[General]
atc_type=AEROSTAR
atc_model=V1
editable=0
performance=\n

[fltsim.0]
title=AI kamaz
sim=KAMAZ
model=Kamaz
panel=
sound=
texture=
atc_airline=AEROFLOT
ui_manufacturer=AI
ui_type=kamaz
ui_variation=kamaz
visual_damage=1
atc_parking_types=Cargo
atc_parking_codes=avto

[weight_and_balance]

// ACM V2.3
max_gross_weight = 6000
empty_weight = 2500
reference_datum_position = 3.6, 0, 0
empty_weight_CG_position = -3, 0, 0
empty_weight_pitch_MOI = 8400
empty_weight_roll_MOI = 1137
empty_weight_yaw_MOI = 2000
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = "170, -3.0, -1.5, -2.0, "
station_load.1 = "170, -3.0,  1.5, -2.0, "
station_load.2 = "0, -3.2, -1.5, -2.0, "
station_load.3 = "0, -6.2,  1.5, -2.0, "
station_load.4 = "0, -8.0,  0.0, -2.0, "

[lights]

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

light.0 = 3, 7.94, 0, 6.66, fx_VEH_EmergencyLights
light.1 = 3, 8.55, 0, 4.34, fx_shockwave_vclight
light.2 = 3, 11.11, -2.71, 1.51, fx_shockwave_landing_light_narrow_no_flare
light.3 = 3, 11.11, 2.86, 1.51, fx_shockwave_landing_light_narrow_no_flare
light.4 = 1, -16.44, 3.54, 3.73, fx_navredc
light.5 = 3, -16.41, -3.59, 3.73, fx_navred

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =0 
fuel_flow_scalar = 0.88
engine.0 = -10.0, 0.0, -3.0
min_throttle_limit=0.599976

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

[fuel]

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

fuel_type = 1
number_of_tank_selectors = 1

LeftMain = -3, 0, 0, 139, 0
electric_pump=0

[contact_points]
static_pitch = 0
static_cg_height = 1.5
max_number_of_points = 10

point.0 = 1,  2.50,  -2.61, -1.62 , 9500, 0, 2.0, 38.0, 0.3,1.5, 1.8, 0.0, 0.0, 0
point.1 = 1,  2.50,   2.61, -1.62 , 9500, 0, 2.0, 38.0, 0.3,1.5, 1.8, 0.0, 0.0, 0
point.2 = 1, -5.8, -2.65, -1.83, 9500, 1, 1.5,  0.0, 0.5, 1.5, 1.8, 0.0, 0.0, 2
point.3 = 1, -5.8  2.65, -1.83, 9500, 2, 1.5,  0.0, 0.5, 1.5, 1.8, 0.0, 0.0, 3
point.4 = 2, 3.0, -2.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.5 = 2, 3.0   2.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.6 = 2,-10.23,   0.0,  0.30, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.7 = 2,  1.48,   0.0, 1.70, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.8 = 2,-12.80,   0.0,  5.83, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.9 = 2, -4.90,   0.0, 1.70, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8

[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000

[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

[airplane_geometry]
//ACM_AREAW1// 0,0,0,0.2743,0.1710,0.1710,0,0.2606,0.3420,0.3420
//ACM_AREAW2// 0,0.2468,0.5130,0.5130,0,0.2330,0.6840,0.6840,0,0.2194
//ACM_AREAW3// 0.8550,0.8550,0,0.2056,1.0261,1.0261,0,0.1920,1.1971,1.1971
//ACM_AREAW4// 0,0.1782,1.3681,1.3681,0,0.1644,1.5391,1.5391,0,0.1508
//ACM_AREAH1// 0,0,0,1.1886,0.1981,0.1981,0.0348,1.1641,0.3962,0.3962
//ACM_AREAH2// 0.0697,1.1397,0.5942,0.5942,0.1048,1.1152,0.7924,0.7924,0.1396,1.0907
//ACM_AREAH3// 0.9904,0.9904,0.1746,1.0662,1.1886,1.1886,0.2096,1.0417,1.3868,1.3868
//ACM_AREAH4// 0.2444,1.0171,1.5849,1.5849,0.2793,0.9926,1.7829,1.7829,0.3143,0.9682
//ACM_AREAV1// 0,0,0,1.4630,0.1624,0.1624,0.1363,1.4823,0.3251,0.3251
//ACM_AREAV2// 0.2727,1.5017,0.4875,0.4875,0.4092,1.5211,0.6502,0.6502,0.5455,1.5404
//ACM_AREAV3// 0.8127,0.8127,0.6819,1.5598,0.9753,0.9753,0.8184,1.5792,1.1378,1.1378
//ACM_AREAV4// 0.9548,1.5985,1.3004,1.3004,1.0911,1.6179,1.4630,1.4630,1.2275,1.6371
//ACM_CAREAW1// 0.7695,0.7695,0.1370,0.1920,0.8550,0.8550,0.1370,0.1891,0.9405,0.9405
//ACM_CAREAW2// 0.1370,0.1864,1.0261,1.0261,0.1370,0.1836,1.1116,1.1116,0.1370,0.1809
//ACM_CAREAW3// 1.1971,1.1971,0.1370,0.1782,1.2826,1.2826,0.1370,0.1755,1.3681,1.3681
//ACM_CAREAW4// 0.1370,0.1728,1.4536,1.4536,0.1370,0.1700,1.5391,1.5391,0.1370,0.1673
//ACM_CAREAH1// 0,0,0.5942,1.1886,0.1981,0.1981,0.6291,1.1938,0.3962,0.3962
//ACM_CAREAH2// 0.6642,1.1991,0.5942,0.5942,0.6991,1.2043,0.7924,0.7924,0.7340,1.2094
//ACM_CAREAH3// 0.9904,0.9904,0.7689,1.2146,1.1886,1.1886,0.8039,1.2200,1.3868,1.3868
//ACM_CAREAH4// 0.8388,1.2252,1.5849,1.5849,0.8737,1.2303,1.7829,1.7829,0.9086,1.2355
//ACM_CAREAV1// 0,0,0.3657,1.0972,0.1624,0.1624,0.5020,1.1750,0.3251,0.3251
//ACM_CAREAV2// 0.6384,1.2530,0.4875,0.4875,0.7749,1.3308,0.6502,0.6502,0.9113,1.4088
//ACM_CAREAV3// 0.8127,0.8127,1.0477,1.4866,0.9753,0.9753,1.1841,1.5644,1.1378,1.1378
//ACM_CAREAV4// 1.3205,1.6424,1.3004,1.3004,1.4569,1.7202,1.4630,1.4630,1.5932,1.7982
wing_area = 10.0
wing_span = 10.1
wing_root_chord = 0.9
wing_dihedral = 1.7
wing_incidence = 1.5
wing_twist = -3.0
oswald_efficiency_factor = 0.68
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = -2.4
wing_pos_apex_vert = 0.0
htail_area = 9.0
htail_span = 11.7
htail_pos_lon = -18.3
htail_pos_vert = 0.0
htail_incidence = 3.2
htail_sweep = 10.0
vtail_area = 18.0
vtail_span = 4.8
vtail_sweep = 40.0
vtail_pos_lon = -16.2
vtail_pos_vert = 1.5
elevator_area = 16.6
aileron_area = 0.1
rudder_area = 0.7
elevator_up_limit = 28.0
elevator_down_limit = 21.0
aileron_up_limit = 90.0
aileron_down_limit = 90.0
rudder_limit = 34.0
elevator_trim_limit = 19.5
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
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
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=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.0 
roll_stability=1.6 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[piston_engine]
power_scalar=1.0                             //Piston power scalar
cylinder_displacement=90.0                     //Cubic inches per cylinder
compression_ratio=8.5                          //Compression ratio
number_of_cylinders=6                          //Number of cylinders
max_rated_rpm=3700                             //Max rated RPM
max_rated_hp=260                               //Max rated HP
fuel_metering_type=0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                 //Starter torque factor
turbocharged=0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0                                //Max design manifold pressure, (inHg)
min_design_mp=0                                //Min design manifold pressure, (inHg)
critical_altitude=0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
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=0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
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=1.0                             //Propeller thrust scalar
propeller_type=1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.3                         //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=5.0                              //Propeller moment of inertia
beta_max=0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0                                  //Miminum governed RPM
prop_tc=0                                      //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=20                            //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=0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0                          //Minimum RPM for prop feathering
beta_feather=0                                 //Feathering pitch angle (degrees)
power_absorbed_cf=0                            //Coefficient of friction for power absorbed by propeller
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                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0                         //Minimum pitch angle in reverse, (degrees)

[brakes]
parking_brake=1.4        //Parking brake available
toe_brakes_scale=1.0  //Brake scalar
[hydraulic_system]
normal_pressure=0.0    //PSI
[Views]
eyepoint=-3.8, 1.4, 3.35        //(feet) longitudinal, lateral, vertical distance from reference datum

[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 
//[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=5,  2.8, -1.95, -1.34, fx_landing,
light.1=5,  2.8,  1.95, -1.34, fx_landing,
light.2=4,  -3.25, 0.0, 0.89, fx_vclight,

[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 

[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=1,1    //Turn AND Bank
[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=7                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=12.7                                 // degrees
flaps-position.2=25.3                                 // degrees
flaps-position.3=38                                   // degrees
damaging-speed=120                                  // KIAS
blowout-speed=150                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=0                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[Reference Speeds]
flaps_up_stall_speed=53.0                  //Knots True (KTAS)
full_flaps_stall_speed=48.0                  //Knots True (KTAS)
cruise_speed=115.0                 //Knots True (KTAS)
max_indicated_speed=263                   //Red line (KIAS)
max_mach=1.000000

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.0 
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=0.0

[stall_warning]
type=1
[exits]
number_of_exits=2
exit_rate.0=0.5                               ;Percent per second
exit_rate.1=0.7                               ;Percent per second

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.7,0.7	                          ;Percent per second