// Dornier Flying boat Do-X v1b2 (05 Diciembre 2002) [fltsim.0] title=AI Dornier DO-X sim=Dornier DoX model= panel= sound= texture= checklists= kb_checklists= kb_reference= prop_anim_ratio=1.76 atc_id=D1929 ui_manufacturer=Dornier ui_type=Dornier X ui_variation=D-1929 atc_id_color=0000000000 atc_id=H0002NL atc_airline=Flua atc_flight_number=2001 atc_parking_codes=Flua atc_parking_types=GATE description=The DORNIER Do X was an all metal large flying boat, first flown in 1929. The Do X was suitable for 70 passengers in well equipped cabins of high comfort and luxury. [General] atc_type=Dornier atc_model=DoX editable=0 performance=Length: 40.05 m (131.4 feet)\nWing span: 48 m (157.5 feet)\nWeight: 30 tons empty (72752 lbs), 56 tons max (123459 lbs)\nPower: max.12x660 hp , Curtiss Conqueror\nCeiling: 3200 m (9900 feet)\nSpeed: Cruise 170 km\/h (95 kts)\nMax Speed: 210 km\/h (113 kts) [Weight_and_Balance] reference_datum_position= 0.000, 0.000, 0.000 // The configuration file reference datum will be the a/c nose empty_weight_CG_position= 29.000, 0.000, 0.000 // Aprox. 19% of M.A.C. // Moments of Inertia (slug-ft^2) empty_weight_roll_MOI=1452787 empty_weight_pitch_MOI=1067884 empty_weight_yaw_MOI=2498456 empty_weight_coupled_MOI=0 CG_forward_limit=0.000 // We don't know what is the CG tolerance of this A/C CG_aft_limit=1.000 // We have supoused the standard tolerance max_gross_weight=123459 // 56 metric tons empty_weight=72752 // 30 metric tons // Peso (lb) , longitudinal (ft), lateral (ft), vertical (ft) station_load.0="170, 38.000, -2.000, 0.000, Pilot" // ok station_load.1="170, 38.000, 2.000, 0.000, Copilot" // ok station_load.2="1700, 15.000, 0.000, 0.000, Crew" // Crew (10) // Subtotal with basic equipment 74792 lbs // Fuel Weight (6340 gallons) 38040 lbs // Basic take off weight 112832 lbs // Load capacity 10648 lbs // Total take off weight 123459 lbs station_load.3="1360.00, 30.000, 0.000, -7.000, Forward Cabin" // 8 passengers station_load.4="2720.00, 5.000, 0.000, -7.000, Main Cabin" // 16 passengers station_load.5="6460.00, -5.000, 0.000, -7.000, Rear Cabin" // 30 passengers max_number_of_stations=7 [Fuel] // There is no available information of fuel tanks of this aircraft, only that was located in then lowest deck number_of_tank_selectors=1 fuel_type=1 LeftMain= 39.000, 0, -12.000, 2113, 0 //forward tank Center1= 29.000, 0, -12.000, 2114, 0 //center tank RightMain= 19.000, 0, -12.000, 2113, 0 //backward tank // All airplane geometry are calculated of a scaned blueprint of DoX // May be inexact but is very aproximated electric_pump=0 [Airplane_Geometry] wing_area=4843.700 wing_span=157.500 wing_root_chord=30.762 wing_dihedral=0.000 wing_incidence=8.000 wing_twist=0.000 wing_sweep=0.000 wing_pos_apex_lon=30.000 //¿borde de ataque? ok wing_pos_apex_vert=5.537 wing_winglets_flag=0 oswald_efficiency_factor=0.98 // Horizontal stabilizer htail_area=331.000 htail_span=49.219 htail_pos_lon=-67.000 //eje deriva ok htail_pos_vert=7.000 //posicion horizontal deriva ok htail_incidence=20.000 //cambiado antes 3 htail_sweep=0.000 // Vertical stabilizer vtail_area=269.876 vtail_span=14.150 vtail_pos_lon=-60.000 //eje timon ok vtail_pos_vert=7.000 //posicion ok vtail_sweep=24.300 // Control surfaces elevator_area=105.942 aileron_area=261.141 rudder_area=52.228 // All control surfaces angles estimated, not found enough data elevator_up_limit=20.000 // 28 elevator_down_limit=15.000 // 22 elevator_trim_limit=30.000 // 20.5-20 aileron_up_limit=18.000 // 26 aileron_down_limit=12.000 // 18 rudder_limit=30.000 // 28 // Spoilers and spoilerons spoiler_limit=0 // No spoilers available spoilerons_available=0 // No spoilers available aileron_to_spoileron_gain=0 min_ailerons_for_spoilerons=0 min_flaps_for_spoilerons=0 [Flight_Tuning] cruise_lift_scalar=1 pitch_stability=1 roll_stability=1 yaw_stability=1 parasite_drag_scalar=1 induced_drag_scalar=1 elevator_effectiveness=1 aileron_effectiveness=0.2 rudder_effectiveness=1 elevator_trim_effectiveness=1 aileron_trim_effectiveness=0 rudder_trim_effectiveness=1 [Pitot_static] vertical_speed_time_constant=1.0 // Increasing this value will cause a more instantaneous reaction in the VSI [Contact_Points] //0 Class (0=None, 1=Wheel, 2=Scrape, 3=Skid, 4=Float, 5=Water Rudder) //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 0=Center Gear 1=Auxiliary Gear 2=Left Gear 3=Right Gear 4=Fuselage Scrape 5=Left Wing Scrape 6=Right Wing Scrape 7=Aux1 Scrape 8=Aux2 Scrape 9=Tail Scrape. //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) // 0 Lo La Ve 4 5 6 7 8 9 10 11 12 13 14 15 point.0=4, -15.700, 0.000, -16.000, 1000, 0, 0, 30, 0.00, 0.00, 1.00, 0, 0, 7, 0, 0 // Water rudder ok point.1=4, 64.200, 0.000, -15.500, 1200, 0, 0, 0, 0.50, 2.50, 0.65, 0, 0, 0, 0, 0 // Extremo delantero de la quilla ok point.2=4, 57.000, 0.000, -16.600, 1200, 0, 0, 0, 0.50, 3.08, 0.65, 0, 0, 0, 0, 0 // Extremo delantero inferior de la quilla ok point.3=4, 34.992, 0.000, -16.000, 1200, 0, 0, 0, 0.90, 3.69, 0.65, 0, 0, 0, 0, 0 // Centro inferior de la quilla point.4=4, -15.300, 0.000, -15.500, 1200, 0, 0, 0, 0.90, 3.69, 0.65, 0, 0, 0, 0, 0 // Extremo trasero inferior de la quilla point.5=4, -66.600, 0.000, -5.500, 1200, 0, 0, 0, 0.50, 2.50, 0.65, 0, 0, 0, 0, 0 // Extremo trasero de la quilla //point.6=4, 10.226, -4.300, -9.228, 1200, 0, 0, 0, 0.50, 2.50, 0.65, 0, 0, 3, 0, 0 // Extremo delantero de la quilla (lateral izquierdo) //point.7=4, 10.226, 4.300, -9.228, 1200, 0, 0, 0, 0.50, 2.50, 0.65, 0, 0, 4, 0, 0 // Extremo delantero de la quilla (lateral derecho) //point.6=4, 30.500, -7.800, -15.600, 1200, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 3, 0, 0 // Centro inferior de la quilla (lateral izquierdo) //point.7=4, 30.500, 7.800, -15.600, 1200, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 4, 0, 0 // Centro inferior de la quilla (lateral derecho) //point.10=4, -30.217, -7.800, -11.074, 1200, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 3, 0, 0 // Extremo trasero inferior de la quilla (lateral izquierdo) //point.11=4, -30.217, 7.800, -11.074, 1200, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 4, 0, 0 // Extremo trasero inferior de la quilla (lateral derecho) point.6=4, 14.600, -17.840, -15.500, 900, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 3, 0, 0 // Left float/stabilizer ok //point.13=4, -32.678, -17.840, -17.000, 900, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 3, 0, 0 // Left float/stabilizer point.7=4, 14.600, 17.840, -15.500, 900, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 4, 0, 0 // Right float/stabilizer ok //point.15=4, -32.678, 17.840, -17.000, 900, 0, 0, 0, 0.88, 2.46, 0.65, 0, 0, 4, 0, 0 // Right float/stabilizer point.8=2, -38.215, -68.291, 5.537, 300, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Left wing point.9=2, -17.850, -78.000, 2.537, 300, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Left wing tip point.10=2, -7.453, -68.291, 5.537, 300, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Left wing point.11=2, -38.215, 68.291, 5.537, 300, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Right wing point.12=2, 17.850, -78.000, 2.537, 300, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Right wing tip point.13=2, -7.453, 68.291, 5.537, 300, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Right wing point.14=2,-127.969, 0.000, 17.226, 600, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Vertical stabilizer point.15=2,-66.600, 0.000, -5.000, 600, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail ok point.16=2,-127.969, -24,609, 8.000, 600, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Horizontal stabilizer left point.17=2,-127.969, 24,609, 8.000, 600, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Horizontal stabilizer right point.18=2, 67.200, 0.000, -4.500, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose ok max_number_of_points=33 // This two values are only aproximated because when a/c fall to water this has no effect static_pitch=0.0 static_cg_height=15.000 [Views] eyepoint= 1.050, -2.500, 0.650 // From pilot seat ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [GeneralEngineData] engine_type=0 // Piston engine fuel_flow_scalar=1.480 // To get the correct fuel flow (aprox. 400 GPH in real A/C) Engine.0= 34.453, -23.5, 15.766 // Frontal left engines (1, 2 & 3 of real A/C) Engine.1= 20.603, -23.5, 15.766 // Rear left engines (7, 8 & 9 of real A/C) Engine.2= 34.453, 23.5, 15.766 // Frontal right engines (4, 5 & 6 of real A/C) Engine.3= 20.603, 23.5, 15.766 // Rear right engines (10, 11 & 12 of real A/C) min_throttle_limit=0.000000 [Piston_Engine] // The real A/C has 12 engines with 660 HP each. // Due FS limitation I must simulate with only four engines. // The simulated engines has 1570 cu.in. and 12 cylinders and aprox. 1350 HP // Basic engines information cylinder_displacement=130.834 // 1570 cu.in total displacement compression_ratio=6 number_of_cylinders=12 max_rated_rpm=2450 max_rated_hp=1980 // 660HP x3 to get the correct sound level fuel_metering_type=1 // Normal Carburettor fuel_air_auto_mixture=0 // Manual mixture cooling_type=1 // Water cooling normalized_starter_torque=0.035 auto_ignition=0 // No auto ignition // Turbo/Supercharger information turbocharged=0 // No turbo in 1929 max_design_mp=0 min_design_mp=0 critical_altitude=0 // Emergency boots system emergency_boost_type=0 // This is not a military a/c emergency_boost_mp_offset=0 emergency_boost_gain_offset=0 // Engine tunning max_rpm_mechanical_efficiency_scalar=1 idle_rpm_mechanical_efficiency_scalar=1 max_rpm_friction_scalar=1 idle_rpm_friction_scalar=1 power_scalar=1 [Propeller] // This propellers are very similar to the real ones, this is to get like real one behavior // The thrust of the egine/propeller couple has been modified in .air file to get three time of the real one. // Basic propeller information thrust_scalar=1 propeller_type=1 // Fixed Pitch propeller_diameter=11 // 11 ft. diameter (more than 3 mtrs, a realy big propeller) propeller_blades=4 propeller_moi=37,93 // This big propellers has a big inertia fixed_pitch_beta=20 // Beta degrees of each blade beta_max=0 beta_min=0 min_gov_rpm=0 prop_tc=0.010 gear_reduction_ratio=1 low_speed_theory_limit=80 rotation=1,1,1,1 prop_sync_available=0 prop_deice_available=0 // Feathering prop_feathering_available=0 // Fixed pitch no feathering available prop_auto_feathering_available=0 min_rpm_for_feather=0 beta_feather=0 power_absorbed_cf=1 defeathering_accumulators_available=0 // Reverse prop_reverse_available=0 // Fixed pitch reverse power available minimum_on_ground_beta=0 minimum_reverse_beta=0 [Reference Speeds] flaps_up_stall_speed=58 // 108 km/h (Estimated) full_flaps_stall_speed=58 // 108 km/h cruise_speed=95 // 176 km/h max_indicated_speed=115.000000 [autopilot] autopilot_available= 1 flight_director_available= 0 pitch_takeoff_ga=0.0 default_vertical_speed=200.000000 autothrottle_available=0 direction_indicator=1 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=10.000000 //era 25 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 = 0.0 default_bank_mode=2 //Default to Heading Hold //[Autopilot] viejo //use_no_default_pitch=0 //use_no_default_bank=1 // Only one axis autopilot //default_vertical_speed=200 // Realy 236 but only suport VSI rounded to 100 //default_bank_mode=0 [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=3, 0 [Electrical] max_battery_voltage=24 generator_alternator_voltage=28 max_generator_alternator_amps=60 // BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) starter1=0, 20, 18.0 starter2=0, 20, 18.0 starter3=0, 20, 18.0 starter4=0, 20, 18.0 light_nav=0, 5, 15.0 light_panel=2, 10, 24.0 //pitot_heat=0, 2, 18.0 fuel_pump=0, 8, 17.0 fuel_transfer_pump=0, 5, 17.0 //propeller_deice=0, 5, 17.0 additional_system=1, 20, 18.0 avionics_bus=0, 10, 20.0 avionics=1, 5, 20.0 autopilot=1, 5, 20.0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 17.850, -78.000, 2.537, fx_navredh // Left wing tip light.1=3, 17.850, 78.000, 2.537, fx_navgreh // Right wing tip light.2=3,-66.600, 0.000, -5.000, fx_navwhih // Tail ok light.3=4, 37.000, 0.000, 1.500, fx_vclighth // Luz prueba punto 0 //light.4=3, 35.000, 5.000, 2.750, fx_navredh // Luz prueba punto 0 //light.4=3, 67.200, 0.000, -4.500, fx_navredh // luz prueba punta morro ok //light.4=3, 59.000, 0.000, 15.000, fx_navredh // luz prueba maletas //light.5=3, 50.000, 0.000, -17.700, fx_navgreh // luz prueba punto2 quilla //light.6=3, 64.200, 0.000, -15.500, fx_navgreh // luz prueba punto1 quilla ok //light.7=3, -4.992, 0.000, -15.920, fx_navgreh // luz prueba punto3 quilla //light.8=3, -30.217, 0.000, -12.920, fx_navgreh // luz prueba punto4 quilla //light.9=3, -54.210, 0.000, -12.720, fx_navgreh // luz prueba punto5 quilla //light.10=3, 30.000, 0.000, 15.000, fx_strobeh // luz prueba wing appex ok //light.11=3, 0.000, 0.000, 15.000, fx_navwhih // luz prueba datum position ok //light.12=3, 48.000, 2.000, 0.000, fx_navwhih // luz prueba piloto ok //light.13=3,-60.000, 12.000, 7.000, fx_navredh // luz prueba eje timon ok //light.13=3, 25.000, 0.000, 16.000, fx_navredh // luz prueba CG ok [Exits] number_of_exits=2 exit_rate.0=0.4 exit_rate.1=0.8 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 // Only audio Com.1=1, 0 Com.2=0 Nav.1=0 Nav.2=0 Adf.1=1 Transponder.1=0 Marker.1=0 [EFFECTS] wake=fx_wake_l water=fx_spray waterspeed=fx_wtrspray_m // Beauty water splash when a/c tuoch the water too fast dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt [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=90, 100 aileron=90, 100 rudder=90, 100 [forcefeedback] // This are not tested stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=0.000000 parking_brake=0 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
