[fltsim.0]
title=Turkmenistan Airlines Boeing B717-200
sim=pai712v5
model=
panel=
sound=
texture=Turkmenistan
kb_checklists=
kb_reference=
atc_id=
atc_id_color=
atc_airline=Turkmenistan
atc_flight_number=
atc_parking_codes=TKM
atc_parking_types=GATE
ui_manufacturer=AI
ui_type=Boeing 717-200
ui_variation=Turkmenistan Airlines
atc_heavy=0
description=Project Ai B712 Only for use with Ai Traffic!\nmodel by John Rogers\nflight dynamics by Oliver Caspers\n\n! not for commercial use !
visual_damage=0
atc_parking_types=GATE
atc_parking_codes=TUA




//    Do not remove or edit this section.
//    This section is for PAI Installer information and will not interfere with aircraft behaviour
[Project AI]
Version=6.01
//    FDE Revision by Oliver Caspers
//
//    End of Project AI specific settings

[General]
atc_type=BOEING
atc_model=B717
editable=1
performance=


[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight = 118000.0
empty_weight = 67500.0

reference_datum_position     = 10.0, 0.0, 0.0
empty_weight_CG_position     = 2.6, 0.0, 0.0

max_number_of_stations =2

station_load.0 =24500.0, 8.0,0.0,0.0

;Moments of Inertia
empty_weight_pitch_MOI  = 2500000.0
empty_weight_roll_MOI   = 1900000.0
empty_weight_yaw_MOI    = 2900000.0
empty_weight_coupled_MOI        = 0.0
CG_forward_limit= 0.0
CG_aft_limit= 1.0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness =1.3
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 = -26.0, -9.8, 3.25
Engine.1 = -26.0,  9.8, 3.25
fuel_flow_scalar = 1.0
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 16.5
rated_N2_rpm = 29920.0
static_thrust = 21000
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

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.75  //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=49.4, -1.31, 5.9   //(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

[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=0,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2500
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 93
autothrottle_takeoff_ga=1
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[fuel]
Center1 = 1.0, 0.0, -1.0, 1273.0, 0.0
LeftMain  = -2.7, -8.0, 0.0, 1200.0, 0.0
RightMain = -2.7, 8.0, 0.0, 1200.0, 0.0
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[airplane_geometry]
wing_area               = 1000.7
wing_span               = 93.3
wing_root_chord         = 18.3
wing_dihedral           = 2.0
wing_incidence          = 1.0
wing_twist              = 0.0
oswald_efficiency_factor= 0.75
wing_winglets_flag      = 0
wing_sweep              = 26.0
wing_pos_apex_lon       = 4.5
wing_pos_apex_vert      = 0.0
htail_area              = 468.6
htail_span              = 36.9
htail_pos_lon           = -47.5
htail_pos_vert          = 19.5
htail_incidence         = 0.5
htail_sweep             = 35.0
vtail_area              = 194.4
vtail_span              = 14.9
vtail_sweep             = 45.0
vtail_pos_lon           = -35.1
vtail_pos_vert          = 9.1
elevator_area           = 94.6
aileron_area            = 36.8
rudder_area             = 53.2
elevator_up_limit       = 22.5
elevator_down_limit     = 21.5
aileron_up_limit        = 20.0
aileron_down_limit      = 20.0
rudder_limit            = 26.0
elevator_trim_limit     = 20.0
spoiler_limit           = 60.0
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.0
min_ailerons_for_spoilerons = 10.0
min_flaps_for_spoilerons = 0.0

[Reference Speeds]
flaps_up_stall_speed    = 129.0
full_flaps_stall_speed  = 102.0
cruise_speed            = 499.0
max_mach                = 0.86
max_indicated_speed     = 340                   //Red line (KIAS)

[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

[stall_warning]
type=2

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1                                    // degrees
flaps-position.2 = 2                                    // degrees
flaps-position.3 = 5                                    // degrees
flaps-position.4 = 10                                   // degrees
flaps-position.5 = 20                                   // degrees
flaps-position.6 = 30                                   // degrees
flaps-position.7 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Outboard Leading Edge Slat
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 3                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 0.5                                  // 
flaps-position.4 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -13.0, -46.20,  0.95, fx_navredm ,
light.1=3, -13.0,  46.20,  0.95, fx_navgrem ,
light.2=2, -13.0, -46.20,  0.95, fx_strobeh ,
light.3=2, -13.0,  46.20,  0.95, fx_strobeh ,
light.4=1,  -4.1,   0.00,  -3.10, fx_beaconb ,
light.5=1,  2.5,   0.00,  8.95, fx_beaconh ,
light.6=3, -16.7, -46.55,  0.95, fx_navwhih ,
light.7=3, -16.7,  46.55,  0.95, fx_navwhih ,
light.8=2, -16.7, -46.55,  0.95, fx_strobeh ,
light.9=2, -16.7,  46.55,  0.95, fx_strobeh ,

        //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=1.0, 42.0, 0.0, -6.3, 1181.1, 0.0, 1.44, 55.9,0.6, 2.5, 0.8, 4.0, 4.0, 0.0, 0.0, 0.0
point.1=1.0, -5.2,-10.0, -6.9, 1574.8, 1.0, 1.44, 0.0, 0.9, 2.5, 0.85,6.9, 6.9, 2.0, 0.0, 0.0
point.2=1.0, -5.2, 10.0, -6.9, 1574.8, 2.0, 1.44, 0.0, 0.9, 2.5, 0.85,7.1, 7.1, 3.0, 0.0, 0.0

point.3=2.0, -23.4, -46.7, 1.3, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0, -23.4, 46.7, 1.3, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0, -52.8, 0.000, 3.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0, 42.8, 0.000, -2.6, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0

max_number_of_points=7

static_pitch=-0.2
static_cg_height=6.3
gear_system_type=1      //Hydraulic