[fltsim.0] title=SGA DC-10-30F Varig F sim=SGA1030 model=30F panel= sound= texture=variglog kb_checklists= kb_reference= atc_airline=Varig atc_flight_number=472 atc_id= atc_heavy=1 ui_manufacturer=McDonnell Douglas ui_type=DC10-30F ui_variation=Varig Log atc_parking_types=GATE //GATE, RAMP, CARGO etc. atc_parking_codes=FED //UAL, AAL etc visual_damage=1 description=Varig Log repaint by Capt. Wes Archibald. 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. [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 [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 [fltsim.2] title=SGA DC-10-30F Varig F sim=SGA1030 model=30F panel= sound= texture=2 kb_checklists= kb_reference= atc_airline=Varig atc_flight_number=472 atc_id= atc_heavy=1 ui_manufacturer=McDonnell Douglas ui_type=DC10-30F ui_variation=Varig Log atc_parking_types=GATE //GATE, RAMP, CARGO etc. atc_parking_codes=FED //UAL, AAL etc visual_damage=1 description=Varig Log repaint by Capt. Wes Archibald. 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.
