[fltsim.0]
title=Lockheed L1011-200 Tristar
sim=L1011-200
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N728DA
atc_airline=Delta
atc_flight_number=1011
ui_manufacturer=OM Wings
ui_type=L1011-200
ui_variation=L1011-200
description=Lockheed L1011-200 TriStar
atc_heavy=1
visual_damage=1

[General]
atc_type=LOCKHEED
atc_model=L101
atc_heavy=1
atc_id_enable=1
performance=Cruising Speed: 898km/h (484kts) at 35000ft\nMax. Speed: 974km/h (526kts) at 30000ft\nMax. FlightLevel: 42000ft (12802m)\nTake-off field length: 7998ft (2438m)\nLanding field length: 6775ft (2065m)\nRange: 7700km(400 Pass.) / 9047km(Empty)\nPower: 3x Rolls-Royce RB.211-524 at 50.000 lbs thrust\nWingspan: 47.35m\nLength: 54.15m\nWing Area: 321 square meters\nFuselage Diameter: 5.97m

[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=0.9120
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=5.000
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= 1.000, -36.000, -8.500
Engine.1= -71.000, 0.000, 3.500
Engine.2= 1.000, 36.000, -8.500
fuel_flow_scalar= 1.000
min_throttle_limit=-0.199951

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=28.000
rated_N2_rpm=14000.000
static_thrust=36800.000
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar=1.000

[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=14.035
gear_system_type=0

[Views]
eyepoint=76.5, -1.55, 8.2  //(feet) longitudinal, lateral, vertical distance from reference datum

[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, 8848.333, 3.000
LeftMain=-7.000, -35.000, 0.000, 4800.333, 3.000
RightMain=-7.000, 35.000, 0.000, 4800.333, 3.000
LeftAux   =-7.000, -35.000, 0.000,  4048.0, 3.000
RightAux  = -7.000,  35.000, 0.000,  4048.0, 3.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0


[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=0
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
max_indicated_speed=355.000000
max_mach=0.860010

[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
autoland_available=1
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


[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

[brakes]
toe_brakes_scale=1.000000
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]
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

[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=4.000, 0.000
flaps-position.2=10.000, 0.000
flaps-position.3=14.000, 0.000
flaps-position.4=18.000, 0.000
flaps-position.5=22.000, 0.000
flaps-position.6=27.000, 0.000
flaps-position.7=33.000, 0.000
flaps-position.8=45.000, 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=4.000, 0.000
flaps-position.2=10.000, 0.000
flaps-position.3=14.000, 0.000
flaps-position.4=18.000, 0.000
flaps-position.5=22.000, 0.000
flaps-position.6=27.000, 0.000
flaps-position.7=33.000, 0.000
flaps-position.8=45.000, 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-position.7=1.000, 0.000
flaps-position.8=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
flaps-position.7=1.000, 0.000
flaps-position.8=1.000, 0.000