// Copyright Vladimir Zhyhulskiy (UKRAINE)
// 05/2007 Ukraine (Kiev) 

[fltsim.0]
title=Antonov An-2T Amur Ski
sim=AN2Tski
texture=Amur
prop_anim_ratio=-1.52
atc_id=3336
atc_airline=Amur
atc_flight_number=3336
ui_manufacturer=Antonov
ui_type=An2
ui_variation=Amur Ski
visual_damage=1 
description=Antonov AN-2T Northern Ski version light universal transport (USSR-1947)

///========================================================
[fltsim.1]
title=Antonov An-2T Polar Airlines Ski
sim=AN2Tski
texture=PAL
prop_anim_ratio=-1.52
atc_id=3363
atc_airline=Amur
atc_flight_number=3363
ui_manufacturer=Antonov
ui_type=An2
ui_variation=Polar Airlines Ski
visual_damage=1 
description=Antonov AN-2T Northern Ski version light universal transport (USSR-1947)
///=======================================================================

[General]
atc_type=Antonov
atc_model=An2
editable=0
performance=Length: 40' 8''\nWing span: 59' 8''\nMax Speed 160 mph\nCruise Speed:105 to 120 mph\nRange: 525 miles\nCeiling: 145750'\nWeight Empty\/Gross:7500\/12125#\nPower: 1000 hp Shvetsov\n\nDesigner: Vlad Zhyhulskiy\nDate: 11\/11\/02\n

///========================================================
///========================================================
///========================================================
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 7100                         // (pounds)
empty_weight     = 4145                         // (pounds)

reference_datum_position     =   19.25, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -20.90, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations =50

station_load.0  = "170.0,   -5.4,  -2.0,   0.0, Pilot"              //Weight, Lat, Lon, Vert Position
station_load.1  = "170.0,   -5.4,   2.0,   0.0, Co-Pilot"           //Weight, Lat, Lon, Vert Position
station_load.2  = "680.0,  -14.2,   0.0,   0.0, Passenger Row 1"    //Weight, Lat, Lon, Vert Position
station_load.3  = "680.0,  -17.4,   0.0,   0.0, Passenger Row 2"    //Weight, Lat, Lon, Vert Position
station_load.4  = "680.0,  -20.7,   0.0,   0.0, Passenger Row 3"    //Weight, Lat, Lon, Vert Position
station_load.5  = "680.0,  -23.9,   0.0,   0.0, Passenger Row 4"    //Weight, Lat, Lon, Vert Position
station_load.6  = "510.0,  -27.2,   0.0,   0.0, Passenger Row 5"    //Weight, Lat, Lon, Vert Position
station_load.7  = "510.0,  -30.4,   0.0,   0.0, Passenger Row 6"    //Weight, Lat, Lon, Vert Position
station_load.8  = "340.0,  -33.7,   0.0,   0.0, Passenger Row 7"    //Weight, Lat, Lon, Vert Position
station_load.9  = "340.0,  -36.9,   0.0,   0.0, Passenger Row 8"    //Weight, Lat, Lon, Vert Position
station_load.10 = "500.0,  -23.8,   0.0,   0.0, Forward Baggage"    //Weight, Lat, Lon, Vert Position
station_load.11 = "100.0,  -45.5,   0.0,   0.0, Rear Cargo"         //Weight, Lat, Lon, Vert Position

;Moments of Inertia
empty_weight_pitch_MOI   =  69699.03  
empty_weight_roll_MOI    =  60179.10  
empty_weight_yaw_MOI     = 124797.97 
empty_weight_coupled_MOI = 0.0      

///========================================================
///========================================================
///========================================================   

[flight_tuning]
cruise_lift_scalar     =0.83
parasite_drag_scalar   =0.91
induced_drag_scalar    =1.0
elevator_effectiveness =1.0
aileron_effectiveness  =1.23
rudder_effectiveness   =0.95  
pitch_stability        =1.0
roll_stability         =1.0
yaw_stability          =1.71  
elevator_trim_effectiveness =0.85
aileron_trim_effectiveness  =0.90
rudder_trim_effectiveness   =1.0
p_factor_on_yaw          =0.74    
torque_on_roll           =1.0
gyro_precession_on_yaw   =1.0
gyro_precession_on_pitch =1.0

///========================================================
///========================================================
///========================================================
[GeneralEngineData]
engine_type =0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 =9.167, 0.0, -2.000
fuel_flow_scalar=1.0                           //Fuel flow scalar
min_throttle_limit =0.0                        //Minimum percent throttle.  Generally negative for turbine reverser
master_ignition_switch =1                      //Master Ignition Switch
///==============================================
[piston_engine]
cylinder_displacement=204.400
compression_ratio=6.400
number_of_cylinders=9
max_rated_rpm=2200.000
max_rated_hp=1000
fuel_metering_type=1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.035
turbocharged=1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=41.500
min_design_mp=1000
critical_altitude=0.000
emergency_boost_type=0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=1
max_rpm_mechanical_efficiency_scalar=1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0                   //Scalar on idle RPM friction
///==============================================
[propeller]
thrust_scalar =0.95                            //Propeller thrust scalar
propeller_type=0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=18.53                       //Propeller Diameter, (feet)
propeller_blades=4                             //Number of propeller blades
propeller_moi=40.2                             //Propeller moment of inertia
beta_max=30.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=18.0                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400                               //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.778                     //Propeller gear reduction ratio
fixed_pitch_beta=0.0                           //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.0                    //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=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700.0                      //Minimum RPM for prop feathering
beta_feather=89.5                              //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                          //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0.0                     //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.0                       //Minimum pitch angle in reverse, (degrees)
feathering_switches =1                         //Switches which invoke feathering
///==============================================
[fuel]
LeftMain =-22.55,  -6.7, -3.0, 302.0,  0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-22.55,   6.7, -3.0, 302.0,  0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
\\Center1  =  -22.55,   0.0, -2.7, 200.0,  0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type =1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors =2                    
electric_pump=1

///==============================================
///==============================================
///==============================================


        //0  Class
        //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


[contact_points]
point.0=1,  -41.00,  0.0,   -3.10, 1200.0, 0, 0.60, 180.0, 0.200, 2.5, 0.695,  0.0,  0.0, 0.0,   0.0,   0.0
point.1=1,  -15.75, -5.0, -8.10, 1600.0, 1, 1.35,   0.0, 0.504, 2.5, 0.686,  0,  0, 0, 0, 0
point.2=1,  -15.75,  5.0, -8.10, 1600.0, 2, 1.35,   0.0, 0.504, 2.5, 0.682,  0,  0, 0, 0, 0
point.3=2,  -27.00, -46.3,  -0.1,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 5.0, 0.0, 0.0
point.4=2,  -27.00,  46.3,  -0.1,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 6.0, 0.0, 0.0
point.5=2,  -61.00,   0.0,  14.0,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 9.0, 0.0, 0.0
point.6=2,    0.40,   0.0,  -1.2,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 4.0, 0.0, 0.0

static_pitch =11.95
static_cg_height =6.65
gear_system_type=1      //Hydraulic
tailwheel_lock =1 
///==============================================
///==============================================
///==============================================

[flaps.0]       //Trailing Edge Flaps
type             =1                                    // 1 - tail, 2 - lead
span-outboard    =0.5                                  // 0.0 .. 1.0
extending-time   =3                                    // seconds
flaps-position.0 =0                                    // degrees
flaps-position.1 =11                                   // degrees
flaps-position.2 =23                                   // degrees
flaps-position.3 =34                                   // degrees
damaging-speed   =170                                  // KIAS
blowout-speed    =195                                  // KIAS
lift_scalar =0.89                                       
drag_scalar =1.44
pitch_scalar=1.0
system_type =1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None


///==============================================
[brakes]
parking_brake =1       //Parking brake available
toe_brakes_scale =1  //Brake scalar
differential_braking_scale =1.0        //Delta on the amount of brake when the rudder pedals deflected

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

[Views]
eyepoint =-16.25, -1.41, 4.30

\\\=============================================================
///==============================================
///==============================================
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -19.0,-28.8, 5.3, fx_navredc
light.1 =3, -19.0, 28.8, 5.3,  fx_navgrec
light.2 =4, -26.20,   0.00,  1.95, fx_vclight ,
light.3 =4, -13.20,   0.00,  2.59,  fx_vclight ,
light.4 =4, -20.20,   0.00,  2.09, fx_vclight ,
light.5 =4, -15.20,   0.00,  2.90, fx_vclight ,
light.6 =5, -17.05,   -19.30,  -1.95, An2_land ,
light.7 =5, -17.05,   19.30,  -1.95, An2_land ,
 
///==============================================
///==============================================
///==============================================

[EFFECTS]
wake=fx_wake
water=fx_spray
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup=fx_An2start
windshield_rain_effect_available =1
dirt =fx_An2snow


[exits]
number_of_exits=2
exit_rate.0=0.2                               ;Percent per second
exit_rate.1=0.1                             ;Percent per second

///===========================================================================
[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13   

[TailHook]
tailhook_length=1                             ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.3

///==================================================================

[SMOKESYSTEM]
smoke.0=-0,-20.00,-4.00,fx_fallsw.fx
///==============================================
///==============================================
///==============================================

[autopilot]
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 =0.0
default_bank_mode=2     //Default to Heading Hold
///==============================================


[airplane_geometry]
wing_area               =987.0                 //Square feet
wing_span               =95.0                  //Feet
wing_root_chord         =12.85                  //Feet
wing_dihedral           =5.0                   //Degrees
wing_incidence          =2.0                   //Degrees
wing_twist              =-1.0                  //Degrees
oswald_efficiency_factor=0.65                  //Measure of lift effeciency of wing
wing_winglets_flag      =0                     //Are winglets available?
wing_sweep              =14.5                   //Degrees, wing leading edge
wing_pos_apex_lon       =-13.00                //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      =-2.7                   //Feet, vertical distance from reference point, positive going up

htail_area              =95.8                  //Square feet
htail_span              =28.25                 //Feet
htail_pos_lon           =-52.7                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          =-52.7                 //Feet, vertical distance from reference point, positive going up
htail_incidence         =-1.0                   //Degrees
htail_sweep             =27.0                  //Degrees, horizontal tail leading edge

vtail_area              =37.9                  //Square feet
vtail_span              =11.49                 //Feet, tip to body
vtail_sweep             =50.4                  //Degrees, vertical tail leading edge
vtail_pos_lon           =-51.4                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          =6.7                   //Feet, vertical distance from reference point, positive going up

elevator_area           =83.4                  //Square feet
aileron_area            =102.8                 //Square feet
rudder_area             =46.7                  //Square feet
elevator_up_limit       =30.0                  //Degrees
elevator_down_limit     =20.0                  //Degrees
aileron_up_limit        =27.0                  //Degrees
aileron_down_limit      =18.0                  //Degrees
rudder_limit            =30.0                  //Degrees
elevator_trim_limit     =12.0                  //Degrees
spoiler_limit=60.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000            //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
               

[Reference Speeds]
flaps_up_stall_speed    =55.000
full_flaps_stall_speed  =44.000
cruise_speed            =152
max_indicated_speed     =245.703125

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[stall_warning]
type=1
stick_shaker=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
Adf.2         =1
Transponder.1 =0
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 =200, 1000
aileron  =200, 1000
rudder   =200, 1000

[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=1,0
direction_indicator.1=2,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 =1 
attitude_indicator.1 =2 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0

[hydraulic_system]
normal_pressure =732.0    //PSI
electric_pumps  =0         //no electric pumps
engine_map      =1,1,0,0   //pumps on Eng1,2
[gear_warning_system]
gear_warning_available =1    //Normal
pct_throttle_limit =0.1     //Percent throttle that activates warning
flap_limit_idle    =0.0     //Flap angle that activates warning at idle
flap_limit_power   =16.0     //Flap angle that activates warning at above idle
[electrical]
max_battery_voltage =24
generator_alternator_voltage =25
max_generator_alternator_amps =100

///============================================== END!!!




[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=5.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0