[fltsim.0] title=Biman DC-10-30ER ADN sim=FFXDC1030ER model=30F panel= sound= texture=bcc kb_checklists= kb_reference= ui_manufacturer=McDonell Douglas ui_type=MD-10-30 ui_variation=Biman DC-10-30ER ADN visual_damage=0 description=In memory of S2-ADN came into service November 2000, future of this aircraft came to an halt after crashing on runray 23 at Chittagong airport on July 2nd 2005.Biman Bangladesh Airlines Home Away From Home,Though It's a dream to have the newest luxury aircraft in the Biman's Fleet wit the growing number of passengers each year, For now let us enjoy the flights in virtual simulations. atc_heavy=1 atc_id=S2-ADN atc_airline=Bangladeshi atc_flight_number=69 [General] atc_type=MCDONNELDOUGLAS atc_model=DC10 editable=0 performance=Engines: SEE ENGINE SECTION\nFuel capacity: 36,554 USG (244,912 lb @ 6.7 lb USG)\nMax speed: 350 kts IAS or Mach 0.88\nFlap settings: 5-15-22-35-50\nMax operating altitude: 42,000 Ft\nTypical cruise setting: FL310-370 @ Mach 0.82 [forcefeedback] gear_bump_nose_magnitude= 3000 ; 0 - 10000 gear_bump_nose_direction= 18000 ; 0 - 35999 degrees gear_bump_nose_duration= 250000 ; in microseconds gear_bump_left_magnitude= 2700 ; 0 - 10000 gear_bump_left_direction= 35500 ; 0 - 35999 degrees gear_bump_left_duration= 250000 ; in microseconds gear_bump_right_magnitude= 2700 ; 0 - 10000 gear_bump_right_direction= 00500 ; 0 - 35999 degrees gear_bump_right_duration= 250000 ; in microseconds ground_bumps_magnitude1= 1300 ; 0 - 10000 ground_bumps_angle1= 08900 ; 0 - 35999 degrees ground_bumps_intercept1= 3.0 ground_bumps_slope1= 0.20 ground_bumps_magnitude2= 200 ; 0 - 10000 ground_bumps_angle2= 09100 ; 0 - 35999 degrees ground_bumps_intercept2= 1.075 ground_bumps_slope2= 0.035 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 [flight_tuning] cruise_lift_scalar= 1.10 parasite_drag_scalar= 1.20 induced_drag_scalar= 1.10 elevator_effectiveness= 0.90 aileron_effectiveness= 0.90 rudder_effectiveness= 1.00 pitch_stability= 1.20 roll_stability= 1.20 yaw_stability= 1.00 elevator_trim_effectiveness= 1.20 aileron_trim_effectiveness= 1.00 rudder_trim_effectiveness= 1.00 //Series 30// //Design gross weight (ramp) 575,000 lb (260,820 kg) //Maximum takeoff weight 572,000 lb (259,459 kg) //Design landing weight (1) 405,000 lb (182,766 kg) //Maximum zero fuel weight 368,000 lb (166,924 kg) //Operator's empty weight 267,996 lb (121,563 kg) //Fuel capacity 36,650 USgal (138,735L) //245,566 lb //(111,388 kg) //Weight limited payload 100,809 lb (45,726 kg) //Level flight speed 600+ mph (965 km/h) //FAA takeoff field lgth-std.wght 9,650 ft(2,847 m) //FAA landing field lgth-std.wght 5,960 ft(1,758 m) //Design range (2) 5,860 mi //5,096 nmi //9,429 km // (1)Higher weights are available. // (2)277 passengers and baggage; domestic reserves. // Passenger Capacity 250-380 [WEIGHT_AND_BALANCE] max_gross_weight= 575000.00 empty_weight= 267996.00 reference_datum_position= 0.00, 0.00, 0.00 empty_weight_CG_position= 0.00, 0.00, 0.00 station_load.0= 2400, 65.50,-5.00, 1.50 station_load.1= 2900, 65.50, 5.00, 1.50 station_load.2= 1000, 59.00,-5.00, 1.50 station_load.3= 2100, 59.00, 5.00, 1.50 station_load.4= 3200, 52.50,-5.00, 1.50 station_load.5= 850, 52.50, 5.00, 1.50 station_load.6= 2100, 46.00,-5.00, 1.50 station_load.7= 2050, 46.00, 5.00, 1.50 station_load.8= 1000, 39.50,-5.00, 1.50 station_load.9= 1250, 39.50, 5.00, 1.50 station_load.10= 2200, 33.00,-5.00, 1.50 station_load.11= 1450, 33.00, 5.00, 1.50 station_load.12= 2050, 26.50,-5.00, 1.50 station_load.13= 1700, 26.50, 5.00, 1.50 station_load.14= 1650, 20.00,-5.00, 1.50 station_load.15= 2000, 20.00, 5.00, 1.50 station_load.16= 3000, -15.00,-5.00, 1.50 station_load.17= 2450, -15.00, 5.00, 1.50 station_load.18= 1100, -21.00,-5.00, 1.50 station_load.19= 2000, -21.00, 5.00, 1.50 station_load.20= 2800, -27.00,-5.00, 1.50 station_load.21= 1000, -27.00, 5.00, 1.50 station_load.22= 2000, -33.00,-5.00, 1.50 station_load.23= 2150, -33.00, 5.00, 1.50 station_load.24= 1150, -39.00,-5.00, 1.50 station_load.25= 1700, -39.00, 5.00, 1.50 station_load.26= 500, 77.00,-3.00, 9.50 station_load.27= 500, 77.00, 3.00, 9.50 station_load.28= 1020, 56.66,-4.00, 9.50 station_load.29= 680, 56.66, 0.00, 9.50 station_load.30= 1260, 56.66, 4.00, 9.50 station_load.31= 1020, 36.31,-6.00, 9.50 station_load.32= 850, 36.31, 0.00, 9.50 station_load.33= 680, 36.31, 6.00, 9.50 station_load.34= 1200, 18.97, 0.00, 9.50 station_load.35= 1200, 15.97, 0.00, 9.50 station_load.36= 120,-10.64, 0.00, 9.50 station_load.37= 120,-10.64, 0.00, 9.50 station_load.38= 10220,-24.73,-6.00, 9.50 station_load.39= 10220,-24.73, 0.00, 9.50 station_load.40= 10220,-24.73, 6.00, 9.50 station_load.41= 1200,-45.07,-3.00, 9.50 station_load.42= 1220,-45.07, 3.00, 9.50 station_load.43= 8900, 14.00,-29.25,-2.80 station_load.44= 8900,-78.50, 0.00, 22.50 station_load.45= 8900, 14.00, 29.25,-2.80 station_load.46= 240, 87.75,-2.30, 9.50 station_load.47= 180, 87.75, 2.30, 9.50 station_load.48= 225, 86.75, 2.00, 9.50 station_load.49= 5500, -50.00, 0.00, 2.50 max_number_of_stations= 50 empty_weight_pitch_MOI= 28900000.00 empty_weight_roll_MOI= 15400000.00 empty_weight_yaw_MOI= 45100000.00 empty_weight_coupled_MOI= 401000.00 [GeneralEngineData] engine_type= 1 Engine.0= 14.00, -29.25, -2.80 Engine.1= -78.50, 0.00, 22.50 Engine.2= 14.00, 29.25, -2.80 fuel_flow_scalar= 0.500 min_throttle_limit=-0.399902 //Series 30 GECF6-50C 51000 LBS MAX [TurbineEngineData] bypass_ratio= 4.8000 fuel_flow_gain= 0.002 inlet_area= 61.000 rated_N2_rpm= 29920.000 static_thrust= 51000.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar= 1.20 [airplane_geometry] wing_area= 3647.00 wing_span= 165.40 wing_root_chord= 39.35 wing_dihedral= 4.20 wing_incidence= 0.70 wing_twist= 0.00 oswald_efficiency_factor= 0.90 wing_winglets_flag= 0 wing_sweep= 35.00 wing_pos_apex_lon= 20.50 wing_pos_apex_vert= 2.60 htail_area= 844.88 htail_span= 71.20 htail_pos_lon= -56.00 htail_pos_vert= 10.00 htail_incidence= 0.80 htail_sweep= 35.00 vtail_area= 452.60 vtail_span= 35.20 vtail_sweep= 35.00 vtail_pos_lon= -60.50 vtail_pos_vert= 28.50 elevator_area= 60.35 aileron_area= 50.28 rudder_area= 40.32 elevator_up_limit= 26.00 elevator_down_limit= 26.00 aileron_up_limit= 26.00 aileron_down_limit= 26.00 rudder_limit= 26.00 elevator_trim_limit= 17.00 spoiler_limit= 60.00 spoilerons_available= 1 aileron_to_spoileron_gain= 1.00 min_ailerons_for_spoilerons= 1.00 min_flaps_for_spoilerons= 0 [Reference Speeds] //AI USE ONLY!! No effect on normal flight. flaps_up_stall_speed= 140 full_flaps_stall_speed= 120 cruise_speed= 600 max_indicated_speed=350.000000 max_mach=0.879980 [contact_points] point.0=1, 67.00, 0.00, -11.90, 1200, 0, 2.0, 68, 0.900, 2.0, 0.7, 8.0, 9.0, 0, 180, 250 //nose point.1=1, -12.00, -18.20, -11.70, 1500, 1, 2.0, 0, 0.887, 2.5, 0.6, 9.9, 10.9, 2, 180, 250 //left main point.2=1, -12.00, 18.20, -11.70, 1500, 2, 2.0, 0, 0.887, 2.5, 0.6, 9.1, 10.1, 3, 180, 250 //right main point.3=1, -11.00, 0.00, -11.70, 1500, 0, 2.0, 0, 0.887, 2.5, 0.6, 9.6, 10.6, 3, 180, 250 //center main point.4=2, -34.00, -86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing point.5=2, -34.00, 86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing point.6=2, -97.50, 0.00, 6.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //nose point.7=2, -93.50, 0.00, 25.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //#2 engine point.8=2, -85.50, 0.00, 11.50, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage point.9=2, -46.50, 0.00, -1.65, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //aft fuselage scrape max_number_of_points= 10 static_pitch= 0.050 static_cg_height= 10.90 gear_system_type=0 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 15.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.900 drag_scalar= 1.200 pitch_scalar= 0.300 system_type= 1 flaps-position.0= 0.000 flaps-position.1= 5.000 flaps-position.2=15.000 flaps-position.3=22.000 flaps-position.4=35.000 flaps-position.5=50.000 [Flaps.1] type= 2 span-outboard= 0.990 extending-time= 5.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.900 drag_scalar= 0.900 pitch_scalar= 0.100 system_type= 1 flaps-position.0= 0.000 flaps-position.1= 5.000 flaps-position.2=15.000 flaps-position.3=22.000 flaps-position.4=35.000 [electrical] autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 pitot_heat = 0, 15, 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 starter3 = 0, 20, 17.0 auto_brakes = 0, 15, 17.0 hydraulic_pump = 0, 2, 17.0 fuel_transfer_pump = 0, 5, 17.0 max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 60.0 electric_always_available = 1 [pitot_static] vertical_speed_time_constant=99 [exits] number_of_exits = 2 exit_rate.0 = 0.105 //L2 main exit door (shift+E) exit_rate.1 = 0.105 //L1 exit door (shift+E2) [TailHook] //landing lights (normally shift+T) tailhook_length= 4 tailhook_position= 0.0, 0.0, 0.0 cable_force_adjust= 0.5 [folding_wings] //cargo doors and R2+L4 galley service doors (normally shift+F) wing_fold_system_type= 4 fold_rates= 0.110,0.110 [Views] //PILOTS CORRECT VIEWPOINT! IF YOU WANT WING VIEWS, ADJUST YOUR PANEL CONFIG! eyepoint=89.75, -2.30, 11.20 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=nose gear light.0=1, -0.90, 0.00, 18.70, DC10BCNU , //upper beacon light.1=1, -30.70, 0.00, -3.00, DC10BCNL , //lower beacon light.2=3, -74.00, -12.00, 34.50, DC10logo , //left logo splash light.3=3, -74.00, 12.00, 34.50, DC10logo , //right logo splash light.4=5, 88.35, -14.50, -4.00, DC10landing , //left landing light splash light.5=5, 88.35, 14.50, -4.00, DC10landing , //right landing light splash light.6=6, 82.00, 0.00, -3.50, DC10wing , //nose gear splash [keyboard_response] elevator= 100, 200 aileron= 100, 200 rudder= 100, 200 [direction_indicators] direction_indicator.0=3,0 [fuel] Center1= 15.00, 0.00, 0.00, 9766, 0 //tank 2 Center2= 0.00, 0.00, 3.00, 13000, 0 //upper aux Center3= 0.00, 0.00, -1.00, 1642, 0 //lower aux LeftMain= -5.00, -27.50, 5.00, 6075, 0 //tank 1 RightMain= -5.00, 27.50, 5.00, 6075, 0 //tank 3 fuel_type= 2 number_of_tank_selectors= 1 electric_pump=0 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 800 autothrottle_available= 1 use_no_default_pitch= 1 use_no_default_bank= 1 pitch_takeoff_ga= 8 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 95 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 [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 [SMOKESYSTEM] [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] smoke.0= 14.00, -29.25, -2.80, fx_smoke_rx smoke.1= -78.50, 0.00, 22.50, fx_smoke_rx smoke.2= 14.00, 29.25, -2.80, fx_smoke_rx [SMOKESYSTEM] smoke.0=0, 14.00, -29.25, -2.80, Opensky_vortex smoke.1=0, -78.50, 0.00, 22.50, Opensky_vortex smoke.2=0, 14.00, 29.25, -2.80, Opensky_conden [brakes] toe_brakes_scale=0.671407 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=24.637185 flap_limit_idle=0.974028 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
