[fltsim.0]
title=L-159A-1
sim=alcaa
model=1
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=clean
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.1]
title=L-159A-2
sim=alcaa
model=2
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=long range
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.2]
title=L-159A-3
sim=alcaa
model=3
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=Anti Ground
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.3]
title=L-159A-4
sim=alcaa
model=4
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=3x plamen
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.4]
title=L-159A-5
sim=alcaa
model=5
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=350l tanks
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.5]
title=L-159A-6
sim=alcaa
model=1
panel=
sound=
texture=ani
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=clean 6066
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.6]
title=L-159A-7
sim=alcaa
model=2
panel=
sound=
texture=ani
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=long range 6066
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.7]
title=L-159A-8
sim=alcaa
model=3
panel=
sound=
texture=ani
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=Anti Ground 6066
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.8]
title=L-159A-9
sim=alcaa
model=4
panel=
sound=
texture=ani
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=3x plamen 6066
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[fltsim.9]
title=L-159A-10
sim=alcaa
model=5
panel=
sound=
texture=ani
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id=NSSJ
atc_airline=Czech Air Force
atc_flight_number=CZ007
ui_manufacturer=Aero Vodochody
ui_type=L-159A
ui_variation=350l tanks 6066
description =Advanced Light Combat Aircraft \nAuthor: Vit Storch (c)2008\n 
atc_heavy=0
visual_damage=1 

[General]
atc_type=AEROSTAR
atc_model=L159
performance=Manufactured by Aero Vodochody\/Boeing\nWing span: \t                       9,54 m\nLength: \t                                    12,73 m\nHeight: \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= 17637.000
empty_weight = 9590.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, -1.000

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

;Moments of Inertia
empty_weight_pitch_MOI = 20651.000
empty_weight_roll_MOI  = 5500.000
empty_weight_yaw_MOI   = 10800.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =0.814
induced_drag_scalar    =1.500
elevator_effectiveness =0.712
aileron_effectiveness  =1.303
rudder_effectiveness   =0.790
pitch_stability        =1.351
roll_stability         =1.405
yaw_stability          =1.306
elevator_trim_effectiveness =1.802
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)
fuel_transfer_pump         = 0, 10, 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, 11.667, 0.000, -5.250, 1574.803, 0.000, 0.566, 30.000, 0.180, 2.000, 0.700, 6.000, 8.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.250, -5.083, -5.900, 1574.803, 1.000, 0.566, 0.000, 0.700, 1.500, 0.500, 5.000, 7.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.250, 5.083, -5.900, 1574.803, 2.000, 0.566, 0.000, 0.700, 1.500, 0.500, 5.400, 7.300, 3.000, 0.000, 0.000
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, -16.167, 0.000, -2.333, 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, 20.417, 0.000, -3.333, 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 = 9.6, 0, 1.8 //9.5, 0, 1.7


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,   4.00, -15.55, -0.65, fx_navred           // (feet) longitudinal, lateral, vertical 
light.1=3,   4.00,  15.55, -0.65, fx_navgre
light.2=3, -19.00,   0.00,  9.90, fx_navwhi
light.3=1,  -1.95,   0.00,  3.50, fx_beacon 
light.4=4,     11,   1.50,  -1.5,  fx_vclight
light.5=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, 1

[SMOKESYSTEM]
smoke.0=-9.00, -6.00,  9.10, fx_contrail_s
smoke.1=-9.00, -6.00, -9.10, fx_contrail_s


[fuel]
Center1= 0.000, 0.000, -1.000, 350.000, 1.000
LeftMain= 0.000, -9.000, -1.000, 220.000, 1.000
RightMain= 0.000, 9.000, -1.000, 220.000, 1.000
fuel_type= 2.000
number_of_tank_selectors= 1
electric_pump=1

[airplane_geometry]
wing_area= 184.000
wing_span= 31.500
wing_root_chord= 8.250
wing_dihedral= 1.000
wing_incidence= 0.000
wing_twist= 0.000
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.500
wing_pos_apex_vert= -1.500
htail_area= 57.500
htail_span= 15.000
htail_pos_lon= -14.500
htail_pos_vert= 2.310
htail_incidence= -0.500
htail_sweep= 0.000
vtail_area= 47.000
vtail_span= 9.000
vtail_sweep= 30.000
vtail_pos_lon= -13.500
vtail_pos_vert= 2.800
elevator_area= 28.000
aileron_area= 26.000
rudder_area= 12.960
elevator_up_limit= 18.000
elevator_down_limit= 12.000
aileron_up_limit= 25.000
aileron_down_limit= 25.000
rudder_limit= 25.000
elevator_trim_limit= 10.000
spoiler_limit= 45.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000

[GeneralEngineData]
engine_type= 1
Engine.0= -16.500, 0.000, 0.000
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= 4.200
rated_N2_rpm= 29920.000
static_thrust= 6330.000
afterburner_available= 0
reverser_available= 0.000

[Reference Speeds]
flaps_up_stall_speed= 110.000
full_flaps_stall_speed= 80.000
cruise_speed= 501.000
max_mach=0.82
max_indicated_speed= 600.000

[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= 0.400
extending-time= 4.000
system_type= 1
damaging-speed= 210.000
blowout-speed= 240.000
lift_scalar= 0.200
drag_scalar= 0.150
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