[fltsim.0]
title=Mercedes_SL600
sim=Mercedes_SL600
model=
panel=
sound=
texture=
panel_alias = Mercedes_SL600\panel
sound_alias = Mercedes_SL600\sound
kb_checklists=
kb_reference=
atc_id=N1998MB
ui_manufacturer=Mercedes-Benz
ui_type=2-Door Luxury
ui_variation=First set of rims
description=Enter your description here.

[fltsim.1]
title=Mercedes_SL600_01
sim=Mercedes_SL600
model=1
panel=
sound=
texture=
panel_alias = Mercedes_SL600\panel
sound_alias = Mercedes_SL600\sound
kb_checklists=
kb_reference=
atc_id=N1998MB
ui_manufacturer=Mercedes-Benz
ui_type=2-Door Luxury
ui_variation=Second set of rims
description=Enter your description here.

[fltsim.2]
title=Mercedes_SL600_02
sim=Mercedes_SL600
model=2
panel=
sound=
texture=
panel_alias = Mercedes_SL600\panel
sound_alias = Mercedes_SL600\sound
kb_checklists=
kb_reference=
atc_id=N1998MB
ui_manufacturer=Mercedes-Benz
ui_type=2-Door Luxury
ui_variation=Third set of rims
description=Enter your description here.

[General]
atc_type=
atc_model=
editable=1
performance=Enter your performance information here.

[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0                      // (pounds)
empty_weight = 11700.0                          // (pounds)

reference_datum_position     =   0.0, 0.0, 0.0    // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =   0.0, 0.0, -2.703    // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 1

station_load.0  = 170, 0.0, -1.518, -1.341         //Pilot    Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI   = 50000
empty_weight_roll_MOI    = 45000
empty_weight_yaw_MOI     = 70000
empty_weight_coupled_MOI = 0.0

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 5 , 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 2 , 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -4.0, 0.0, 0.0                     //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit = 0.0                      //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain          = 0.0025                //Gain on fuel flow
inlet_area              = 4.2895                //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 3500                  //Lbs, max rated static thrust at Sea Level
afterburner_available   = 0                     //Afterburner available?
reverser_available      = 0                     //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

        //0  Class
        //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
[contact_points]
point.0=1,   5.94, -2.604, -2.703, 1574.8, 0, 1.5, 46.8, 0.4798, 2.5, 1, 10.0, 10.0, 0, 0.0, 0.0
point.1=1,   5.94,  2.604, -2.703, 1574.8, 0, 1.5, 46.8, 0.4798, 2.5, 1,  9.0,  9.0, 0, 0.0, 0.0
point.2=1, -2.586, -2.604, -2.703, 1574.8, 1, 1.5,  0.0, 0.4798, 2.5, 1,  9.0,  9.0, 2, 0.0, 0.0
point.3=1, -2.586,  2.604, -2.703, 1574.8, 2, 1.5,  0.0, 0.4798, 2.5, 1,  9.0,  9.0, 3, 0.0, 0.0
point.4=2,    0.0,   -5.0,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.5=2,    0.0,    5.0,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.6=2,  -7.00,   0.00,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.7=2,   7.00,   0.00,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

static_pitch = 0.0
static_cg_height = 4.0
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 16.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint = -1.7, -1.7, 1.5

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 8                                    // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Nav.1         = 1, 0, 1
Nav.2         = 1, 0, 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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[fuel]
LeftMain  = 0.0, 0.0, -3.0, 50, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1

[airplane_geometry]
wing_area               = 0.0                 //Square feet
wing_span               = 0.0                  //Feet
wing_root_chord         = 0.0                   //Feet
wing_dihedral           = 0.0                   //Degrees
wing_incidence          = 0.0                   //Degrees
wing_twist              = 0.0                  //Degrees
oswald_efficiency_factor= 0.0                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 0.0                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 0.0                  //Square feet
htail_span              = 0.0                  //Feet
htail_pos_lon           = 0.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 0.0                  //Degrees, horizontal tail leading edge
vtail_area              = 42.0                  //Square feet
vtail_span              = 7.4                   //Feet, tip to body
vtail_sweep             = 30.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -55.0                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 4.1                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 0.0                  //Square feet
aileron_area            = 0.0                  //Square feet
rudder_area             = 7.3                   //Square feet
elevator_up_limit       = 0.0                  //Degrees
elevator_down_limit     = 0.0                  //Degrees
aileron_up_limit        = 0.0                  //Degrees
aileron_down_limit      = 0.0                  //Degrees
rudder_limit            = 25                  //Degrees
elevator_trim_limit     = 0.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 4.6                 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5                 //Degrees
min_flaps_for_spoilerons= 0.0                   //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 100.0                 //Knots True (KTAS)
full_flaps_stall_speed  =  80.0                 //Knots True (KTAS)
cruise_speed            = 80.0                 //Knots True (KTAS)
max_mach                = 0.90
max_indicated_speed=130.000000

[autopilot]
autopilot_available= 0
flight_director_available= 0
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0


[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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

[stall_warning]
type=0