[fltsim.0]
title=L-39C
sim=L39C
model=
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=LET
atc_flight_number=035
ui_manufacturer=LET
ui_type=L-39C
ui_variation=VVS USSR
description =well known jet fighter trainer
atc_heavy=0
visual_damage=1 

[fltsim.1]
title=L-39Clit
sim=L39C
model=
panel=
sound=
texture=lit
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=LET
atc_flight_number=RF103
ui_manufacturer=LET
ui_type=L-39C
ui_variation=Vjazma-Rus
description =well known jet fighter trainer
atc_heavy=0
visual_damage=1 

[fltsim.2]
title=L-39Cwc
sim=L39C
model=
panel=
sound=
texture=wc
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=LET
atc_flight_number=04
ui_manufacturer=LET
ui_type=L-39C
ui_variation=Belaja Rus
description =well known jet fighter trainer
atc_heavy=0
visual_damage=1 

[fltsim.3]
title=L-39Cr
sim=L39C
model=
panel=
sound=
texture=r
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=LET
atc_flight_number=035
ui_manufacturer=LET
ui_type=L-39C
ui_variation=Aerobatic team "RUS'"
description =well known jet fighter trainer
atc_heavy=0
visual_damage=1 
 


//---------
[General]
atc_type=AEROSTAR
atc_model=L39C
performance=Manufactured by Aero Vodochody\/Boeing\nWing span: \t                       9,54 m\nLength: \t                                    12,73 m\nHight: \t                        4,77 m (4,87 m)\nMax. level speed:    936 km\/hr (505 KTAS)\nMax. rate of climb: \t62.1 m\/s (12,210 ft\/min)\nLoad factor \t\t    +8g\/-4g\nMax. ramp weight \t     8,000kg (17,637 lb)\nService ceiling           13,200 m (43,300 ft)\nInternal fuel \t         1,547 kg (3,411 lb)\nTotal fuel (int.+4 x ext.)  2,924 kg (6,447 lb)\nMax. range (int. fuel only)  1,570 km (850 nm)\nMax. range (int., ext. fuel)2,530 km (1,350 nm)\n\n

=============================================================================================
[WEIGHT_AND_BALANCE]
max_gross_weight= 12360.000	// podla wiki
empty_weight = 7625.000		// podla wiki

reference_datum_position     = 0.000, 0.000, 0.000
//empty_weight_CG_position     = -0.300, 0.000, 0.000
//empty_weight_CG_position     = 0.300, 0.000, -1.000
empty_weight_CG_position     = 0.300, 0.000, -0.500


max_number_of_stations = 5
station_load.0 =200.000000, 8.500000, 0.000000, 0.000000, pilot/student
station_load.1 =160.000000, 3.000000, 0.000000, 0.000000, instructor

;Moments of Inertia
empty_weight_pitch_MOI = 18820.000
empty_weight_roll_MOI  = 15000.000
empty_weight_yaw_MOI   = 25512.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.500
CG_aft_limit= 0.500

------------------------------------------------------
[flight_tuning]			//povodne vsetko=1
cruise_lift_scalar     =0.80
parasite_drag_scalar   =0.70
induced_drag_scalar    =0.70

elevator_effectiveness =1.40
aileron_effectiveness  =1.30
rudder_effectiveness   =0.70

pitch_stability        =0.9
roll_stability         =0.9
yaw_stability          =0.9

elevator_trim_effectiveness =1.20
aileron_trim_effectiveness  =1.20
rudder_trim_effectiveness   =1.20

-------------------------------------------------------

[airplane_geometry]
wing_area= 202.250	// podla wiki
wing_span= 31.000	// podla wiki
wing_root_chord= 8.930	// merane priblizne
wing_dihedral= 2.000
wing_incidence= 0.000
wing_twist= 0.000
oswald_efficiency_factor= 0.600		// povodne 0,9
wing_winglets_flag= 0
wing_sweep= 2.000
wing_pos_apex_lon= 0.00
wing_pos_apex_vert= -1.060

htail_area= 80.000	// merane priblizne
htail_span= 14.600	// merane priblizne
htail_pos_lon= -18.500
htail_pos_vert= 2.000
htail_incidence= 0.000
htail_sweep= 10.000
vtail_area= 67.300	// merane priblizne
vtail_span= 7.450	// merane priblizne
vtail_sweep= 40.000
vtail_pos_lon= -17.500
vtail_pos_vert= 0.000

elevator_area= 32.000	// merane priblizne
aileron_area= 33.500	// merane priblizne
rudder_area= 22.380	// merane priblizne

elevator_up_limit= 30.000
elevator_down_limit= 20.000
aileron_up_limit= 18.000
aileron_down_limit= 16.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 55.000
spoilerons_available    =0
aileron_to_spoileron_gain=0.0
min_ailerons_for_spoilerons=0.0
min_flaps_for_spoilerons=0.0

-------------------------------------------------------------
[GeneralEngineData]
engine_type= 1
//aav
//Engine.0= -16.00, 0.00, 0.00
//Engine.0= -16.00, 0.00, -0.3
Engine.0= -16.00, 0.00, -0.5


fuel_flow_scalar= 1.1538	//zere 15 l/min pri N1=80% (hodnota 1.0 = 13 l/min)
min_throttle_limit = 0		//Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain= 0.015	
inlet_area= 3.900
rated_N2_rpm= 15920.000
static_thrust= 3600.000		// podla wiki	//zere cca 1307 l/h podla vypoctu
afterburner_available= 0
reverser_available= 0.000

[fuel]
//aav//Center1= -1.50, 0.000, 1.00, 290.500, 10.000		// =1100 l
Center1  = -1.50,   0.000, -0.50, 290.500, 10.000		// =1100 l
LeftMain =  0.000, -15.00, -0.800, 26.500, 3.000		// = 100 l
RightMain=  0.000,  15.00, -0.800, 26.500, 3.000
fuel_type=  2.000
number_of_tank_selectors= 1
electric_pump=1

[jet_engine]
thrust_scalar =1.000

--------------------------------------------------------
        //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)

[contact_points] 
//aav//point.0= 1.000, 12.213, 0.000, -5.600, 1574.803, 0.0, 1.200, 25.00, 0.200, 4, 0.85, 4.0, 5.0, 0, 220, 280
//
point.0= 1.000, 14.213, 0.000, -5.700, 1574.803, 0.0, 0.60, 25.00, 0.200, 5,     0.50,  4.0, 5.0, 0, 220, 280
point.1= 1.000, -1.16, -4.010, -5.650, 1574.803, 1.0, 0.90, 0.000, 0.400, 1.600, 0.500, 5.000, 6.000, 2.000, 220.000, 280.000
point.2= 1.000, -1.16,  4.010, -5.650, 1574.803, 2.0, 0.90, 0.000, 0.400, 1.600, 0.500, 5.200, 6.100, 3.000, 220.000, 280.000
// drak
point.3= 2.000, 3.000, -15.750, -1.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000     // LKridloVpredu
point.4= 2.000, 3.000, 15.750, -1.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000      // PKridloVpredu
point.5= 2.000, -4.000, -15.750, -1.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000    // LKridloVzadu
point.6= 2.000, -4.000, 15.750, -1.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000     // PKridloVzadu
point.7= 2.000, -19.00,   0.00,  9.5, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000   // Smerovka
point.8= 2.000, -2.000, -4.75, -2.000, 2074.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000      // LBok
point.9= 2.000, -2.000, 4.750, -2.000, 2074.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000      // PBok
point.10= 2.00, 12.000, 0.000, -2.000, 2074.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000      // PBok
point.11= 2.00, -17.167, 0.000, -1.3, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000   //dyza
point.12= 2.00, 16.417, 0.000, -3.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000  //nos

static_pitch= -0.500
static_cg_height= 5.3//aav//5.650
gear_system_type=1      //Hydraulic


[Views]
eyepoint = 8.75, 0, 1.9		//9.5, 0, 1.7

[LIGHTS]	//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,   1.80, -15.55, -0.62, fx_navred           // (feet) longitudinal, lateral, vertical 
light.1=3,   1.80,  15.55, -0.62, fx_navgre
light.2=2,   1.60, -15.55, -0.62, fx_recog          
light.3=2,   1.60,  15.55, -0.62, fx_recog
light.4=3, -19.45,   0.00,  9.95, fx_navwhi 
light.5=4,     11,   1.50,  -1.5,  fx_vclight
light.6=4,     11,  -1.50,  -1.5,  fx_vclight

--------------------------------------------------------------
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 230.0
blowout-speed= 260.0
lift_scalar= 0.00//aav//0.20
drag_scalar= 0.35
pitch_scalar= 0.10
flaps-position.0= 0.000, 0.000		// 0 stupnov
flaps-position.1= 50.000, 0.000		//25 stupnov
flaps-position.2= 100.000, 0.000	//44 stupnov
//
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 230.0
blowout-speed= 260.0
lift_scalar= 0.20
drag_scalar= 0.00//aav//0.35
pitch_scalar= 0.10
flaps-position.0= 0.000, 0.000		// 0 stupnov
flaps-position.1= 50.000, 0.000		//25 stupnov
flaps-position.2= 100.000, 0.000	//44 stupnov

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.0     //Percent throttle that activates warning
flap_limit_idle    =  49.0     //Flap angle that activates warning at idle
flap_limit_power   = 99.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1     	  //Parking brake available
toe_brakes_scale = 0.5//aav//0.8	  //Brake scalar
differential_braking_scale = 1

[hydraulic_system]
normal_pressure = 3000.0   //PSI
electric_pumps  = 0        //no electric pumps
engine_map      = 1,0,0,0  //pumps on Eng1,2,3,4

[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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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

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

[SMOKESYSTEM]
smoke.0= 0, -20, 0, fx_smoke_w

[Reference Speeds]
flaps_up_stall_speed= 110.000
full_flaps_stall_speed= 80.000
cruise_speed= 350.000
max_mach=0.82
max_indicated_speed= 500.000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=108
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
autoland_available=1
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=12.000000
max_pitch_acceleration=3.000000
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=45.000000
max_bank_acceleration=4.000000
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

[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

[exits]
number_of_exits=2
exit_rate.0=0.6
exit_rate.1=0.8

[stall_warning]
type=1


[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
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 3 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 1 , 17.0
gear_warning       = 0, 1 , 17.0
fuel_pump          = 0, 4 , 17.0
starter1           = 0, 20, 18.0
light_nav          = 0, 3 , 17.0
light_beacon       = 0, 3 , 17.0
light_landing      = 0, 8 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 3 , 17.0
light_panel        = 0, 2 , 17.0