//=============================================
//====== An-12BK - AAV Dynamics ===============
//=============================================
[fltsim.0]
title=Antonov An-12BK RuAF (VVS-15)
sim=An12BKzh-AAV-V10
model=
panel=
sound=
texture=VVS
checklists=
atc_id=VS15
prop_anim_ratio=1.15
atc_airline=VVS
atc_flight_number=VS15
ui_manufacturer=Antonov
ui_type=An-12BK
visual_damage=1
atc_heavy=0
ui_variation=VVS-15
description=wAntonov An-12BK Ru AF (VVS, AFB Chkalovsky) long ranger military transport (autor Vladimir Zhyhulskiy - 12/2008)

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

[fltsim.1]
title=Antonov An-12BK Ru Navi (VMS)
sim=An12BKzh-AAV-V10
model=
panel=
sound=
texture=VMS
checklists=
atc_id=VM16
prop_anim_ratio=1.15
atc_airline=VVS
atc_flight_number=VM16
ui_manufacturer=Antonov
ui_type=An-12BK
visual_damage=1
atc_heavy=0
ui_variation=VMS
description=Antonov An-12BK Ru Navi (VMS - Nord fleet, AFB Pushkin) long ranger military transport (autor Vladimir Zhyhulskiy - 12/2008)


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

[fltsim.2]
title=Antonov An-12BK RuAF (VVS-09)
sim=An12BKzh-AAV-V10
model=
panel=
sound=
texture=V09
checklists=
atc_id=VS15
prop_anim_ratio=1.15
atc_airline=VVS
atc_flight_number=VS09
ui_manufacturer=Antonov
ui_type=An-12BK
visual_damage=1
atc_heavy=0
ui_variation=VVS-09
description=Antonov An-12BK Ru AF (VVS) (Khabarovsk AB) long ranger military transport (autor Vladimir Zhyhulskiy - 12/2008, texture -D.Smirnov)

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

[fltsim.3]
title=Antonov An-12BK Slovakia AF
sim=An12BKzh-AAV-V10
model=
panel=
sound=
texture=SLK
checklists=
atc_id=VS15
prop_anim_ratio=1.15
atc_airline=SLK AF
atc_flight_number=2209
ui_manufacturer=Antonov
ui_type=An-12BK
visual_damage=1
atc_heavy=0
ui_variation=Slovakia
description=Antonov An-12BK Slovakia AF long ranger military transport (autor Vladimir Zhyhulskiy - 12/2008)

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

[fltsim.4]
title=Antonov An-12BK RuAF (VVS-28)
sim=An12BKzh-AAV-V10
model=
panel=
sound=
texture=V28
checklists=
atc_id=VS15
prop_anim_ratio=1.15
atc_airline=VVS
atc_flight_number=VS28
ui_manufacturer=Antonov
ui_type=An-12BK
visual_damage=1
atc_heavy=0
ui_variation=VVS-28
description=Antonov An-12BK Ru AF (VVS) (Khabarovsk AB) long ranger military transport (autor Vladimir Zhyhulskiy - 12/2008, texture -D.Smirnov)

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

[fltsim.5]
title=Antonov An-12BK Kazakhstan AF
sim=An12BKzh-AAV-V10
model=
panel=
sound=
texture=KAZ
checklists=
atc_id=VS15
prop_anim_ratio=1.15
atc_airline=Kaz AF
atc_flight_number=2209
ui_manufacturer=Antonov
ui_type=An-12BK
visual_damage=1
atc_heavy=0
ui_variation=Kazakhstan
description=Antonov An-12BK Kazakhstan AF long ranger military transport (autor Vladimir Zhyhulskiy - 12/2008)
//

[General]
performance=Antonov An-12BK long ranger military transport \n\n  - FD by AAV -V10
atc_type=Antonov
atc_model=An12

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

[weight_and_balance]
max_gross_weight=134400   
empty_weight=77000.//[35t]//61700 //aav [28t] 
reference_datum_position=0, 0, 0
empty_weight_CG_position=0, 0, 0
empty_weight_pitch_MOI=5000000.//aav//2500000.
empty_weight_roll_MOI=2700000.
empty_weight_yaw_MOI=2500000. 
empty_weight_coupled_MOI=0
max_number_of_stations=6
station_load.0="200,  34, -1, -4, Captain"
station_load.1="200,  34,  1, -4, First Officer"
station_load.2="200,  31,  2, -9, Radist"
station_load.3="200,  29,  0, -7, Navigator"
station_load.4="200,  25, -2, -9, Flight Engeneer"
station_load.5="0, 0,  0, 0, CARGO"

//=============================================
//=================TUNING===================
//=============================================

[FLIGHT_TUNING]
cruise_lift_scalar  =1.0 
parasite_drag_scalar=1.0
induced_drag_scalar =1.5
elevator_effectiveness= 1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.5 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00


//=================== ENGINES //===================

[GeneralEngineData]
engine_type=5
fuel_flow_scalar=0.685   
engine.0=10, -42.0, -0.5
engine.1=10, -26.0, -0.5
engine.2=10, 26.0, -0.5
engine.3=10, 42.0, -0.5
//
//engine.0=10, -32.0, -0.5
//engine.1=10, -16.0, -0.5
//engine.2=10, 16.0, -0.5
//engine.3=10, 32.0, -0.5
//
//engine.0=10, -32.0, -2.5
//engine.1=10, -16.0, -2.5
//engine.2=10, 16.0, -2.5
//engine.3=10, 32.0, -2.5
//
//engine.0=10, -42.0, -2.5
//engine.1=10, -26.0, -2.5
//engine.2=10, 26.0, -2.5
//engine.3=10, 42.0, -2.5
//
min_throttle_limit=-0.001

[TurbineEngineData]
fuel_flow_gain=0.005 
inlet_area=1.5 
rated_N2_rpm=27920 
static_thrust=500 
afterburner_available=0
reverser_available=0.0

[turboprop_engine]
power_scalar  = 1.0 
maximum_torque= 14000.    

[propeller]
thrust_scalar=1.0                  //Propeller thrust scalar
propeller_type=0                  //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=12             //Propeller Diameter, (feet)
propeller_blades=4                //Number of propeller blades
propeller_moi=70.                 //Propeller moment of inertia
beta_max=50.//60.                      //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=10.0                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25500                 //Miminum governed RPM
prop_tc=0.01                      //Prop time-constant
gear_reduction_ratio=15.4         //Propeller gear reduction ratio
fixed_pitch_beta=0                //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=0.5        //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=500.           //Minimum RPM for prop feathering
beta_feather=93.                   //Feathering pitch angle (degrees)
power_absorbed_cf=0.95             //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0  //Defeathering accumulators available? 0=FALSE,1=TRUE
prop_reverse_available=1.0             //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0.0            //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=1                 //Minimum pitch angle in reverse, (degrees)
rotation=-1 -1 -1 -1

//===================FUEL=====================================

[FUEL]
// 6.7 lbs/gal; -> 3.04liters/Gal -> (1Gal=3.786liters) -> Ro~0.8
//
// [15.6t] 
//
//LeftMain = 0.00, -8.5,   -1.00,   2565.0, 50.0
//RightMain= 0.00,  8.5,   -1.00,   2565.0, 50.0
// 
// [22t]
//

//Center1    = 0.00,  0.0,    0.00,   7249.0, 0.0
LeftMain   = 0.00, -8.5,   -1.00,   3624.0, 0.0
RightMain  = 0.00,  8.5,   -1.00,   3624.0, 0.0

//
fuel_type=2
number_of_tank_selectors=2
electric_pump=1


//=====================================================   
///================FLAPS==============================   
///=====================================================   

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.
system_type= 0
damaging-speed= 270.000
blowout-speed= 320.000
lift_scalar= 0.0
drag_scalar= 0.0 
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 35.000, 0.000
flaps-position.4= 45.000, 0.000
//
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 20.
system_type= 0
damaging-speed= 270.000
blowout-speed= 320.000
lift_scalar= 1.0 
drag_scalar= 0.0 
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 35.000, 0.000
flaps-position.4= 45.000, 0.000
//
[Flaps.2]
type= 1
span-outboard= 0.800
extending-time= 20.
system_type= 0
damaging-speed= 270.000
blowout-speed= 320.000
lift_scalar= 0.0 
drag_scalar= 1.0  
pitch_scalar= 0.000
flaps-position.0=  0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 45.000, 0.000


//==============================================================
//===================CONTACT==============================
//==============================================================
[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)


//         0      1        2        3     4          5      6      7     8       9     10      11      12    13    14    15
// realistic landing
point.0 = 1.000, 28.000, 0.000, -9.90, 3000.000, 0.000, 1.500, 35.00, 0.300, 2.500, 0.30, 11.000, 11.000, 0.000, 335.000, 340.000
point.1 = 1.000, -3.500, -7.000, -9.4, 5000.000, 1.000, 2.200, 0.000, 0.300, 2.500, 0.40, 14.000, 14.000, 2.000, 335.000, 340.000
point.2 = 1.000, -3.500,  7.000, -9.4, 5000.000, 2.000, 2.200, 0.000, 0.300, 2.500, 0.40, 14.000, 14.000, 3.000, 335.000, 340.000
// easy landing
//point.0 = 1.000, 34.000, 0.000, -9.90, 3000.000, 0.000, 1.500, 35.00, 0.300, 2.500, 0.80, 11.000, 11.000, 0.000, 335.000, 340.000
//point.1 = 1.000, -3.500, -7.000, -9.4, 5000.000, 1.000, 2.200, 0.000, 0.300, 2.500, 0.80, 14.000, 14.000, 2.000, 335.000, 340.000
//point.2 = 1.000, -3.500,  7.000, -9.4, 5000.000, 2.000, 2.200, 0.000, 0.300, 2.500, 0.80, 14.000, 14.000, 3.000, 335.000, 340.000
//
point.3 = 2.000, -6.0,-61.0, 7.50, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2.000, -6.0, 61.0, 7.50, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5 = 2.000, -52.50, 0.000, 5.0, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6 = 2.000, 41.270, 0.000, -1.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000, 0.000
point.7= 5, -20.9, -5.25, -7.30,1600, 0, 0.00, 50.0, 0.0,  0.0,   1.00, 8.0, 8.2, 0, 0.0, 0.0

static_pitch = 0.95 
static_cg_height = 9.1//9.45
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

//==============================================================
//===================LIGHTS=====================================
//==============================================================

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 
//7=RECOGNITION, 9=LOGO, 10=CABIN

light.0=1, -20.00, 0.00, -5.80, fx_beacon ,
light.1 = 2, -6.1, -59.90, 6.3, ZH_strobeR ,
light.2 = 2,-6.1, 59.90, 6.3, ZH_strobeG ,
light.3 = 3, -52.60, 0.00, 27.40, fx_navred ,
Light.4 = 3, -62.70, 0.00, 6.30, fx_navwhi ,
light.5=2, -6.1, 59.90, 6.3, fx_navgre,
light.6=4, 2.39, 0.00, 4.50, ZH_vcAn12 ,
Light.7 = 10, -12.30, -0.20, 5.1, ZH_cabin ,
////SMOKE
light.8= 7, -6.9, -32.8, 2, zh_An12smok, 
light.9= 7, -6.9, -16.8, 2, zh_An12smok, 
light.10= 7, -6.9, 16.8, 2, zh_An12smok, 
light.11=7, -6.9, 32.8, 2, zh_An12smok, 

////IK piropatron
////light.12=8, -64.00, 0.00, 3.80, ZH_ikpp,
////STURMAN
///Light.15 = 3, 38.30,   -0.00,  1.50, fx_navgrem ,


//=============================================
[brakes]
toe_brakes_scale=0.3
parking_brake=1
///==============================================


///==============================================
///================AUTO==========================
///==============================================
auto_brakes=4
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=100.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=110
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
autoland_available=0
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=5.
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.5
max_pitch_velocity_lo_alt_breakpoint=16000.
max_pitch_velocity_hi_alt_breakpoint=20000.0
max_bank=15.000000
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=1.000000

//==============================================================
//===================VVVVVVVV===================================
//==============================================================

[Views]

eyepoint=3.7 , -2.90, 5.20

//==============================================================
//====================EFFECT&ANIMATIONS=========================
//==============================================================

[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4

[TailHook]
tailhook_length=1.1            ;(feet)
tailhook_position=-21.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9

[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13                         ;Percent per second

//===================================================
[EFFECTS]
wake   = 	fx_wake
water  = 	fx_spray
dirt   =   ZH_An12dust       
///dirt =  ZH_An12snow   
concrete = 	fx_sparks
touchdown=	fx_tchdwn, 1
startup=	zh_An12start
windshield_rain_effect_available = 1
///===================================================
[SMOKESYSTEM]

smoke.4=-68.00, -0.00, 3.80, ZH_ikpp.fx /// 1 click-20 second!





//==============================================================
//===================GEOMETRY===================================
//==============================================================

[airplane_geometry]
wing_area      = 1340 
wing_span      = 122. 
wing_root_chord= 11.  
wing_dihedral  = 0.0
wing_incidence = 0 
wing_twist=0
wing_winglets_flag = 0
wing_sweep         = 0.0
wing_pos_apex_lon  = 2.9
wing_pos_apex_vert = 2 
oswald_efficiency_factor=0.8 
//
htail_area=250.
htail_span=40.3 
htail_pos_lon=-50.2 
htail_pos_vert=6 
htail_incidence=0.5
htail_sweep= 15.0
//
vtail_area=300.
vtail_span=20.0 
vtail_sweep=25.0 
vtail_pos_lon=-40.0 
vtail_pos_vert=8.0 
//
elevator_area=70.0 
aileron_area =50.0 
rudder_area  =65. 
elevator_up_limit=28
elevator_down_limit=15
aileron_up_limit=25
aileron_down_limit=15
rudder_limit= 25.0 
elevator_trim_limit=12
spoiler_limit=0.
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0
spoilerons_available=0

//==============================================================
//===================MISK=======================================
//==============================================================
auto_spoiler_available=1
positive_g_limit_flaps_up=2.099359
positive_g_limit_flaps_down=1.500000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.199786

[forcefeedback]
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=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=1300
ground_bumps_angle1=08900
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200
ground_bumps_angle2=09100
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

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

[Reference Speeds]
flaps_up_stall_speed=130
full_flaps_stall_speed=95.0
cruise_speed=300.0
max_indicated_speed=370.0
max_mach=0.75 

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

[ELECTRICAL]
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 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

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

[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, 1
//Nav.1=1, 1, 1 // ????????????
//Nav.2=1, 1, 0
Adf.1=1, 0
Adf.2=1, 0
Transponder.1=1
Marker.1=1


[direction_indicators]
direction_indicator.0=3,0 

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_idle=5.042029
flap_limit_power=25.496622

[hydraulic_system]
normal_pressure=3000.000000
electric_pumps=0
engine_map=1,1,1,1

[stall_warning]
type=1
stick_shaker=1

[pitot_static]
vertical_speed_time_constant=1

pitot_heat=1.000000
[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=2