[fltsim.0]
title=AI Aeroflot Antonov An-10A 1966 c/s
sim=AN10
model=
texture=11213
ui_variation=11213
ui_manufacturer=AI
ui_type=Ан-10
description=An-12 N11120\n
atc_parking_types=GATE,RAMP
atc_parking_codes=AN0,AFL

[fltsim.1]
title=AI Aeroflot Antonov An-10A 1959 c/s
sim=AN10
model=
texture=11185
ui_variation=11185
ui_manufacturer=AI
ui_type=Ан-10
description=An-12 N11120\n
atc_parking_types=GATE,RAMP
atc_parking_codes=AN0,AFL

[fltsim.2]
title=AI Aeroflot Antonov An-10A 1966 c/s 'Deer'
sim=AN10
model=
texture=11174
ui_variation=11174
ui_manufacturer=AI
ui_type=Ан-10
description=An-12 N11120\n
atc_parking_types=GATE,RAMP
atc_parking_codes=AN0,AFL

[General]
atc_type=Antonov
atc_model=AN10
editable = 1
performance =AN10
Category=airplane

[LIGHTS]
light.0 =  3,  4.5, -61.6,  6.5, fx_navred
light.1 =  3,  4.5,  61.6,  6.5, fx_navgre
light.2 =  3, -54.0,   0,    7.0, fx_navwhi
light.3 =  1,  -8.5,   0,   -6.36, fx_beaconb
light.4 =  1, -48.5,   0,   24.5, fx_beaconb
light.5 = 5,4.388, -30.80, 1.6,  cs130_smoke, // Engine 1
light.6 = 5,4.217, -14.80, 1.6,  cs130_smoke, // Engine 2
light.7 = 5,4.217, 14.80, 1.6,  cs130_smoke, // Engine 3
light.8 = 5,4.388, 30.80, 1.6,  cs130_smoke, // Engine 4

[WEIGHT_AND_BALANCE]
empty_weight=71000 
max_gross_weight=155000         
reference_datum_position=0.0, 0.0, 0.0       // (feet) 
empty_weight_CG_position=4.8, 0.0, 0.0       // (feet) 
max_number_of_stations=50
station_load.0 = "170.0, 31.0, -1.5, 0.0, Pilot"
station_load.1 = "170.0, 31.0, 1.5, 0.0, Co-Pilot"
station_load.2 = "510.0, 25.0, 0.0, 0.0, Crew"
station_load.3 = "7000.0, 5.0, 0.0, 0.0, Payload"
;Moments of Inertia
empty_weight_pitch_MOI=1000000
empty_weight_roll_MOI=696271
empty_weight_yaw_MOI=1289428 
empty_weight_coupled_MOI=0

[GeneralEngineData]
engine_type=5                          //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0= -5.0, -33.8, 4.0              //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1= -5.0, -16.8, 4.0
Engine.2= -5.0,  16.8, 4.0
Engine.3= -5.0,  33.8, 4.0
fuel_flow_scalar=1.00                  //Scalar for fuel flow efficiency
min_throttle_limit= -0.30
max_contrail_temperature=-27

[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        = 4                     //Number of propeller blades
propeller_moi           = 100                   //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             = 25520                 //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            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 6000                  //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 12000                 //Maximum torque available (ft-lbs)


[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.7
aileron_effectiveness=1.7
rudder_effectiveness=1.0
pitch_stability=1.9
roll_stability=0.4
yaw_stability=1.0
elevator_trim_effectiveness=1.3
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=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]
        //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)
max_number_of_points = 12
point.0 = 1, 26.5,  0,   -10.45, 2000, 0, 2.00, 55.92, 0.75, 0.9, 0.8, 5, 5, 0, 0, 0
point.1 = 1, -7.5, -9.0,  -9.80, 2000, 1, 3.47,  0.00, 0.85, 0.9, 0.7, 5, 5, 2, 0, 0
point.2 = 1, -7.5,  9.0,  -9.80, 2000, 2, 3.47,  0.00, 0.85, 0.9, 0.7, 5, 5, 3, 0, 0
 
point.3 = 2,  39.251,  0,     -3.675, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.4 = 2, -64.5,    0,      5.5, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.5 = 2, -21.0,    0,     -6.36, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.6 = 2, -11.893,-61.6,    6.5, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.7 = 2, -11.893, 61.6,    6.5, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.8 = 2, -59.668, -0.306, 26.95, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.9 = 2,  22.1,    0,     -7.044, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.10 = 2,-14.65,  -5.819, -7.044, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.11 = 2,-14.65,   4.593, -7.044, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0
static_pitch= 1.2
static_cg_height= 9.8		//9.2
gear_system_type=1

[Views]
eyepoint=35.0, -1.20, 5.0

[flaps.0]
type=1                                 
span-outboard=0.8                             
extending-time=10                                
flaps-position.0=0		
flaps-position.1=5		
flaps-position.2=15			
flaps-position.3=25
flaps-position.4=40
damaging-speed=250                                 
blowout-speed=300                                 
lift_scalar=0.5
drag_scalar=0.5
pitch_scalar=0.0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 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

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown = fx_tchdwn_turboprop, 1
contrail=fx_A_I_Contrail
startup=il 18_engstart.fx, 1

[fuel]
LeftMain=0,-16,0,1605,0
LeftAux=0,-20,0,1662,0
RightMain=0,16,0,1605,0
RightAux=0,20,0,1662,0
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=2200
wing_span=125
wing_root_chord=20.0
wing_dihedral=3.0
wing_incidence=3.0
oswald_efficiency_factor=0.7
wing_twist=0.0
wing_winglets_flag=0
wing_sweep=20.0
wing_pos_apex_lon=8.0
wing_pos_apex_vert=0.0
htail_area=338.0
htail_span=52.0
htail_pos_lon=-50.0
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=0.0
vtail_area=224.0
vtail_span=20.0
vtail_sweep=20.0
vtail_pos_lon=-40.0
vtail_pos_vert=3.0
elevator_area=80.0
aileron_area=52.28
rudder_area=58.0
elevator_up_limit=27.0
elevator_down_limit=20.0
aileron_up_limit=19.0
aileron_down_limit=14.0
rudder_limit=23.0
elevator_trim_limit=19.0
spoiler_limit=90.0
spoilerons_available=0
aileron_to_spoileron_gain=0.0
min_ailerons_for_spoilerons=0.0
min_flaps_for_spoilerons=0.0
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed=117	
full_flaps_stall_speed=96	
cruise_speed=340                
max_indicated_speed=320
max_mach=0.6

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[brakes]
toe_brakes_scale=0.8
parking_brake=1
auto_brakes=4

[gear_warning_system]
gear_warning_available=1

[hydraulic_system]
electric_pumps=1
engine_map=1,1,1,1
normal_pressure=3000.000000

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[pitot_static]
pitot_heat=1.000000