[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 

 


[General]
atc_type=LET
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= 10360.000
empty_weight = 7625.000

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

station_load.0 =170.000000, 10.000000, 0.000000, 0.000000, longitudinal
max_number_of_stations = 50

;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]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[jet_engine]
thrust_scalar =1.000

[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

        //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]
point.0= 1.000, 12.213, 0.000, -5.350, 1574.803, 0.000, 0.748, 25.000, 0.180, 2.000, 0.700, 7.000, 8.000, 0.000, 250.000, 280.000
point.1= 1.000, -1.16, -4.010, -5.650, 1574.803, 1.000, 1.053, 0.000, 0.400, 1.600, 0.500, 8.000, 9.000, 2.000, 250.000, 280.000
point.2= 1.000, -1.16, 4.010, -5.650, 1574.803, 2.000, 1.053, 0.000, 0.400, 1.600, 0.500, 8.200, 9.100, 3.000, 250.000, 280.000
point.3= 2.000, 0.000, -14.750, -2.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.000, 14.750, -2.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -13.167, 0.000, -1.7, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 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

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

[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 = 1.0  //Brake scalar

[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

[Views]
eyepoint = 8.45, 0, 1.67 //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


[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



[fuel]
Center1= -1.50, 0.000, 1.00, 290.000, 1.000
LeftMain= 0.000, -15.000, -0.800, 26.000, 1.000
RightMain= 0.000, 15.000, -0.800, 26.000, 1.000
fuel_type= 2.000
number_of_tank_selectors= 1
electric_pump=1

[airplane_geometry]
wing_area= 202.250
wing_span= 31.000
wing_root_chord= 8.530
wing_dihedral= 2.000
wing_incidence= 0.000
wing_twist= 0.000
oswald_efficiency_factor= 0.900
wing_winglets_flag= 0
wing_sweep= 2.000
wing_pos_apex_lon= 1.880
wing_pos_apex_vert= -1.060
htail_area= 54.000
htail_span= 14.400
htail_pos_lon= -14.500
htail_pos_vert= 2.000
htail_incidence= 0.000
htail_sweep= 10.000
vtail_area= 40.100
vtail_span= 7.500
vtail_sweep= 40.000
vtail_pos_lon= -13.500
vtail_pos_vert= 0.000
elevator_area= 15.100
aileron_area= 28.800
rudder_area= 9.580
elevator_up_limit= 30.000
elevator_down_limit= 20.000
aileron_up_limit= 17.000
aileron_down_limit= 17.000
rudder_limit= 30.000
elevator_trim_limit= 25.000
spoiler_limit= 55.000
spoilerons_available    =0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000


[GeneralEngineData]
engine_type= 1
Engine.0= -18.200, 0.000, 0.800
fuel_flow_scalar= 1.000
min_throttle_limit = 0                        //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 3.400
rated_N2_rpm= 29920.000
static_thrust= 3790.000
afterburner_available= 0
reverser_available= 0.000

[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 = 100
autothrottle_takeoff_ga= 1
pitch_takeoff_ga = 8
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=35.0
max_bank_acceleration=3.5
max_bank_velocity=4.00
max_throttle_rate=0.20
nav_proportional_control=11.00
nav_integrator_control=0.20
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

[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

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 230.000
blowout-speed= 260.000
lift_scalar= 0.200
drag_scalar= 0.350
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 50.000, 0.000
flaps-position.2= 100.000, 0.000