[fltsim.0]
title=Flyme Boeing MD-80 MD87 FLM
sim=fsp_md87
model=V2
sound=
texture=2
atc_id=SE-RBA
atc_airline=Flybird
atc_flight_number=MD
ui_manufacturer=Active Korea FS Traffic
ui_type=McDonnell-Douglas/Boeing MD-87
ui_variation="FlyMe"
description="Aircraft optimized by Martin Landmann"
atc_parking_codes=RBA
atc_parking_types=GATE



[General]
visual_damage=0 // 0=off, 1=on
atc_type=MCDONNELDOUGLAS
atc_model=MD80
editable=0
performance=FSWINE TP
[WEIGHT_AND_BALANCE]
max_gross_weight = 140000                       // (pounds)
empty_weight = 59686                            // (pounds)
reference_datum_position     =  77.0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -71.0, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 33000, -69.5,  0.0, 0.0        //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI   = 1651967
empty_weight_roll_MOI    =  465681
empty_weight_yaw_MOI     = 1447094
empty_weight_coupled_MOI = 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 = -103.6, -8.5, 0.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -103.6,  8.5, 0.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain          = 0.002                 //Gain on fuel flow
inlet_area              = 10.4                  //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 21000                 //Lbs, max rated static thrust at Sea Level
afterburner_available   = 0                     //Afterburner available?
reverser_available      = 1                     //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[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,   -9.20,   0.00, -8.0, 1500, 0, 1.08, 65.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0
point.1 = 1,  -83.10,  -8.33, -9.1, 3000, 1, 1.85,  1.6, 1.50, 2.5, 0.8, 7.0, 7.0, 2
point.2 = 1,  -83.10,   8.33, -9.1, 3000, 2, 1.85,  1.6, 1.50, 2.5, 0.8, 7.0, 7.0, 3
point.3 = 2,  -95.75, -53.92, -1.0, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2,  -98.75,  53.92, -1.0, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6
point.5 = 2, -139.00,   0.00,  3.0, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9
point.6 = 2,   -3.00,   0.00,  0.0, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4 
max_number_of_points = 21
static_pitch = -0.8          //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height = 8.0         //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint= -13.3, -1.82, 5.0    //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.1]    //Outboard Trailing Edge
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 23                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 0                                    // degrees
flaps-position.2 = 5                                    // degrees
flaps-position.3 = 15                                   // degrees
flaps-position.4 = 20                                   // degrees
flaps-position.5 = 25                                   // degrees
flaps-position.6 = 30                                   // degrees
damaging-speed   = 260                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.35
drag_scalar = 0.35
pitch_scalar= 0.35
system_type = 1                                         //Hydraulic
[flaps.2]     //Inboard Leading Edge Slats
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 4                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 0.5                                  // degrees
flaps-position.2 = 0.5                                  // degrees
flaps-position.3 = 0.5                                  // degrees
flaps-position.4 = 0.5                                  // degrees
flaps-position.5 = 1.0                                  // degrees
flaps-position.6 = 1.0                                  // degrees
damaging-speed   = 260                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.25
drag_scalar = 0.25
pitch_scalar= 2.5
system_type = 1                                         //Hydraulic
[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -95.50,  57,  1.10, fx_navgrem ,
light.1 = 3, -95.50, -57,  1.10, fx_navredm ,
light.2 = 2, -96.50, -57.20, 1.10, fx_strobeh ,
light.3 = 2, -96.50,  57.20, 1.10, fx_strobeh ,
light.4 = 1,  -48.00,   0.00, 8.00, fx_beaconb ,
light.5 = 1,  -72.00,   0.00, -4.60, fx_beaconb ,
light.6 = 7, -115.8 , -9.0 , 1.8 , fx_nicksmokeAI_lrglear-MD-7x // Engine 1
light.7 = 7, -115.8 , 9.0 , 1.8 , fx_nicksmokeAI_lrglear-MD-7x // Engine 2
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1   =  -76.2,   0.0, -6.0,  580.0, 3.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2   =  -78.2,   0.0, -6.0,  580.0, 3.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =  -78.7, -12.1, -4.0, 2920.0, 3.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =  -78.7,  12.1, -4.0, 2920.0, 3.0    //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=0
[airplane_geometry]
wing_area               = 1209.0                //Square feet
wing_span               = 107.8                 //Feet
wing_root_chord         = 23.1                  //Feet
wing_dihedral           = 3.0                   //Degrees
wing_incidence          = 1.3                   //Degrees
wing_twist              = 0.0                   //Degrees
oswald_efficiency_factor= 0.8                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 24.5                  //Degrees, wing leading edge
wing_pos_apex_lon       = -61.0                 //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              = 341.0                 //Square feet
htail_span              = 40.0                  //Feet
htail_pos_lon           = -134.0                //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             = 30.0                  //Degrees, horizontal tail leading edge
vtail_area              = 168.0                 //Square feet
vtail_span              = 14.8                  //Feet, tip to body
vtail_sweep             = 25.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -131.8                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 10.9                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 145.0                 //Square feet
aileron_area            = 38.0                  //Square feet
rudder_area             = 65.3                  //Square feet
elevator_up_limit       = 26.0                  //Degrees
elevator_down_limit     = 26.0                  //Degrees
aileron_up_limit        = 30.0                  //Degrees
aileron_down_limit      = 30.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10                //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed    = 142.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 113.6                 //Knots True (KTAS)
cruise_speed            = 337.7                 //Knots True (KTAS)
max_indicated_speed=340.000000
max_mach=0.820020
[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= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0
[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;
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
[direction_indicators]
direction_indicator.0=3,0
//    Do not remove or edit this section.
//    This section is for PAI Installer information and will not interfere with aircraft behaviour
[Active Korea FS Traffic]
Version=1.0
//    FDE Revision by Oliver Caspers
//
//    End of Active Korea FS Traffic specific settings
[brakes]
toe_brakes_scale=0.289926
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=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
