[fltsim.0] title=DR400 sim=DR400 model= panel= sound= texture= kb_checklists=DR400_check kb_reference=DR400_ref atc_id=FGUXK ui_manufacturer=Robin ui_type=DR400 ui_variation= visual_damage=0 description=La plupart des pilotes français on volé au moins quelques heures sur Robin DR 400, c'est l'appareil le plus répandu dans les aéro-clubs et il est utilisé par la plupart des écoles de pilotage. modélisation FSDS ©Yannick Lavigne-Fred Banting-Rob Young - novembre 2002 [General] editable=0 atc_type=Robin atc_model=DR400 performance=Maximum Speed\t160 kts\nCruise Speed\t140 kts\nEngine\tLycoming O-360-A3A 180 hp\nPropeller\tTwo-bladed Sensenich Fixed\nMaximum Range\t757 nm\nService Ceiling\t14,720 ft\nFuel Capacity\t50 U.S gal\nMax Gross Weight\t2425 lbs\nLength\t\t23 ft, 3 in\nWingspan\t\t28 ft, 7 in\nHeight\t\t7 ft, 4 in\nSeating\t\t4\nUseful Load\t1019 lb\n [WEIGHT_AND_BALANCE] max_gross_weight=2425.0 empty_weight=1406.0 reference_datum_position=0.0, 0.0, 0.0 empty_weight_CG_position=0.0, 0.0, 0.0 //-0.55 max_number_of_stations=10 //MAX station loads (Including Fuel) 1019 lbs. //Weight (lbs), long, lat, vert positions from datum (feet) station_load.0=170.0, 1.0, 0.0, 0.0 //Pilot station_load.1=170.0, 1.0, 0.0, 0.0 //Co Pilot station_load.2=100.0, -2.0, 0.0, 0.0 //Rear Passenger station_load.3=100.0, -2.0, 0.0, 0.0 //Rear Passenger station_load.4=060.0, -4.4, 0.0, 0.0 //Baggage //Moments of Inertia empty_weight_pitch_MOI=2400.0 // 1400 empty_weight_roll_MOI=2200.0 // 1200 empty_weight_yaw_MOI=1226.0 // 2400 empty_weight_coupled_MOI=0.0 CG_forward_limit=0.0 CG_aft_limit=1.0 [Views] eyepoint=-0.25, -0.85, 2.0 //(feet) longitudinal, lateral, vertical [fuel] Center1=-0.20, 0.0, -1.7, 26.5, 0.0 LeftMain=-0.20, -2.5, -1.5, 10.5, 0.0 RightMain=-0.20, 2.5, -1.5, 10.5, 0.0 fuel_type=1.0 number_of_tank_selectors=1 electric_pump=1 [electrical] //BusType, MaxAmpLoad, MinVoltage //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 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 [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 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.0 autothrottle_available=1 autoland_available=0 pitch_takeoff_ga=8.0 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=0 default_bank_mode=0 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=25.000000 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 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 [pitot_static] vertical_speed_time_constant=0.7 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.4 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.9 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.324, -14.645, -0.241, dr_navred light.1=3, 0.324, 14.645, -0.241, dr_navgre light.2=1,-14.081, 0.00, 4.200, dr_navwhi light.3=5, 1.847, -7.972, -1.334, dr_landing.fx light.4=5, 1.847, -7.562, -1.334, dr_landing.fx light.5=2, -5.780, 0.000, 1.900, dr_strobe light.6=4, 0.000, 0.000, 2.200, fx_vclight [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 [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 [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [GeneralEngineData] engine_type=0 Engine.0=6.5, 0.0, 0.0 fuel_flow_scalar=1.04 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.1 cylinder_displacement=90.0 compression_ratio=8.5 number_of_cylinders=4 max_rated_rpm=2700.0 max_rated_hp=180.0 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=3.0 turbocharged=0 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0.0 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 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=1.6 [propeller] thrust_scalar=0.81 propeller_type=1 propeller_diameter=6.5 // 6.33 propeller_blades=2 propeller_moi=2.2 beta_max=0.0 beta_min=0.0 min_gov_rpm=0.0 prop_tc=0.0 gear_reduction_ratio=1.0 fixed_pitch_beta=19.0 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [flaps.0] type=1 // 1 - trail, 2 - lead span-outboard=0.56 // 0.0 .. 1.0 extending-time=6.0 // seconds system_type=3 // 0=Elec, 1=Hyd, 2=Pneu, 3=Man, 4=None flaps-position.0=0.0, 0.0 //Degrees flaps-position.1=30.0, 0.0 //was 15.0 but needs more drag Degrees flaps-position.2=60.0, 0.0 //Degrees damaging-speed=120 //KIAS blowout-speed=150 //KIAS [reference speeds] flaps_up_stall_speed=57.0 //Knots True (KTAS) full_flaps_stall_speed=51.0 //Knots True (KTAS) cruise_speed=140.0 //Knots True (KTAS) max_indicated_speed=166.000000 [airplane_geometry] wing_area=153.0 wing_span=28.58 wing_root_chord=6.16 wing_dihedral=2.0 //7.0 wing_incidence=4.6 wing_twist=-0.8 // -1.5 oswald_efficiency_factor=0.8 // 0.6 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=1.58 wing_pos_apex_vert=-1.3 htail_area=31.0 htail_span=10.50 htail_pos_lon=-12.3 htail_pos_vert=0.5 htail_incidence=2.0 // 2.2 htail_sweep=0.0 vtail_area=18.0 vtail_span=4.8 vtail_sweep=30.0 vtail_pos_lon=-13.3 vtail_pos_vert=1.66 elevator_area=16.6 aileron_area=12.26 rudder_area=6.78 elevator_up_limit=25.0 elevator_down_limit=24.0 // 16.0 aileron_up_limit=15.0 aileron_down_limit=12.0 //15.0 rudder_limit=25.0 elevator_trim_limit=20.0 spoiler_limit=0.0 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [contact_points] //0 Class //1 Longitudinal Position (feet, +=fwd) //2 Lateral Position (feet, +=right) //3 Vertical Position (feet, +=above) //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1.0, 4.4, 0.0, -3.90, 1500.0, 0.0, 0.5, 29.0, 0.18, 1.5, 1.0, 0.0, 0.0, 0.0, 0.0, 0.0 point.1=1.0, -1.5, -4.5, -3.90, 3000.0, 1.0, 0.5, 0.0, 0.25, 1.5, 0.8, 0.0, 0.0, 2.0, 0.0, 0.0 point.2=1.0, -1.5, 4.5, -3.90, 3000.0, 2.0, 0.5, 0.0, 0.25, 1.5, 0.8, 0.0, 0.0, 3.0, 0.0, 0.0 point.3=2.0, 0.0,-14.1, -0.75, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2.0, 0.0, 14.1, -0.75, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2.0,-14.5, 0.0, -1.0, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2.0, 5.8, 0.0, -1.2, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 point.7=2.0,-16.3, 0.0, 4.0, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0 max_number_of_points=10 static_pitch=-0.7 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=3.55 //feet, altitude of CG when at rest on the ground // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 //point.0=1.0, 4.0, 0.0, -3.95, 1500.0, 0.0, 0.5, 29.0, 0.15, 2.5, 0.8, 0.0, 0.0, 0.0, 0.0, 0.0 //point.1=1.0, -1.5, -4.5, -4.06, 3000.0, 1.0, 0.5, 0.0, 0.25, 2.5, 0.8, 0.0, 0.0, 2.0, 0.0, 0.0 //point.2=1.0, -1.5, 4.5, -4.06, 3000.0, 2.0, 0.5, 0.0, 0.25, 2.5, 0.8, 0.0, 0.0, 3.0, 0.0, 0.0 //point.3=2.0, 0.0,-14.1, -0.75, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 //point.4=2.0, 0.0, 14.1, -0.75, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 //point.5=2.0,-14.5, 0.0, -1.0, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 //point.6=2.0, 5.8, 0.0, -1.2, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 //point.7=2.0,-16.3, 0.0, 4.0, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0 //max_number_of_points=10 //static_pitch=-0.7 //degrees, pitch when at rest on the ground (+=Up, -=Dn) //static_cg_height=3.55 //feet, altitude of CG when at rest on the ground [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=0.543229 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
