[fltsim.0]
JABIndex=14
title=B717-200 Turkmenistan Airlines
sim=B717-200
model=01
panel=
sound=
texture=tua
checklists=
kb_checklists=
kb_reference=
atc_id=AZ-A101
atc_airline=Turkmenistan Airlines
atc_flight_number=AZ-A101
ui_manufacturer=Boeing
ui_type=717-200
ui_variation=Turkmenistan Airlines
description=Самолет Боинг 717 — развитие линейки McDonnell Douglas DC-9/MD-80/MD-90. Первый полет самолет совершил в июле 1994 года.Среди авиакомпаний, использующих Боинг 717, — AeBal (Балеарские острова), Туркменские Авиалинии и д.р. 
atc_heavy=0




[GENERAL]
atc_type= BOEING
atc_model= B717
Editable    = 0
performance=Крейсерская скорость (км/ч): 811 \ Дальность полета с максимальным запасом топлива (км): 3815

[VIEWS]
eyepoint =  48.487,-1.884,5.135   //Cockpit View Viewpoint

[FORCEFEEDBACK]
stick_shaker_magnitude    = 0
stick_shaker_direction    = 0
stick_shaker_period       = 0
gear_bump_nose_magnitude  = 3000
gear_bump_nose_direction  = 18000
gear_bump_nose_duration   = 250000
gear_bump_left_magnitude  = 2700
gear_bump_left_direction  = 35500
gear_bump_left_duration   = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration  = 250000
ground_bumps_magnitude1   = 1300
ground_bumps_angle1       = 8900
ground_bumps_intercept1   = 3.0
ground_bumps_slope1       = 0.2
ground_bumps_magnitude2   = 200
ground_bumps_angle2       = 9100
ground_bumps_intercept2   = 1.075
ground_bumps_slope2       = 0.035
crash_magnitude1          = 10000
crash_direction1          = 1000
crash_magnitude2          = 10000
crash_direction2          = 9000
crash_period2             = 75000
crash_duration2           = 2500000


[FLIGHT_TUNING]
elevator_effectiveness      =0.85
aileron_effectiveness       =1.0
rudder_effectiveness        =1.1
elevator_trim_effectiveness =1.0
aileron_trim_effectiveness  =1.0
rudder_trim_effectiveness   =1.0
pitch_stability             =1.0
roll_stability              =1.0
yaw_stability               =1.0
cruise_lift_scalar          =1.3
parasite_drag_scalar        =1.0
induced_drag_scalar         =1.0

[WEIGHT_AND_BALANCE]
max_gross_weight         = 110000
empty_weight             = 65700
reference_datum_position =  0.0, 0.0, 0.0
empty_weight_CG_position =  -4.0, 0.0, 0.0
empty_weight_pitch_MOI   = 956815
empty_weight_roll_MOI    = 254787
empty_weight_yaw_MOI     = 801229
empty_weight_coupled_MOI = 0.0
max_number_of_stations   = 10
station_load.0           =  " 380,  42.80, 0.0, 0.0, Pilot (2)"
station_load.1           =  " 570,   5.95, 0.0, 0.0, Cabin (2)"
station_load.2           =  "3040,  25.45, 0.0, 0.0, First (16)"
station_load.3           =  "8550,   7.84, 0.0, 0.0, Coach (45)"
station_load.4           =  "8550, -16.82, 0.0, 0.0, Coach (45)"
station_load.5           =  "2700,  15.32, 0.0, 0.0, Fwd Cargo"
station_load.6           =  "1500, -22.08, 0.0, 0.0, Aft Cargo"


[FUEL]
Center1   =  -8.595,   0.0, 0.0,   893.0, 10.7
LeftMain  = -13.814, -18.0, 0.00, 1393.0,  7.7    
RightMain = -13.814,  18.0, 0.00, 1393.0,  7.7
fuel_type = 2.00
number_of_tank_selectors = 1
electric_pump            = 0


[GENERALENGINEDATA]
engine_type        = 1
Engine.0           = -39.3, -9.1, 3.4
Engine.1           = -39.3,  9.1, 3.4
fuel_flow_scalar   = 1.00
min_throttle_limit = -0.30


[TURBINEENGINEDATA]
fuel_flow_gain        = 0.00100
inlet_area            = 14.7
rated_N2_rpm          = 29920
static_thrust         = 18500
afterburner_available = 0
reverser_available    = 1


[JET_ENGINE]
thrust_scalar =1.0


[AIRPLANE_GEOMETRY]
wing_area                   = 1000.7
wing_span                   = 93.5
wing_root_chord             = 15.9
wing_dihedral               = 3.0
wing_incidence              = 1.0
wing_twist                  = -0.30
oswald_efficiency_factor    = 0.75
wing_winglets_flag          = 0
wing_sweep                  = 29
wing_pos_apex_lon           = 8.575
wing_pos_apex_vert          = 0.0
htail_area                  = 275.6
htail_span                  = 36.85
htail_pos_lon               = -52.12
htail_pos_vert              = 20.00
htail_incidence             = 0
htail_sweep                 = 36
vtail_area                  = 161
vtail_span                  = 14
vtail_sweep                 = 44
vtail_pos_lon               = -41.20
vtail_pos_vert              = 8.570
elevator_area               = 95.8
aileron_area                = 38.0
rudder_area                 = 65.3
elevator_up_limit           = 22.5
elevator_down_limit         = 19.5
aileron_up_limit            = 20.0
aileron_down_limit          = 20.0
rudder_limit                = 26.0
elevator_trim_limit         = 12.0
spoiler_limit               = 45
spoilerons_available        = 1
aileron_to_spoileron_gain   = 2
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons    = 0


[REFERENCE SPEEDS]
flaps_up_stall_speed   = 130
full_flaps_stall_speed = 110
cruise_speed           = 467
max_indicated_speed    = 350
max_mach               = 0.84


[CONTACT_POINTS]
// Gear    0     1        2       3         4   5   6      7    8     9     10    11     12   13     14     15
point.0  = 1,  48.700,   0.000, -7.075, 2500.0, 0, 1.08, 65.0, 1.00, 1.25, 0.66, 15.00, 8.00,  0, 250.0, 300.0
point.1  = 1,  -8.650,  -8.235, -7.500, 2500.0, 1, 1.75,  0.0, 0.75, 1.50, 0.70, 15.00, 8.00,  2, 250.0, 300.0
point.2  = 1,  -8.650,   8.235, -7.500, 2500.0, 2, 1.75,  0.0, 0.75, 1.50, 0.70, 15.00, 8.00,  3, 250.0, 300.0

// Scrapes 0     1        2       3         4   5   6      7    8     9     10    11     12   13     14     15
point.3  = 2,  57.200,   0.000,  0.000,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  4,   0,0,   0.0
point.4  = 2,  52.700,   0.000, -3.000,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  4,   0,0,   0.0
point.5  = 2,   0.000,   0.000, -3.250,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  4,   0,0,   0.0
point.6  = 2, -38.800,   0.000, -2.250,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  4,   0,0,   0.0
point.7  = 2, -57.550,   0.000,  5.250,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  4,   0,0,   0.0
point.8  = 2, -18.750, -43.750,  0.400,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  5,   0,0,   0.0
point.9  = 2, -18.750,  43.750,  0.400,  700.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  0.00, 0.00,  6,   0,0,   0.0

// LL      0     1        2       3         4   5   6      7    8     9     10    11    12    13     14     15
point.10 = 5, -18.590, -43.151,  0.475, 2500.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  4.00, 4.00,  0, 350.0, 400.0
point.11 = 5, -18.590,  43.151,  0.475, 2500.0, 0, 0.00,  0.0, 0.00, 0.00, 0.00,  4.00, 4.00,  0, 350.0, 400.0

max_number_of_points = 15
static_pitch         = 0.35
static_cg_height     = 7.5
gear_system_type     = 1


[FLAPS.0]
type             = 2
span-outboard    = 0.96
extending-time   = 15
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 1
flaps-position.3 = 1
flaps-position.4 = 1
flaps-position.5 = 1
damaging-speed   = 300
blowout-speed    = 350
lift_scalar      = 1.0
drag_scalar      = 1.0
pitch_scalar     = 1.0
system_type      = 1


[FLAPS.1]
type             = 1
span-outboard    = 0.65
extending-time   = 30
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 5
flaps-position.3 = 15
flaps-position.4 = 25
flaps-position.5 = 40
damaging-speed   = 300
blowout-speed    = 350
lift_scalar      = 1.0
drag_scalar      = 1.0
pitch_scalar     = 1.0
system_type      = 1


[ELECTRICAL]
max_battery_voltage           = 24
generator_alternator_voltage  = 28
max_generator_alternator_amps = 65
electric_always_available     = 0
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
starter2                      = 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
standby_vacuum                = 0,  5, 17.0
hydraulic_pump                = 0,  2, 17.0
fuel_transfer_pump            = 0,  5, 17.0
light_recognition             = 0,  5, 17.0
light_wing                    = 0,  5, 17.0
light_logo                    = 0,  5, 17.0


[PITOT STATIC]
vertical_speed_time_constant = 1


[EXITS]
number_of_exits = 2
exit_rate.0     = 0.25
exit_rate.1     = 0.15


[KEYBOARD_RESPONSE]
elevator = 150, 250
aileron  = 150, 250
rudder   = 150, 250


[DIRECTION_INDICATORS]
direction_indicator.0 = 3,0



[AUTOPILOT]
autopilot_available                  = 1
flight_director_available            = 1
default_vertical_speed               = 0
autothrottle_available               = 1
use_no_default_pitch                 = 1
use_no_default_bank                  = 1
pitch_takeoff_ga                     = 12
autothrottle_arming_required         = 1
autothrottle_takeoff_ga              = 1
autothrottle_max_rpm                 = 96.0
default_pitch_mode                   =0
default_bank_mode                    =0
max_pitch                            = 15.0
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                             = 30.0
max_bank_acceleration                = 1.8
max_bank_velocity                    = 3.0
max_throttle_rate                    = 0.1
nav_proportional_control             = 12.0
nav_integrator_control               = 0.5
nav_derivative_control               = 0.01
nav_integrator_boundary              = 0.5
nav_derivative_boundary              = 0.3
gs_proportional_control              = 15.0
gs_integrator_control                = 0.3
gs_derivative_control                = 0.0
gs_integrator_boundary               = 0.7
gs_derivative_boundary               = 0.0
yaw_damper_gain                      = 1.0


[RADIOS]
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


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


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0  =3, -17.387, -45.439,   0.661, fx_navredm,
light.1  =3, -17.631, -45.556,   0.661, fx_navredm,
light.2  =3, -21.612, -45.864,   0.637, fx_navwhi,
light.3  =2, -17.877, -45.745,   0.661, fx_strobe,
light.4  =2, -21.668, -45.739,   0.637, fx_strobe,

light.5  =3, -17.387,  45.439,   0.661, fx_navgrem,
light.6  =3, -17.631,  45.556,   0.661, fx_navgrem,
light.7  =3, -21.612,  45.864,   0.637, fx_navwhi, 
light.8  =2, -17.877,  45.745,   0.661, fx_strobe,
light.9  =2, -21.668,  45.739,   0.637, fx_strobe,

light.10 =1, -16.500,   0.375,  -3.299, fx_beacon,
light.11 =1,  -0.250,   0.375,   8.575, fx_beacon,

light.12 =4,  49.300,  -1.875,   4.000, fx_vclight,
light.13 =4,  49.300,   1.875,   4.000, fx_vclight,


[TAILHOOK]
tailhook_length    = 1
tailhook_position  = 0,0,0
cable_force_adjust = 0.00001


[FOLDING_WINGS]
wing_fold_system_type = 4
fold_rates            = 0.25, 0.25


[brakes]
toe_brakes_scale=0.885037
parking_brake=1


[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit     = 0.10
flap_limit_power       = 25.0
flap_limit_idle        = 15.0


[hydraulic_system]
electric_pumps  = 1
engine_map      = 1,1,0,0
normal_pressure = 3000.0


[stall_warning]
type = 1


[attitude_indicators]
attitude_indicator.0 = 1


[turn_indicators]
turn_indicator.0 = 1,0