[General] atc_type=MCDONELDOUGLAS 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 0.82-0.84 [fltsim.0] title=SGA DC-10-30 Surclaro sim=SGA1030 model=30 panel= sound= texture=Surclaro kb_checklists= kb_reference= ui_manufacturer=McDonnell Douglas ui_type=DC-10-30 ui_variation=Surclaro visual_damage=0 description=Model by SGA, Repaint by Exx/Gonzalo. The Series 30 offered considerably improved payload and range capability with increased fuel capacity and thrust, which necessitated an increase of 10 feet in wingspan and the addition of a center main landing gear assembly. Most popular of all the variants, a total of 206 Series 30s were built, including 27 -30CFs, 4 extended range -30ERs, and 12 pure freighter -30Fs. Unlike the Series 10, most -30s were ordered without the optional lower deck galley to allowed increased cargo capacity. First revenue flight for a Series 30ER was on December 15, 1972 with Swissair. The Series 30CF (Convertible Freighter) was first certified in March 1973 and placed into revenue service in April 1973. atc_heavy=1 atc_id=CC-GBE atc_airline=Surclaro atc_flight_number=269 [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= 1.00 parasite_drag_scalar= 1.00 induced_drag_scalar= 1.00 elevator_effectiveness= 1.00 aileron_effectiveness= 1.00 rudder_effectiveness= 1.00 pitch_stability= 1.00 roll_stability= 1.00 yaw_stability= 1.00 elevator_trim_effectiveness= 1.00 aileron_trim_effectiveness= 1.00 rudder_trim_effectiveness= 1.00 [WEIGHT_AND_BALANCE] //DC10 Series 30 max_gross_weight= 558000.00 //Design gross weight (ramp) 558,000 lb (260,820 kg) empty_weight= 238036.00 //Maximum takeoff weight 555,000 lb (259,459 kg) reference_datum_position= 0.00, 0.00, 0.00 //Design landing weight (1) 411,000 lb (182,766 kg) empty_weight_CG_position= -1.23, 0.00, 6.00 //Maximum zero fuel weight 391,000 lb (166,924 kg) station_load.0= "180, 89.221, -2.267, 9.7, Pilot" station_load.1= "180, 89.221, 2.267, 9.7, Co-Pilot" station_load.2= "180, 85.497, 2.267, 9.7, F/E" station_load.3= "360, 77.024, 0.000, 9.7, Crew 1" station_load.4= "8316, 64.000, 0.000, 9.7, Zone A" station_load.5= "8316, 53.000, 0.000, 9.7, Zone B" station_load.6= "8316, 42.000, 0.000, 9.7, Zone C" station_load.7= "8316, 31.000, 0.000, 9.7, Zone D" station_load.8= "8316, 20.000, 0.000, 9.7, Zone E" station_load.9= "14360, 9.000, 0.000, 9.7, Zone F" station_load.10= "14360, -2.000, 0.000, 9.7, Zone G" station_load.11= "14360, -13.000, 0.000, 9.7, Zone H" station_load.12= "10142, -24.000, 0.000, 9.7, Zone I" station_load.13= "8316, -35.000, 0.000, 9.7, Zone J" station_load.14= "8316, -46.000, 0.000, 9.7, Zone K" station_load.15= "15000, 48.500, 0.000, 1.6, Fwd Lower Cargo" station_load.16= "15000, -30.000, 0.000, 1.6, Aft Lower Cargo" station_load.17= "500, -51.733, 0.000, 2.5, Bulk Cargo" //Over all payload above minus crew = 142544 lb max_number_of_stations= 20 //FAA takeoff field lgth-std.wght 9,650 ft(2,847 m) empty_weight_pitch_MOI= 12229499 //FAA landing field lgth-std.wght 5,960 ft(1,758 m) empty_weight_roll_MOI= 4035153 //Design range (2) 5,860 mi empty_weight_yaw_MOI= 11280172 //5,096 nmi empty_weight_coupled_MOI= 0.00 //9,429 km // (1)Higher weights are available. // (2)277 passengers and baggage; domestic reserves. // Passenger Capacity 250-380 CG_FORWARD_LIMIT= 5.58 CG_AFT_LIMIT= 1.265 [GeneralEngineData] engine_type= 1 Engine.2= 14.00, 29.25, -2.80 Engine.0= 14.00, -29.25, -2.80 Engine.1= -78.50, 0.00, 22.50 min_throttle_limit=-0.299927 fuel_flow_scalar=0.77 [TurbineEngineData] bypass_ratio= 4.24 //fuel_flow_gain= 0.0019 fuel_flow_gain= 0.0019 inlet_area= 60.13 rated_N2_rpm= 10761 //N2 at 109.5%, N1 @ 4068rpm @ 119.5% static_thrust= 46300 //46300 max continuous afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar= 1.00 [airplane_geometry] wing_area= 3958.7 wing_span= 165.33 wing_root_chord= 35.145 wing_dihedral= 6.00 wing_incidence= 0.00 wing_twist= -0.50 oswald_efficiency_factor= 0.75 wing_winglets_flag= 0 wing_sweep= 35.0 wing_pos_apex_lon= 27.64 wing_pos_apex_vert= 2.60 htail_area= 1231.10 htail_span= 71.20 htail_pos_lon= -51.61 htail_pos_vert= 10.00 htail_incidence= 0.00 htail_sweep= 33.00 vtail_area= 479.00 vtail_span= 24.25 vtail_sweep= 45.00 vtail_pos_lon= -60.50 vtail_pos_vert= 28.50 elevator_area= 325.00 aileron_area= 255.39 rudder_area= 161.00 elevator_up_limit= 26.00 elevator_down_limit= 20.00 aileron_up_limit= 30.00 aileron_down_limit= 30.00 rudder_limit= 33.00 elevator_trim_limit= 24.00 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] flaps_up_stall_speed= 192 full_flaps_stall_speed= 130 cruise_speed= 600 max_indicated_speed= 360 max_mach= 0.88 [contact_points] point.0=1, 67.00, 0.00, -11.80, 1200, 0, 2.0, 68, 0.900, 2.0, 0.7, 8.0, 9.0, 0, 210, 250 point.1=1, -11.00, 0.00, -11.90, 1500, 0, 2.0, 0, 0.887, 2.5, 0.6, 9.6, 10.6, 3, 210, 250 point.2=1, -12.00, -18.20, -11.70, 1500, 1, 2.0, 0, 0.887, 2.5, 0.6, 9.9, 10.9, 1, 210, 250 point.3=1, -12.00, 18.20, -11.70, 1500, 2, 2.0, 0, 0.887, 2.5, 0.6, 9.1, 10.1, 2, 210, 250 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 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 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 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 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 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 max_number_of_points= 11 static_pitch= 0.5 static_cg_height= 10.90 gear_system_type= 1 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 20.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.4 drag_scalar= 0.6 pitch_scalar= 0.3000 system_type= 1 flaps-position.0= 0.000 flaps-position.1= 0.000 //LEADING EDGE SLATS EXTEND ONLY-TRAILING EDGE FLAPS REMAIN DOCKED flaps-position.2= 5.000 flaps-position.3=15.000 //UNDER MAX TAKEOFF WEIGHT-10,000FT+ EXTENDED LENGTH RUNWAYS-TAKEOFF CONFIGURATION flaps-position.4=22.000 //NORMAL FULL LOAD TAKEOFF CONFIGURATION (WITHIN TAKEOFF WEIGHT LIMITS) flaps-position.5=35.000 //NORMAL LANDING CONFIGURATION WITH APPROPRIATE AIRCRAFT LANDING WEIGHTS flaps-position.6=50.000 //USED ONLY ON WET RUNWAY SUFACES OR RUNWAYS WITH A LENGTH LESS THAN 7000 FEET [Flaps.1] type= 2 span-outboard= 0.80 extending-time= 10.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.200 drag_scalar= 0.5 pitch_scalar= 0.20 system_type= 1 flaps-position.0= 0.000 flaps-position.1=15.000 //NORMAL HALF EXTEND-TAKEOFF CONFIGURATION flaps-position.2=15.000 flaps-position.3=15.000 flaps-position.4=15.000 flaps-position.5=35.000 //FULL EXTEND-LANDING CONFIGURATION flaps-position.6=35.000 [Flaps.2] type= 2 span-outboard= 0.18 extending-time= 10.000 damaging-speed= 280 blowout-speed= 300 lift_scalar= 0.200 drag_scalar= 0.4 pitch_scalar= 0.10 system_type= 1 flaps-position.0= 0.000 flaps-position.1=15.000 //NORMAL HALF EXTEND-TAKEOFF CONFIGURATION flaps-position.2=15.000 flaps-position.3=15.000 flaps-position.4=15.000 flaps-position.5=25.4 //FULL EXTEND-LANDING CONFIGURATION flaps-position.6=25.4 [electrical] autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump1 = 0, 5 , 17.0 fuel_pump2 = 0, 5 , 17.0 fuel_pump3 = 0, 5 , 17.0 fuel_pump4 = 0, 5 , 17.0 fuel_pump5 = 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 hydraulic_pump1 = 0, 2, 17.0 hydraulic_pump2 = 0, 2, 17.0 hydraulic_pump3 = 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 = 0 engine_generator_map= 1, 1, 1, 0 [pitot_static] vertical_speed_time_constant=99.0 [exits] number_of_exits = 2 exit_rate.0 = 0.105 exit_rate.1 = 0.105 [TailHook] //Extends Landing light pods 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 wing_fold_system_type= 4 fold_rates= 0.110,0.110 [Views] eyepoint= 89.20, -2.30, 11.30 //PILOTS CORRECT VIEWPOINT [LIGHTS] //Types: 1 Beacon,2 Strobe,3 Navigation,4 Cockpit,5 Landing,6 Taxi,7 Recognition,8 Wing,9 Logo,10 Cabin (7-10 REQUIRE GAUGE) light.0=1, -0.90, 0.00, 18.70, DC10.4BCNU , light.1=1, -30.90, 0.00, -3.00, DC10.4BCNL , light.2=3, -74.00, -12.00, 34.50, DC10.4logo , light.3=3, -74.00, 12.00, 34.50, DC10.4logo , light.4=5, 80.50, -10.50, 1.10, DC10.4landing , light.5=5, 80.50, 10.50, 1.10, DC10.4landing , [keyboard_response] elevator= 100, 200 aileron= 100, 200 rudder= 100, 200 [direction_indicators] direction_indicator.0=3,0 [fuel] Center1= -0.82, 0.00, -1.50, 10372, 1000 //Tank 2 Center2= 1.48, 0.00, 4.50, 15543, 1000 //Center LeftMain= -17.20, -47.00, 4.50, 6448, 1000 //tank 1 RightMain= -17.20, 47.00, 4.50, 6448, 1000 //tank 3 fuel_type= 2 number_of_tank_selectors= 1 electric_pump=1 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1400 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= 110 default_pitch_mode=0 default_bank_mode=0 max_pitch= 10.00 max_pitch_acceleration= 3.00 max_pitch_velocity_lo_alt= 4.00 max_pitch_velocity_hi_alt= 2.00 max_pitch_velocity_lo_alt_breakpoint= 20000 max_pitch_velocity_hi_alt_breakpoint= 28000 max_bank= 25.00 max_bank_acceleration= 2.0 max_bank_velocity= 3.0 max_throttle_rate= 0.20 nav_proportional_control= 21.00 nav_integrator_control= 0.05 nav_derivative_control= 0.00 nav_integrator_boundary= 1.00 nav_derivative_boundary= 0.00 gs_proportional_control= 20.0 gs_integrator_control= 0.01 gs_derivative_control= 0.00 gs_integrator_boundary= 1.00 gs_derivative_boundary= 0.00 yaw_damper_gain= 0.2 [Radios] Audio.1= 1 Com.1= 1, 1 Com.2= 1, 1 Nav.1= 1, 1, 1 Nav.2= 1, 1, 0 Adf.1= 1 Adf.2= 0 Transponder.1= 1 Marker.1= 1 [SMOKESYSTEM] [EFFECTS] wake= fx_wake water= fx_spray dirt= fx_tchdrt concrete= fx_sparks touchdown= fx_tchdwn, 1 Contrail= startup= windshield_rain_effect_available=1 //0= OFF, 1= ON [brakes] toe_brakes_scale= 0.559 parking_brake= 1 [gear_warning_system] gear_warning_available= 1 pct_throttle_limit= 5.00 flap_limit_power= 24.637 flap_limit_idle= 24.637 [hydraulic_system] electric_pumps= 0 engine_map= 1,1,1,0 normal_pressure= 3000 [stall_warning] type= 1 [attitude_indicators] attitude_indicator.0= 1 [turn_indicators] turn_indicator.0= 1,0 [FSHS_AIBLAST] OldName=MCDONNELDOUGLAS NewName=mcdonneLdoUGLAS
