[fltsim.0] title=Lockheed L-1011 TF-ABM sim=L1011 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=TF-ABM atc_airline=Iberia atc_flight_number=1123 atc_heavy=1 ui_manufacturer=Lockheed ui_type=L-1011 ui_variation=Iberia TF-ABM visual_damage=1 description=The venerable Lockheed L-1011 TriStar was designed as a medium to long haul airliner in the 250 seat range. The 500 was the long range model designed to make the L-1011 more competitive with the DC-10. Shorter than earlier models, it sacrificed passenger capacity for greater range. The TriStar was well liked by pilots and passengers alike, and no greater tribute can be paid to this old workhorse than the fact that some L-1011's are still in front line service today, 36 years after its maiden flight. [fltsim.1] title=Lockheed L-1011 EI-CNN sim=L1011 model= panel= sound= texture=1 kb_checklists= kb_reference= atc_id=EI-CNN atc_airline=Delta atc_flight_number=1123 atc_heavy=1 ui_manufacturer=Lockheed ui_type=L-1011 ui_variation=Iberia EI-CNN visual_damage=1 description=The venerable Lockheed L-1011 TriStar was designed as a medium to long haul airliner in the 250 seat range. The 500 was the long range model designed to make the L-1011 more competitive with the DC-10. Shorter than earlier models, it sacrificed passenger capacity for greater range. The TriStar was well liked by pilots and passengers alike, and no greater tribute can be paid to this old workhorse than the fact that some L-1011's are still in front line service today, 36 years after its maiden flight. [General] atc_type=LOCKHEED AIRCRAFT atc_model=L-1011 performance=Cruise Speed 552 mph \nEngines 3 RB.211-524B with 49,900 lbs of thrust\nMaximum Range 7000 nm\nService Ceiling 43,300 ft\nMaximum Takeoff Weight 502,942 lbs \nLength 164 ft\nWingspan 164 ft\nHeight 55 ft\nSeating 246 \n [WEIGHT_AND_BALANCE] max_gross_weight= 502000.000 empty_weight= 244000.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI= 24000000.000 empty_weight_roll_MOI= 5500000.000 empty_weight_yaw_MOI= 16300000.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=2.002 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 1 Engine.0= 1.000, -36.000, -8.500 Engine.1= 1.000, 36.000, -8.500 fuel_flow_scalar= 1.000 Engine.2= -71.000, 0.000, 3.500 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 105.000 rated_N2_rpm= 29920.000 static_thrust= 49900.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar=1.250 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 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 gear_warning=0, 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 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 87.420, 0.000, -17.000, 1181.100, 0.000, 4.521, 90.000, 1.630, 2.500, 0.724, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -19.500, -12.000, -17.500, 1574.800, 1.000, 4.521, 0.000, 1.910, 2.500, 0.747, 6.900, 6.900, 2.000, 0.000, 0.000 point.2= 1.000, -19.500, 12.000, -17.500, 1574.800, 2.000, 4.521, 0.000, 1.910, 2.500, 0.747, 7.100, 7.100, 3.000, 0.000, 0.000 point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -14.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -83.330, 0.000, 2.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 16.000 [Views] eyepoint=90.0, -2.65, 8.6 [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 [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=150, 250 aileron=150, 250 rudder=150, 250 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -33.00,-81.50, 1.50, fx_navredh , light.1=3, -33.00, 81.50, 1.50, fx_navgreh , light.2=2, -40.70,-81.30, 1.00, fx_strobeh , light.3=2, -40.70, 81.30, 1.00, fx_strobeh , light.4=1, -4.20, 0.00, -9.40, fx_beaconh , light.5=1, 7.50, 0.00, 9.50, fx_beaconb , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] Center1= 0.000, 0.000, -4.000, 10000.000, 3.000 LeftMain= -7.000, -35.000, 0.000, 10000.000, 3.000 RightMain= -7.000, 35.000, 0.000, 10000.000, 3.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 3540.000 wing_span= 164.000 wing_root_chord= 37.000 wing_dihedral= 5.000 wing_incidence= 1.000 wing_twist= -0.500 oswald_efficiency_factor= 0.800 wing_winglets_flag= 0 wing_sweep= 35.000 wing_pos_apex_lon= 11.000 wing_pos_apex_vert= -4.500 htail_area= 1040.000 htail_span= 68.000 htail_pos_lon= -60.000 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 40.000 vtail_area= 300.000 vtail_span= 26.000 vtail_sweep= 35.000 vtail_pos_lon= -67.000 vtail_pos_vert= 8.000 elevator_area= 120.000 aileron_area= 64.000 rudder_area= 90.000 elevator_up_limit= 30.000 elevator_down_limit= 30.000 aileron_up_limit= 30.000 aileron_down_limit= 15.000 rudder_limit= 25.000 elevator_trim_limit= 20.000 spoiler_limit= 60.000 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 10.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 150.000 full_flaps_stall_speed= 120.000 cruise_speed= 482.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; [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 [Flaps.0] type= 1 span-outboard= 0.300 extending-time= 10.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 0.550 drag_scalar= 0.550 pitch_scalar= 0.550 flaps-position.0= 0.000, 0.000 flaps-position.1= 5.000, 0.000 flaps-position.2= 15.000, 0.000 flaps-position.3= 25.000, 0.000 flaps-position.4= 40.000, 0.000 [Flaps.1] type= 1 span-outboard= 0.900 extending-time= 10.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 0.350 drag_scalar= 0.350 pitch_scalar= 0.350 flaps-position.0= 0.000, 0.000 flaps-position.1= 5.000, 0.000 flaps-position.2= 15.000, 0.000 flaps-position.3= 25.000, 0.000 flaps-position.4= 40.000, 0.000 [Flaps.2] type= 2 span-outboard= 0.300 extending-time= 4.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 0.050 drag_scalar= 0.050 pitch_scalar= 0.050 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.500, 0.000 flaps-position.2= 0.500, 0.000 flaps-position.3= 0.500, 0.000 flaps-position.4= 0.500, 0.000 flaps-position.5= 1.000, 0.000 flaps-position.6= 1.000, 0.000 [Flaps.3] type= 2 span-outboard= 0.900 extending-time= 4.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 0.050 drag_scalar= 0.050 pitch_scalar= 0.050 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.500, 0.000 flaps-position.2= 0.500, 0.000 flaps-position.3= 0.500, 0.000 flaps-position.4= 0.500, 0.000 flaps-position.5= 1.000, 0.000 flaps-position.6= 1.000, 0.000