[fltsim.0]
title=AI Antonov An-3
sim=An-3
model=
panel=
sound=
texture=
atc_id=N208BC
atc_id_color=0x00000000
atc_parking_types=RAMP
ui_manufacturer=AI Plane an
ui_type=Antonov An-3
ui_variation="White with blue"
description=ADD NEW DESCRIPTION HERE
visual_damage=0
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_parking_codes=AN3

[fltsim.1]
title=Antonov An-3 Blaveschenskie Avialinii
sim=An-3
model=
panel=
sound=
texture=amurskie
atc_id=N208BC
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_airline=Amur Avia
ui_manufacturer=AI Plane an
ui_type=Antonov An-3
ui_variation=Blaveschenskie Avialinii
description=ADD NEW DESCRIPTION HERE
visual_damage=0
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0

[General]
atc_type=ANTONOV 
atc_model=AN3 
editable=0 
performance="Maximum Speed\n289 km\/hr\n\nCruise Speed\n230 km\/hr at 4400 m\n\nEngine\nTVD-20\n\nPropeller\nAV-17\n" 

[weight_and_balance]

// ACM V2.5
max_gross_weight = 12775
empty_weight = 7599
reference_datum_position = 6.345, 0, 0
empty_weight_CG_position = 2, 0, 0
empty_weight_pitch_MOI = 30000
empty_weight_roll_MOI = 18200
empty_weight_yaw_MOI = 36500
empty_weight_coupled_MOI = 0
max_number_of_stations = 0



[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.11, -29.61, 4.44, fx_navred
light.1 = 3, -1.11, 29.69, 4.23, fx_navgre
light.2 = 2, -24.28, 0, 10.03, fx_strobe
light.3 = 2, 4.62, -0.20, -4.60, fx_strobe

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.12
min_throttle_limit = -0.250000
engine.0 = 14.64, 0, -1.73,

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0

LeftMain = 0, -8, 3, 166, 3.6
RightMain = 0, 8, 3, 166, 3.6


[contact_points]
static_pitch = 12.5
static_cg_height = 9.6
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, -23.5, 0, -5.1, 1500, 0, 0.75, 90, 0.3, 2.5, 0.7, 0, 0, 0, 0, 0
point.1 = 1, 2.75, -5.75, -10, 2500, 1, 1.25, 0, 0.3, 2.5, 0.7, 0, 0, 2, 0, 0
point.2 = 1, 2.75, 5.75, -10, 2500, 2, 1.25, 0, 0.3, 2.5, 0.7, 0, 0, 3, 0, 0
point.3 = 2, -0.73, -29.67, 4.4, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -0.73, 29.67, 4.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 6, 0, 0
point.5 = 2, -29.0342, 0, 0.0112, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 13.1258, 0, -3.6594, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000


[forcefeedback]

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.9507,0.8822,0.8822,0,1.8530,1.7644,1.7644
//ACM_AREAW2// 0,1.7553,2.6466,2.6466,0,1.6581,3.5288,3.5288,0,1.5605
//ACM_AREAW3// 4.4109,4.4109,0,1.4630,5.2933,5.2933,0,1.3653,6.1753,6.1753
//ACM_AREAW4// 0,1.2676,7.0577,7.0577,0,1.1704,7.9400,7.9400,0,1.0728
//ACM_AREAH1// 0,0,0,1.1885,0.1981,0.1981,0.0173,1.1466,0.3962,0.3962
//ACM_AREAH2// 0.0346,1.1045,0.5942,0.5942,0.0518,1.0621,0.7924,0.7924,0.0693,1.0203
//ACM_AREAH3// 0.9904,0.9904,0.0864,0.9782,1.1885,1.1885,0.1039,0.9361,1.3868,1.3868
//ACM_AREAH4// 0.1212,0.8938,1.5849,1.5849,0.1386,0.8518,1.7826,1.7826,0.1559,0.8097
//ACM_AREAV1// 0,0,0,1.4630,0.1624,0.1624,0.1624,1.5082,0.3251,0.3251
//ACM_AREAV2// 0.3251,1.5540,0.4875,0.4875,0.4875,1.5994,0.6502,0.6502,0.6502,1.6447
//ACM_AREAV3// 0.8126,0.8126,0.8126,1.6906,0.9753,0.9753,0.9753,1.7359,1.1375,1.1375
//ACM_AREAV4// 1.1375,1.7812,1.3004,1.3004,1.3004,1.8271,1.4630,1.4630,1.4630,1.8724
//ACM_CAREAW1// 3.9700,3.9700,0.9753,1.3653,4.4109,4.4109,0.9753,1.3459,4.8522,4.8522
//ACM_CAREAW2// 0.9753,1.3264,5.2933,5.2933,0.9753,1.3069,5.7343,5.7343,0.9753,1.2874
//ACM_CAREAW3// 6.1753,6.1753,0.9753,1.2676,6.6166,6.6166,0.9753,1.2482,7.0577,7.0577
//ACM_CAREAW4// 0.9753,1.2288,7.4987,7.4987,0.9753,1.2094,7.9400,7.9400,0.9753,1.1899
//ACM_CAREAH1// 0,0,0.5942,1.1885,0.1981,0.1981,0.6115,1.1763,0.3962,0.3962
//ACM_CAREAH2// 0.6290,1.1639,0.5942,0.5942,0.6463,1.1512,0.7924,0.7924,0.6636,1.1390
//ACM_CAREAH3// 0.9904,0.9904,0.6808,1.1267,1.1885,1.1885,0.6983,1.1144,1.3868,1.3868
//ACM_CAREAH4// 0.7156,1.1016,1.5849,1.5849,0.7329,1.0894,1.7826,1.7826,0.7501,1.0772
//ACM_CAREAV1// 0,0,0.3657,1.0972,0.1624,0.1624,0.5281,1.2013,0.3251,0.3251
//ACM_CAREAV2// 0.6908,1.3049,0.4875,0.4875,0.8532,1.4091,0.6502,0.6502,1.0160,1.5132
//ACM_CAREAV3// 0.8126,0.8126,1.1785,1.6174,0.9753,0.9753,1.3408,1.7215,1.1375,1.1375
//ACM_CAREAV4// 1.5036,1.8255,1.3004,1.3004,1.6662,1.9292,1.4630,1.4630,1.8286,2.0336
wing_area = 768.7
wing_span = 59.6
wing_root_chord = 7.7
wing_dihedral = 3.9
wing_incidence = 1.0
wing_twist = 0
oswald_efficiency_factor = 0.95
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon = 1.925
wing_pos_apex_vert = 2.5
htail_area = 132.0
htail_span = 23.6
htail_pos_lon = -21
htail_pos_vert = 3.75
htail_incidence = 1.0
htail_sweep = 0.0
vtail_area = 62.9
vtail_span = 7.1
vtail_sweep = 25
vtail_pos_lon = -18.9
vtail_pos_vert = 2.5
elevator_area = 44.0
aileron_area = 71.83
rudder_area = 20.97
elevator_up_limit = 28.0
elevator_down_limit = 21.0
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 24.0
elevator_trim_limit = 19.5
spoiler_limit = 0.0
aileron_to_spoileron_gain = 1
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[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 

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8                   //Propeller Diameter, (feet)
propeller_blades=3                     //Number of propeller blades
propeller_moi=19                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.6                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=18.77                  //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=0                     //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=88.0                  //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=29850                 //RPM, second stage compressor rated value *
static_thrust=158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=4542                  //Maximum torque available (ft-lbs) *

[Flaps.0]
type=1
span-outboard=0.75       // Percent span for flap position *
extending-time=5.7      // Seconds, time to fully extend
system_type=0           // 0 = electrical
damaging-speed  = 175                                  // KIAS
blowout-speed   = 175                                  // KIAS
flaps-position.0= 0     // degrees
flaps-position.1=10,150     // degrees
flaps-position.2=20,125     // degrees
flaps-position.3=30,100     // degrees

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI

[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 

[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=1,0
[airspeed_indicators]
airspeed_indicator.0 = 1.183, -24.75
[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 3.0  //Brake scalar *
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,0,0,0   //pump on Eng1
[Views]
eyepoint=-12.1, -1.4, 2.12     //(feet) longitudinal, lateral, vertical distance from reference datum

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

[Reference Speeds]
flaps_up_stall_speed=55.0 //78.0                  //Knots True (KCAS)
full_flaps_stall_speed=43.2                  //Knots True (KCAS)	*
cruise_speed=119.0                 //Knots True (KTAS)	*
max_mach                = 0.60
max_indicated_speed     = 140                   ////Red line (KIAS)	*

[autopilot]
autopilot_available=0    // *
flight_director_available=1 
default_vertical_speed=1000.0 
autothrottle_available=0 
pitch_takeoff_ga=8.0 
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=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0

[stall_warning]
type=2