[fltsim.0]
title=Antonov An-12B
sim=An12Bzh
model=
panel=
sound=
texture=
checklists=
atc_id=
atc_airline=Аэрофлот
atc_flight_number=RA-11653
ui_manufacturer=Antonov
ui_type=An-12B
visual_damage=1
atc_heavy=0
ui_variation=Аэрофлот
description=


[General]
performance=Antonov An-12B long ranger military transport
atc_type=Antonov
atc_model=A-12B



[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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





[WEIGHT_AND_BALANCE]

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000


station_load.0=0.000, 43.000, 0.000, 0.000 //(crew)
station_load.1=0.000, 32.000, 0.000, 0.000 //frontmost cabin
station_load.2=0.000, 25.000, 0.000, 0.000 //front cargo bay
station_load.3=0.000, 15.000, 0.000, 0.000 //center cabin
station_load.4=0.000, -15.000, 0.000, 0.000 //rearmost cargo bay
station_load.5=0.000, -23.000, 0.000, 0.000 //rearmost cabin


//total load=58124lbs, empty wt. 76235lbs (58124+76076= 134200lbs/61T)
empty_weight=76235.068
empty_weight_roll_MOI=1801400.000000
empty_weight_pitch_MOI=3580000.000000
empty_weight_yaw_MOI=2000000.000000
empty_weight_coupled_MOI=1200.000000
max_gross_weight=134480.600

[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, 0, 17.0
avionics=1, 0 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 0, 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, 0 , 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, 0 , 17.0


[GeneralEngineData]
engine_type=1
fuel_flow_scalar=0.45
Engine.0=10.000000,-22.833333,-3.933333
Engine.1=10.000000,-18.833333,-3.933333
Engine.2=10.000000,18.833333,-3.933333
Engine.3=10.000000,22.833333,-3.933333
min_throttle_limit=-0.309937


[Reference Speeds]
flaps_up_stall_speed=310.387
full_flaps_stall_speed=230.793
cruise_speed=307.775
max_indicated_speed=334.000000
max_mach=0.820020

[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=0	//For no wing leveler when AP On
use_no_default_pitch=0	//For no pitch holding when AP On
autoland_available=0

[direction_indicators]
direction_indicator.0=3,0

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



[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

[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 Damping Ratio / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//8 Extension Time              (seconds)
//9 Retraction Time             (seconds)
//10 Sound Type
//11 Airspeed limit for retraction (KIAS)
//12 Airspeed that gear gets damage at (KIAS)

static_pitch=0.470
static_cg_height=11.630
point.0=1.000000,37.166667,0.000000,-12.600000,1574.803150,0.000000,1.680382,75.000000,0.408324,2.500000,0.366167,9.000000,9.400000,0.000000,0.000000,0.000000
point.1=1.000000,-16.333333,-12.416667,-12.066667,1574.803150,1.000000,1.680382,0.000000,1.000746,2.500000,0.665683,13.000000,11.700000,2.000000,0.000000,0.000000
point.2=1.000000,-16.333333,12.416667,-12.066667,1574.803150,2.000000,1.680382,0.000000,1.000746,2.500000,0.665683,13.100000,11.900000,3.000000,0.000000,0.000000
point.3=2.000000,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-13.750000,54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-71.250000,0.000000,0.750000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,51.666667,0.000000,-8.166667,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=5, -50.90, -19.250, -19.300, 1600, 0, 0.00, 70.0, 0.0,  0.0, 5.00, 3.0, 3.2, 0, 0.0, 0.0
point.8=5, -50.90,  19.250, -19.300, 1600, 0, 0.00, 70.0, 0.0,
gear_system_type=0

[fuel]
LeftMain=-15.000, -15.000, 0.000, 2029.5, 5.000
RightMain=-15.000, 15.000, 0.000, 2029.5, 5.000
LeftAux=-15.5,  -30.0, -3.0,   300.0, 0.0
RightAux=-15.5,  30.0, -3.0,  300.0, 0.0
fuel_type=2.000000
number_of_tank_selectors=1
fuel_type=2.000000
electric_pump=0

[keyboard_response]
aileron=180.000000,130.000000

[pitot_static]
vertical_speed_time_constant=1               

[Views]
eyepoint=43.22074,-1.723061,4.355627


[flaps.1]     
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=21                                  // seconds
flaps-position.0=0   
flaps-position.1=5,
flaps-position.2=10, 
flaps-position.3=15, 
flaps-position.4=25,  
flaps-position.5=35,                                    
blowout-speed=200                              // KIAS
lift_scalar=0.85
drag_scalar=0.0
system_type=2 


[jet_engine]
thrust_scalar=1.0

[GROUND_REACTION]
MAX_STEERING_ANGLE=35

[TurbineEngineData]
fuel_flow_gain=0.002300
inlet_area=29.000000
rated_N2_rpm=29920.000000
static_thrust=13000.480000
afterburner_available=0
reverser_available=1

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

[airplane_geometry]
wing_area=1310.000000
wing_span=124.666667
wing_root_chord=10.583333
wing_dihedral=0.000000
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=3.733187
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=487.000000
htail_span=55.000000
htail_pos_lon=-43.750000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=281.000000
vtail_span=19.112823
vtail_sweep=0.000000
vtail_pos_lon=-42.500000
vtail_pos_vert=5.833333
elevator_area=121.750000
aileron_area=52.680000
rudder_area=47.770000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
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 

[flight_tuning]
parasite_drag_scalar=1.7
induced_drag_scalar=1.7
elevator_effectiveness=0.95
pitch_stability=0.6
roll_stability=0.6
yaw_stability=0.8
elevator_trim_effectiveness=1.6
aileron_trim_effectiveness=0.9
rudder_trim_effectiveness=1.1

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

light.0=1,   -25.50,   0.00,  -7.90, fx_beacon320pa ,
light.1=4,  30.41,   0.00,  3.50, fx_vclight ,
light.2=4,  35.59,   0.00,  0.00, fx_vclight ,
light.3 = 2, -14.8, -74.15,  7.4, fx_strobeh ,
light.4 = 2, -14.8,  74.15,  7.4, fx_strobeh ,
light.5 = 3, -80.00,   0.00,  31.90, fx_navredm ,



[ground_reaction]
main_gear_static_compression=1.5	// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.9            // (feet), The distance the center gear strut is compressed when at rest on the ground

[SMOKESYSTEM]
smoke.0=89,-30.3,-38.8, fx_oldsmoke
smoke.1=89,-30.3,-19.8, fx_oldsmoke
smoke.2=89,-30.3,19.8, fx_oldsmoke
smoke.3=89,-30.3,38.8, fx_oldsmoke



[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(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


[brakes]
toe_brakes_scale=0.803555
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0