[fltsim.0]
title=Antonov An38 NAPO
sim=An38
model=
panel=
sound=
texture=
ui_manufacturer=Antonov
ui_type=An38
ui_variation=NAPO
atc_heavy=0
description=Powerplant:  two  900-hp (671-kW) Garret TPE331-10R-513C turboprops\nAccomodation: two (flight deck), maximum of 26 passengers\nDimensions: span 66ft 6 1\/2 in (20.28m)\s height 21ft 7 3\/4 in (6.60m)\s length 52ft 11 3\/4 in (16.15m)  \nWeights: empty 8,333lb (3780 kg)\s maximum take-off 16,975 lb (7700 kg)\n\n; model & textures: makc-sim; FDE: Scorpio9999.

[fltsim.1]
title=Antonov An38 Vostok
sim=An38
model=
panel=
sound=
texture=Vostok
ui_manufacturer=Antonov
ui_type=An38
ui_variation=Vostok
atc_heavy=0
description=Powerplant:  two  900-hp (671-kW) Garret TPE331-10R-513C turboprops\nAccomodation: two (flight deck), maximum of 26 passengers\nDimensions: span 66ft 6 1\/2 in (20.28m)\s height 21ft 7 3\/4 in (6.60m)\s length 52ft 11 3\/4 in (16.15m)  \nWeights: empty 8,333lb (3780 kg)\s maximum take-off 16,975 lb (7700 kg)\n\n; model & textures: makc-sim; FDE: Scorpio9999.



[General]
atc_type=Antonov
atc_model=AN-38
editable=1
performance=Service ceiling  17000 ft (5200 m)  
Maximum cruising speed at H=3000m (350-380 km/h)  
Economy speed at H=9800ft (3000m)   (350 km/h)  
Maximum range (H=9800ft (3000m), 0.5 hour fuel reserve)  650 kts (1300 km)  
Flight endurance (H=9800ft (3000 m), 0.5 hour fuel reserve)  6 h  
Fuel consumption  
Take-off run  
Landing roll (SL, ISA) (water/ground)  98
Seaworthiness, sea state  

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[gear_warning_system]
gear_warning_available = 0
pct_throttle_limit = 0.1
flap_limit_idle = 33.75
flap_limit_power = 16.875


[contact_points]
static_pitch = -0.3
static_cg_height = 7
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, 18.4831, 0, -7.251, 1181, 0, 0.9, 55, 0.3, 1.5, 1.5, 0, 0, 0, 184, 184
point.1 = 1, -2.2863, -5.5, -7.2991, 1574, 1, 1.2, 0, 0.5, 0.4, 0.8152, 0, 0, 2, 184, 184
point.2 = 1, -2.2877, 5.5, -7.2976, 1574, 2, 1.2, 0, 0.5, 0.4, 0.8152, 0, 0, 3, 184, 184
point.3 = 2, -1.55, -36, 3, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.55, 36, 3, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -29.6455, 0, -0.6746, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 20.6654, 0, -3.8928, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

static_pitch=0
static_cg_height=5
gear_system_type=0

[Views]
eyepoint=8.0,-0.8,0.2

[General]
performance=

[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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1 	
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
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

[direction_indicators]
direction_indicator.0=3,0

[SMOKESYSTEM]
smoke.0=0.0, -6.0,  -5.0,  fx_Swordwaterfall
smoke.1=0.0, -6.0,   5.0,  fx_Swordwaterfall


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

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.50000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=10000
empty_weight_roll_MOI=101258.000000
empty_weight_pitch_MOI=102469.000000
empty_weight_yaw_MOI=167467.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=15000

[fuel]
LeftMain=0.000000,0.000000,0.000000,68.000000,0.000000
RightMain=0.000000,0.000000,0.000000,68.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[flight_tuning]
cruise_lift_scalar     = 1.1
parasite_drag_scalar   = 1.35
induced_drag_scalar    = 1.35
elevator_effectiveness = .8
aileron_effectiveness  = 1.4
rudder_effectiveness   = 1.1
pitch_stability        = 2.1
roll_stability         = 1.1
yaw_stability          = 1.1
elevator_trim_effectiveness = 5.1
aileron_trim_effectiveness  = 1.1
rudder_trim_effectiveness   = 1.1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1


[airplane_geometry]
wing_area=639.000000
wing_span=55.166668
wing_root_chord=11.950000
wing_dihedral=10.999315
wing_incidence=0.000000
wing_twist=-0.999799
oswald_efficiency_factor=.82
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=57.000000
htail_span=13.777777
htail_pos_lon=-30.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=100.000000
vtail_span=12.401755
vtail_sweep=0.000000
vtail_pos_lon=-26.888887
vtail_pos_vert=1.600000
elevator_area=21.00000
aileron_area=64.700000
rudder_area=36.000000
elevator_up_limit=15.0
elevator_down_limit=15.0
aileron_up_limit=15.0
aileron_down_limit=15.0
rudder_limit=25.0
elevator_trim_limit=18.480565
spoiler_limit=58.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000



[GeneralEngineData]
engine_type=0
Engine.0=4.000000,-7.000000,0.000000
Engine.1=4.000000,7.000000,0.000000
fuel_flow_scalar=.520000
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.1
max_rpm_mechanical_efficiency_scalar=1.05000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=.950000
idle_rpm_friction_scalar=1.000000
cylinder_displacement=115.700000
compression_ratio=8.000000
number_of_cylinders=12
max_rated_rpm=3000.000000
max_rated_hp=420.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0


[Reference Speeds]
flaps_up_stall_speed=64.000000
full_flaps_stall_speed=58.000000
cruise_speed=170
max_indicated_speed=199

[keyboard_response]
elevator=150.000000,200.000000

[propeller]
propeller_type=0 
propeller_diameter=11.99 
propeller_blades=5 
propeller_moi=19.000 
beta_max=62.000 
beta_min=6.000 
min_gov_rpm=21520.000 
prop_tc=0.004 
gear_reduction_ratio=14.600 
fixed_pitch_beta=20.000 
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=700.000 
beta_feather=84.300 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=1.000 
minimum_reverse_beta=-14.000 
thrust_scalar=1.000 

[brakes]
toe_brakes_scale=.8
parking_brake=1



[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.3                               ;Percent per second
exit_rate.1 = 0.3                               ;Percent per second

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 25                                   // degrees
flaps-position.3 = 40                                   // degrees
damaging-speed   =170                                  // KIAS
blowout-speed    =190                                  // KIAS



[lights]

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

light.0 = 3, 4.98, -36.05, 3.21, fx_navred
light.1 = 3, 4.98, 36.05, 3.21, fx_navgre
light.2= 3, -24.85,   0.00,   1.70, fx_navwhi ,
light.3 = 5 , 25.30 , 0.00 , -3.60, fx_landing,
light.4 = 1, -22.20, 8.55, 8.00, fx_beacon
light.5 = 1, -22.20, -8.55, 8.00, fx_beaconb
light.6 = 3, -1.98, -8.78, -0.80, fx_nicksmokeAI_sm_lear
light.7 = 3, -1.98, 8.78, -0.8, fx_nicksmokeAI_sm_lear
light.8 = 4,  10.11,  0.00,  -1.64, fx_vclight,
light.9 = 2,  -6.70,   0.00, -4.70, fx_strobe ,
light.11 = 2, 3.10, 36.05, 3.21, fx_strobe
light.12 = 2, 3.10, -36.05, 3.21, fx_strobe


[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
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 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)