[fltsim.0]
title=FSP MD83 AMXEXICO
sim=fsp_md81
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=XA-ETZ
atc_airline=AEROMEXICO
atc_flight_number=163
ui_manufacturer=Mc Donnell Douglas
ui_type=MD-83
ui_variation=Aeromexico
description=COMPLETE NEW DESIGN BY STEFFANO ESCAMILLA
atc_heavy=0








[General]
visual_damage=0 // 0=off, 1=on
atc_type=MCDONNELDOUGLAS
atc_model=MD80
performance=Џ„Ќq‘¬“x\t\tѓ}ѓbѓn .74\nЌЕ‘еЌq‘±‹——Ј\t2,059 ЉC—ў\nЋА—pЏгЏёЊА“x\t36,089 ѓtѓBЃ[ѓg\nЌЕ‘е—Ј—¤Џd—К\t138,500 ѓ|ѓ“ѓh\nЌАђИђ”\t\t147 Ѓ` 168\n‰Э•Ё—e—К\t\t1,373 —§•ыѓtѓBЃ[ѓg\n

[WEIGHT_AND_BALANCE]
max_gross_weight = 140000.000
empty_weight = 59686.000

reference_datum_position     = 77.000, 0.000, 0.000
empty_weight_CG_position     = -71.000, 0.000, 0.000
max_number_of_stations = 50

station_load.0 = 33000.000, -69.500, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI   = 1651967.000
empty_weight_roll_MOI    = 465681.000
empty_weight_yaw_MOI     = 1447094.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[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
Engine.0 = -103.600, -8.500, 0.600
Engine.1 = -103.600, 8.500, 0.600
fuel_flow_scalar        = 1.000

[TurbineEngineData]
fuel_flow_gain          = 0.002
inlet_area              = 10.400
rated_N2_rpm            = 29920.000
static_thrust           = 21000.000
afterburner_available   = 0
reverser_available      = 1

[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 = 1.000, -9.200, 0.000, -8.000, 1500.000, 0.000, 1.080, 65.000, 1.000, 2.500, 0.900, 7.000, 5.000, 0.000, 0.000, 0.000
point.1 = 1.000, -83.100, -8.330, -9.100, 3000.000, 1.000, 1.850, 1.600, 1.500, 2.500, 0.800, 7.000, 7.000, 2.000, 0.000, 0.000
point.2 = 1.000, -83.100, 8.330, -9.100, 3000.000, 2.000, 1.850, 1.600, 1.500, 2.500, 0.800, 7.000, 7.000, 3.000, 0.000, 0.000
point.3 = 2.000, -95.750, -53.920, -1.000, 1200.000, 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, -98.750, 53.920, -1.000, 1200.000, 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, -139.000, 0.000, 3.000, 1200.000, 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, -3.000, 0.000, 0.000, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 
 
max_number_of_points = 21


static_pitch = -0.800
static_cg_height = 8.000

[Views]
eyepoint= -13.3, -1.82, 5.0    //(feet) longitudinal, lateral, vertical distance from reference datum



[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,  -38.00,   0.00, 8.50, fx_beaconb ,
light.5 = 1,  -72.00,   0.00, -4.60, fx_beaconb ,

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

[fuel]
Center1   = -76.200, 0.000, -6.000, 580.000, 3.000
Center2   = -78.200, 0.000, -6.000, 580.000, 3.000
LeftMain  = -78.700, -12.100, -4.000, 2920.000, 3.000
RightMain = -78.700, 12.100, -4.000, 2920.000, 3.000
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    

[airplane_geometry]
wing_area               = 1209.000
wing_span               = 107.800
wing_root_chord         = 23.100
wing_dihedral           = 3.000
wing_incidence          = 1.300
wing_twist              = 0.000
oswald_efficiency_factor= 0.800
wing_winglets_flag      = 0
wing_sweep              = 24.500
wing_pos_apex_lon       = -61.000
wing_pos_apex_vert      = 0.000
htail_area              = 341.000
htail_span              = 40.000
htail_pos_lon           = -134.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 30.000
vtail_area              = 168.000
vtail_span              = 14.800
vtail_sweep             = 25.000
vtail_pos_lon           = -131.800
vtail_pos_vert          = 10.900
elevator_area           = 145.000
aileron_area            = 38.000
rudder_area             = 65.300
elevator_up_limit       = 26.000
elevator_down_limit     = 26.000
aileron_up_limit        = 30.000
aileron_down_limit      = 30.000
rudder_limit            = 30.000
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    = 142.000
full_flaps_stall_speed  = 113.600
cruise_speed            = 330.000

[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;

[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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 23.000
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= 0.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.500
extending-time= 4.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar= 0.250
drag_scalar= 0.250
pitch_scalar= 2.500
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