 0, -0.2, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail(?) point.8=2, 6.5, 0, -2.6, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose static_pitch=7 //degrees (pitch when loaded on ground) static_cg_height=3.0 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint=1.30, 0, 1.55 //(feet) longitudinal, lateral, vertical distance from reference datum [Reference Speeds] flaps_up_stall_speed=35.000000 full_flaps_stall_speed=33.500000 cruise_speed=45 max_indicated_speed=150 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [autopilot] autopilot_available=0 flight_director_available=1 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=2,0 [exits] number_of_exits=4 exit_rate.0=0.5 exit_rate.1=1 exit_rate.2=1 exit_rate.3=1 [Flaps.0] type=0 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=0 [vacuum_system] max_pressure=0 vacuum_type=1 [pneumatic_system] max_pressure=0 [deice_system] structural_deice_type=0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000