[fltsim.0]
title=Antonov An-38 NAPO
sim=An-38
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_color=0x00000000
atc_id=
ui_manufacturer=AI
ui_type=Antonov An-38
ui_variation=NAPO
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; AI FDE: Scorpio9999.
visual_damage=0
atc_parking_types=RAMP
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0

[fltsim.1]
title=Antonov An-38 Vostok
sim=An-38
model=
panel=
sound=
texture=Vostok
kb_checklists=
kb_reference=
atc_id_color=0x00000000
atc_id=
ui_manufacturer=AI
ui_type=Antonov An-38
ui_variation=Vostok
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; AI FDE: Scorpio9999.
visual_damage=0
atc_parking_types=RAMP
atc_id_font=Verdana,-11,1,600,0
atc_parking_codes=AN38

[fltsim.2]
title=Antonov An-38 Alrosa
sim=An-38
model=
panel=
sound=
texture=Alrosa
kb_checklists=
kb_reference=
atc_id_color=0000000000
atc_id=
ui_manufacturer=AI
ui_type=Antonov An-38
ui_variation=Alrosa
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; AI FDE: Scorpio9999.
visual_damage=0
atc_parking_types=RAMP
atc_id_font=Verdana,-11,1,600,0
atc_parking_codes=AN38

[General]
atc_type=ANTONOV 
atc_model=An-38 
editable=0 
performance=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 

[weight_and_balance]

// ACM V2.5
max_gross_weight = 19383
empty_weight = 11013
reference_datum_position = 5, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 35802
empty_weight_roll_MOI = 30972
empty_weight_yaw_MOI = 54832
empty_weight_coupled_MOI = 0
max_number_of_stations = 1

station_load.0 = 2000, 0, 0, 0


[lights]

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

light.0 = 3, 0.38, -35.56, 3.21, fx_navred
light.1 = 3, 0.38, 35.56, 3.21, fx_navgre
light.2 = 1, -24.13, 8.55, -1.81, fx_beacon
light.3 = 1, -26.81, -8.55, 7.27, fx_beaconb
light.4 = 2, -24.13, 8.55, -1.81, fx_strobe
light.5 = 2, -26.81, -8.55, 7.27, fx_strobe
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

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.0
min_throttle_limit = -0.250000
engine.0 = 6, -8.84, 0.98,
engine.1 = 6, 8.84, 0.98,

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0

LeftMain = 0, -12, 2, 159.4, 0
LeftAux = 0, -5, 2, 159.4, 0
RightMain = 0, 12, 2, 159.4, 0
RightAux = 0, 5, 2, 159.4, 0


[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


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


[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 = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
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
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.6459,0.9685,0.9685,0.0164,1.5805,1.9371,1.9371
//ACM_AREAW2// 0.0337,1.5151,2.9056,2.9056,0.0507,1.4493,3.8743,3.8743,0.0675,1.3839
//ACM_AREAW3// 4.8428,4.8428,0.0842,1.3186,5.8115,5.8115,0.1014,1.2532,6.7800,6.7800
//ACM_AREAW4// 0.1181,1.1878,7.7486,7.7486,0.1351,1.1224,8.7172,8.7172,0.1518,1.0571
//ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1058,1.7661,0.5824,0.5824
//ACM_AREAH2// 0.2117,1.7847,0.8737,0.8737,0.3179,1.8034,1.1648,1.1648,0.4239,1.8220
//ACM_AREAH3// 1.4562,1.4562,0.5299,1.8406,1.7474,1.7474,0.6359,1.8593,2.0387,2.0387
//ACM_AREAH4// 0.7419,1.8779,2.3299,2.3299,0.8478,1.8961,2.6212,2.6212,0.9538,1.9148
//ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.2099,2.2853,0.5012,0.5012
//ACM_AREAV2// 0.4205,2.3152,0.7518,0.7518,0.6308,2.3450,1.0024,1.0024,0.8410,2.3749
//ACM_AREAV3// 1.2530,1.2530,1.0513,2.4047,1.5036,1.5036,1.2617,2.4346,1.7539,1.7539
//ACM_AREAV4// 1.4720,2.4644,2.0048,2.0048,1.6821,2.4941,2.2555,2.2555,1.8926,2.5241
//ACM_CAREAW1// 4.3586,4.3586,0.8988,1.2280,4.8428,4.8428,0.9074,1.2201,5.3270,5.3270
//ACM_CAREAW2// 0.9157,1.2122,5.8115,5.8115,0.9243,1.2042,6.2958,6.2958,0.9326,1.1962
//ACM_CAREAW3// 6.7800,6.7800,0.9412,1.1878,7.2644,7.2644,0.9495,1.1799,7.7486,7.7486
//ACM_CAREAW4// 0.9581,1.1720,8.2327,8.2327,0.9666,1.1641,8.7172,8.7172,0.9750,1.1561
//ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,0.9797,1.8098,0.5824,0.5824
//ACM_CAREAH2// 1.0857,1.8717,0.8737,0.8737,1.1914,1.9342,1.1648,1.1648,1.2977,1.9967
//ACM_CAREAH3// 1.4562,1.4562,1.4033,2.0590,1.7474,1.7474,1.5096,2.1214,2.0387,2.0387
//ACM_CAREAH4// 1.6158,2.1837,2.3299,2.3299,1.7216,2.2460,2.6212,2.6212,1.8278,2.3083
//ACM_CAREAV1// 0,0,0.5637,1.6914,0.2506,0.2506,0.7741,1.8114,0.5012,0.5012
//ACM_CAREAV2// 0.9843,1.9313,0.7518,0.7518,1.1947,2.0518,1.0024,1.0024,1.4048,2.1719
//ACM_CAREAV3// 1.2530,1.2530,1.6153,2.2918,1.5036,1.5036,1.8256,2.4119,1.7539,1.7539
//ACM_CAREAV4// 2.0359,2.5320,2.0048,2.0048,2.2460,2.6521,2.2555,2.2555,2.4563,2.7722
wing_area = 426
wing_span = 72
wing_root_chord = 7.5
wing_dihedral = 2.0
wing_incidence = 1.0
wing_twist = -1.5
oswald_efficiency_factor = 0.85
wing_winglets_flag = 0
wing_sweep = 1.0
wing_pos_apex_lon = 2.1
wing_pos_apex_vert = 2
htail_area = 67.0
htail_span = 17
htail_pos_lon = -22.5
htail_pos_vert = 2
htail_incidence = 0.5
htail_sweep = 10.0
vtail_area = 42.0
vtail_span = 13
vtail_sweep = 10
vtail_pos_lon = -23
vtail_pos_vert = -2.5
elevator_area = 17.0
aileron_area = 13.5
rudder_area = 7.3
elevator_up_limit = 17.0
elevator_down_limit = 15.5
aileron_up_limit = 18.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 15.0
spoiler_limit = 45.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1.0 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.5 
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=1.0 
rudder_trim_effectiveness=1.0 

[propeller]
thrust_scalar=1.0   //Propeller thrust scalar
propeller_type=0   //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=10   //Propeller Diameter, (feet)
propeller_blades=5   //Number of propeller blades
propeller_moi=24   //Propeller moment of inertia
beta_max=45    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2    //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=17.6  //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=0.0 //-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=29850                 //RPM, second stage compressor rated value
static_thrust=158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=4542                  //Maximum torque available (ft-lbs)

[gear_warning_system]
gear_warning_available = 0    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2
[Views]
eyepoint=4.54, -1.20, 3.25 

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 10                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20                                   // degrees
flaps-position.2 = 45                                   // degrees
flaps-position.3 = 85                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0	//1.25
drag_scalar = 2.5	//1.75
pitch_scalar = 1.0	//0.75

[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 

[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 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[Reference Speeds]
flaps_up_stall_speed=96.0 //Knots True (KTAS)
full_flaps_stall_speed=90.0 //76.8  //Knots True (KTAS)
cruise_speed=205.0   //Knots True (KTAS)
max_mach                = 0.58
max_indicated_speed     = 250		//Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=20