[fltsim.0] title=CDAI L1011500F sim=CDAI L1011500F model= panel= sound= texture= kb_checklists= kb_reference= atc_id= atc_id_color=0xffffffff atc_airline=Delta atc_flight_number=17 ui_manufacturer=CDAI ui_type=Lockheed L1011-500 ui_variation=Delta Airlines atc_heavy=1 description=CDAI L1011-500 for AI Traffic Only! Aircraft design and paint by Charles Dayhuff cdayhuff@comcast.net. FDE by Sam Chin. Wheel and thrust reverser textures by James Campisi. This Aircraft and all files within are FREEWARE. [General] atc_type=Lockheed atc_model=L101 editable=1 performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t39,000 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\nLength: 177 ft 8 in\nWing span: 155 ft 4 in\nMGTW: 504,000 lbs\s EOW: 245,800 lbs\nPower: 3 x 38,000 lb RR RB211-524D4\nDetails: Lockheed L1011-100 \nDesigner:Charles Dayhuff\nDate:08\/20\/03\nPaint:Charles Dayhuff\n\n\n [pitot_static] vertical_speed_time_constant = 1 [WEIGHT_AND_BALANCE] max_gross_weight = 138500.000 empty_weight = 100792.000 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 = 3172439.000 empty_weight_roll_MOI = 2262183.000 empty_weight_yaw_MOI = 3337024.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=0.700 parasite_drag_scalar=0.700 induced_drag_scalar=0.700 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =1.000 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=10.66,-26.83,-5.50 Engine.1=-69.50,0.00,17.33 Engine.2=10.66,26.83,-5.50 fuel_flow_scalar=1.0 min_throttle_limit=-0.150024 reverser_available=1 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 19.600 rated_N2_rpm = 29920.000 static_thrust = 9000.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.000 [fuel] LeftMain= 0.000, -25.000, 0.000, 9750.000, 0.000 RightMain= 0.000, 25.000, 0.000, 9750.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 3457.000 wing_span= 155.000 wing_root_chord= 22.333 wing_dihedral= 6.301 wing_incidence= 0.000 wing_twist= 2.999 oswald_efficiency_factor= 0.824 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 1282.000 htail_span= 71.583 htail_pos_lon= -81.667 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 678.000 vtail_span= 29.688 vtail_sweep= 0.000 vtail_pos_lon= -81.667 vtail_pos_vert= 5.833 elevator_area= 320.500 aileron_area= 138.280 rudder_area= 115.260 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 59.500, 0.000, -14.583, 1574.803, 0.000, 3.427, 72.840, 0.609, 2.500, 0.454, 7.000, 7.000, 0.000, 0.000, 0.000 point.1= 1.000, -10.500, -18.000, -14.583, 1574.803, 1.000, 3.427, 0.000, 0.609, 2.500, 0.454, 8.000, 8.000, 2.000, 0.000, 0.000 point.2= 1.000, -10.500, 18.000, -14.583, 1574.803, 2.000, 3.427, 0.000, 0.609, 2.500, 0.454, 9.000, 9.000, 3.000, 0.000, 0.000 point.3= 2.000, -52.000, -77.500, -2.000, 1574.803, 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, -52.000, 77.500, -2.000, 1574.803, 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, -90.833, 0.000, 0.500, 1574.803, 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, 85.833, 0.000, -2.000, 1574.803, 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= 14.587 gear_system_type=0 [Reference Speeds] flaps_up_stall_speed= 148.000 full_flaps_stall_speed= 118.400 cruise_speed= 499.959 max_indicated_speed=351.265625 max_mach=0.899902 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=-9.957862,-1.499446,7.920153 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 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 [direction_indicators] direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -36.30, -73.56, .90, fx_navredh , light.1=3, -36.30, 73.56, .90, fx_navgreh , light.2=3, -0.00, 0.00, 0.00, fx_navwhih , light.3=2, -36.30, -73.56, .90, fx_strobeh , light.4=2, -36.30, 73.56, .90, fx_strobeh , light.5=2, -0.00, 0.00, 0.00, fx_strobeh , light.6=1, -1.72, 0.00, 12.65, fx_beaconh , light.7=1, 7.90, -2.20, -6.90, fx_beaconb , light.9=2, -44.30, -73.56, .90, fx_strobeh , light.10=2, -44.30, 73.56, .90, fx_strobeh , light.11=1, 7.50, 0.00, 12.65, fx_beaconh , light.12=1, 3.90, 2.20, -6.90, fx_beaconb , [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 10.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 4.999, 0.000 flaps-position.2= 9.998, 0.000 flaps-position.3= 14.997, 0.000 flaps-position.4= 19.996, 0.000 flaps-position.5= 24.995, 0.000 flaps-position.6= 29.994, 0.000 flaps-position.7= 34.993, 0.000 flaps-position.8= 39.992, 0.000 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=-1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0