[FLTSIM.0]
title=Antonov An140
sim=An140
model=
panel=
sound=
texture=
prop_anim_ratio=-1.6
ui_manufacturer=Antonov
ui_type=An140
ui_variation=OdessaAL
atc_id=UR140
atc_airline=OdessaAL
atc_flight_number=UR
visual_damage=1 
description=Antonov An-140  Odessa Airlines Twin engines turboprop 2xPW127A (2х2750 hp)



[General]
atc_type=Antonov
atc_model=An140
editable=0
performance=Crew 3 persons Passenger capacity 52 persons Maximum takeoff weight 19000 kg Maximum payload 6000 kg  Maximum fuel load weight (q = 775 kg/m3) Maximum cruising speed537 km/h    /// copyright by Vlad Zhuhulskiy www.fscargo.narod.ru




\\=====================================================================



[WEIGHT_AND_BALANCE]
max_gross_weight=21500                        // (pounds)
empty_weight=17930                            // (pounds)

reference_datum_position=31.0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-26.0, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50

station_load.0=170,  -9.8, -1.75, 0.0         //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  -9.8,  1.75, 0.0         //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=5660, -27.0,  0.0, 0.0         //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=230701
empty_weight_roll_MOI=71201
empty_weight_yaw_MOI=271691
empty_weight_coupled_MOI=0
======================================================

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.95
aileron_effectiveness=1.0
rudder_effectiveness=0.85
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=5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-28.4, -13.3, 2.7                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-28.4,  13.3, 2.7                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                   //Scalar for fuel flow efficiency

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=13.0                  //Propeller Diameter, (feet)
propeller_blades=6                     //Number of propeller blades
propeller_moi=77                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=12                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=32520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=17.0                  //Propeller gear reduction ratio
fixed_pitch_beta=0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700                   //Minimum RPM for prop feathering
beta_feather=79.3                  //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=32920                 //RPM, second stage compressor rated value
static_thrust=200                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=7878                  //Maximum torque available (ft-lbs)

=======================================================================================
=======================================================================================

[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,  -5.0,    0.00, -7.45, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0, 100, 250
point.1=1,  -29.0, -12.99, -7.55, 3000, 1, 0.633,  0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 2, 100, 250
point.2=1,  -29.0,  12.99, -7.55, 3000, 2, 0.633,  0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 3, 100, 250
point.3=2,  -31.6, -42.50,  5.39, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4=2,  -31.6,  42.50,  5.39, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5=2,  -68.6,   0.00,  1.22, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6=2,    0.0,   0.00, -3.92, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4 

max_number_of_points=21

static_pitch=-0.4             //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.1          //feet, altitude of CG when at rest on the ground
=========================================================================================
===============================================================================



[Views]
eyepoint=-8.8, -1.45, 2.1      //(feet) longitudinal, lateral, vertical distance from reference datum

[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, KIAS
flaps-position.1=10                                   // degrees, KIAS
flaps-position.2=20                                   // degrees, KIAS
flaps-position.3=35                                   // degrees, KIAS
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS

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


[SMOKESYSTEM]
smoke.0=-3.400,-44.00,-16.48, fx_smoke_rx
smoke.1=-3.400,-44.00,16.48, fx_smoke_rx 

===========================================================================
[fuel]
LeftMain=-31.1, -9.1, 3.9, 717.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-31.1,  9.1, 3.9, 717.5, 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                    

===========================================================================

[Reference Speeds]
flaps_up_stall_speed=92.0                  //Knots True (KTAS)
full_flaps_stall_speed=72.0                  //Knots True (KTAS)
cruise_speed=265.0                 //Knots True (KTAS)

[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=1000.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
=============================================================



[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,   -30.6, -38.5,  6.3, fx_navred ,
light.1=3,   -30.6,  38.5,  6.3, fx_navgre ,
light.2=2,   -30.6,  38.5,  6.3, fx_strobe ,
light.3=2,   -30.6, -38.5,  6.3, fx_strobe ,
light.4=1,  -51.0,   0.00, -4.1, fx_beacon ,   \\\1.4
light.5=4,   -7.91,   0.00,  3.64, fx_vclight,
light.6=4,   -8.91,   0.00,  3.64, fx_vclight,
light.7=4,   -50.9,   0.00,  1.64, fx_vclight,
light.8=4,   -52.9,   0.00,  1.64, fx_vclight,
\\light.9=4,   -20.9,   0.00,  1.34, fx_vclight,


[direction_indicators]
direction_indicator.0=3,0

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

=====================================================================

[airplane_geometry]
wing_area=585.000000
wing_span=85.000000
wing_root_chord=7.000000
wing_dihedral=2.499390
wing_incidence=0.999756
wing_twist=-2.999268
oswald_efficiency_factor=0.850061
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=-29.250000
wing_pos_apex_vert=0.000000
htail_area=97.000000
htail_span=26.000000
htail_pos_lon=-66.000000
htail_pos_vert=0.000000
htail_incidence=0.999756
htail_sweep=0.000000
vtail_area=106.000000
vtail_span=11.738824
vtail_sweep=0.000000
vtail_pos_lon=-57.000000
vtail_pos_vert=3.416667
elevator_area=53.500000
aileron_area=12.100000
rudder_area=46.400000
elevator_up_limit=16.999658
elevator_down_limit=15.498508
aileron_up_limit=18.002334
aileron_down_limit=18.002334
rudder_limit=30.000070
elevator_trim_limit=15.000035
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000