[fltsim.0]
title=chengdu j10
sim=ccc
model=
panel=
sound=
texture=
kb_checklists=
atc_id=VH BBB
ui_manufacturer=Chengdu
ui_type=J-10
ui_variation=Aussie
atc_flight_number=

description="Crew:1 Powerplant: One Lyulka Saturn AL-31F turbofan, rated at 17,857 lb (79.43 kN) dry and  27,557lb st (122.58 kN) with afterburning Maximum Speed: Mach 1.2 (sea-level) or Mach 2.0 (high altitude) Range Combat radius over 550 km Service  Ceiling: 18000 m G Limit: -3/+9 G Avionics: One PD radar (Russian Phazotron Zhuk-10 or Israeli EL/M-2035), with  detect-range 52.5~148 km, being able to track up to 8 targets simultaneously Fixed Weapon: One 23 mm internal cannon Stores Stations: 11, six under the wing and five under the fuselage, up to 4,500 kg  Air-to-Air Missiles: PL-8,PL-9, Python-4, R-73, R-77 Ground Attack Weapons: Laser-guided bomb, YJ-81(C-801) anti-ship missile"


[fltsim.1]
title=chengdu j10 Green
sim=ccc
model=1
panel=
sound=
texture=1
kb_checklists=
atc_id=1003
ui_manufacturer=Chengdu
ui_type=J-10
ui_variation=Green
atc_flight_number=

description="Crew:1 Powerplant: One Lyulka Saturn AL-31F turbofan, rated at 17,857 lb (79.43 kN) dry and  27,557lb st (122.58 kN) with afterburning Maximum Speed: Mach 1.2 (sea-level) or Mach 2.0 (high altitude) Range Combat radius over 550 km Service  Ceiling: 18000 m G Limit: -3/+9 G Avionics: One PD radar (Russian Phazotron Zhuk-10 or Israeli EL/M-2035), with  detect-range 52.5~148 km, being able to track up to 8 targets simultaneously Fixed Weapon: One 23 mm internal cannon Stores Stations: 11, six under the wing and five under the fuselage, up to 4,500 kg  Air-to-Air Missiles: PL-8,PL-9, Python-4, R-73, R-77 Ground Attack Weapons: Laser-guided bomb, YJ-81(C-801) anti-ship missile"

[fltsim.2]
title=chengdu j10 Grey
sim=ccc
model=2
panel=
sound=
texture=2
kb_checklists=
atc_id=02
ui_manufacturer=Chengdu
ui_type=J-10
ui_variation=Grey
atc_flight_number=

description="Crew:1 Powerplant: One Lyulka Saturn AL-31F turbofan, rated at 17,857 lb (79.43 kN) dry and  27,557lb st (122.58 kN) with afterburning Maximum Speed: Mach 1.2 (sea-level) or Mach 2.0 (high altitude)  Range: Combat radius over 550 km Service  Ceiling: 18000 m   G Limit: -3/+9 G  Avionics: One PD radar (Russian Phazotron Zhuk-10 or Israeli EL/M-2035), with a detect-range 52.5~148 km, being able to track up to 8 targets simultaneously Fixed Weapon: One 23 mm internal cannon Stores Stations: 11, six under the wing and five under the fuselage, up to 4,500 kg  Air-to-Air Missiles: PL-8, PL-9, Python-4, R-73, R-77 Ground Attack Weapons: Laser-guided bomb, YJ-81 (C-801) anti-ship missile"

[General]
atc_type=Airforce
atc_model=Airforce
editable=0
performance= maximum level speed Mach 2.5 at  (40,000ft)  ceiling above  50,000 feet. 

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000,0.000,0.000
empty_weight_CG_position=0.000,0.000,0.000
max_number_of_stations=50
station_load.0=0.000,0.000,0.000,0.000 //2882(with a full load fuel) max4500
empty_weight=9750
empty_weight_roll_MOI=120000.000
empty_weight_pitch_MOI=196385.000
empty_weight_yaw_MOI=250000.000
empty_weight_coupled_MOI=1300.000
max_gross_weight=18400

[fuel]

LeftMain =0.000,0.000,0.000,300.000,0.000
Center1=0.000,0.000,0.000,380.000,0.000
RightMain=0.000,0.000,0.000,300.000,0.000  

fuel_type=2.000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]

wing_area=500.000
wing_span=40.000
wing_root_chord=10.833333
wing_dihedral=2.142334
wing_incidence=-0.494385
wing_twist=-1.1563
oswald_efficiency_factor=3.195582
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=230.000
htail_span=22.500000
htail_pos_lon=-21.250000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=270.000
vtail_span=18.734994
vtail_sweep=0.000
vtail_pos_lon=-13.3
vtail_pos_vert=8.3
elevator_area=50.000
aileron_area=16.0
rudder_area=34.000
elevator_up_limit=16.5
elevator_down_limit=12.6
aileron_up_limit=15.5
aileron_down_limit=16.0
rudder_limit=23.50
elevator_trim_limit=25.000
spoiler_limit=29.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[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         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[contact_points]
point.0= 1.000, 23, 0.000, -4.6, 1781.102, 0.000, 0.790, 42.780, 0.599, 1.720, 0.441, 2.000, 3.000, 0.000, 0.000, 0.000
point.1= 1.000, -11.000, -10.282, -6.35, 1974.803, 1.000, 0.632, 0.000, 1.867, 1.700, 0.744, 2.000, 3.000, 2.000, 0.000, 0.000
point.2= 1.000, -11.000, 10.282, -6.35, 1974.803, 2.000, 0.632, 0.000, 1.867, 1.700, 0.744, 2.000, 3.000, 3.000, 0.000, 0.000
point.3= 2.000, -7.591, -16.090, -1.010, 787.402, 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, -7.591, 16.090, -1.010, 787.402, 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, -20.250, 0.000, 0.000, 787.402, 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, 19.099, 0.000, -2.343, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 5.000, 13.192, 0.000, -6.300, 1600, 0, 0.00, 50.0, 0.0,  0.0, 1.00, 3.0, 3.0, 0, 0.0, 0.0

static_pitch= 0.000
static_cg_height= 5.0
gear_system_type=0

[flaps.0]
type             = 2                        // Outboard Leading Edge Slat
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 45                                  // degrees
damaging-speed   = 450                                  // KIAS
blowout-speed    = 500                                  // KIAS

[flaps.1]
type             = 1                        // Outboard Leading Edge Slat
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                  // degrees
damaging-speed   = 450                                  // KIAS
blowout-speed    = 500  

[jet_engine]
thrust_scalar=1.000 

[GeneralEngineData]
engine_type= 1
Engine.0= -6.667, 0.000, 0.000
fuel_flow_scalar= 0.25
min_throttle_limit=-0.500000

[TurbineEngineData]
fuel_flow_gain= 0.001
inlet_area= 6.617
rated_N2_rpm= 29920.000
static_thrust= 17857.000
afterburner_available= 1
reverser_available= 0

[Reference Speeds]
flaps_up_stall_speed=108.000
full_flaps_stall_speed=85.000
cruise_speed=600
max_indicated_speed=1400.0
max_mach=2.500

[keyboard_response]
elevator=150.000,250.000
aileron=150.000,250.000
rudder=150.000,250.000

[Views]
eyepoint=12.6,0.0,4.3

[TailHook]
tailhook_length=4				;(feet)
tailhook_position = -13.6, 0.0, 0.4		;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000
pitch_takeoff_ga=8.000
max_pitch=10.000
max_pitch_acceleration=1.000
max_pitch_velocity_lo_alt=2.000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000
max_pitch_velocity_hi_alt_breakpoint=28000.000
max_bank=45.000
max_bank_acceleration=2.800000
max_bank_velocity=3.000
max_throttle_rate=0.100000
nav_proportional_control=9.000
nav_integrator_control=0.250000
nav_derivative_control=0.000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000
yaw_damper_gain=0.000

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                //BusType, MaxAmpLoad, MinVoltage       //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 5 , 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 2 , 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

[direction_indicators]
direction_indicator.0=3,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -10.0, -14.29, -0.40,  fx_navred  ,
light.1 = 3, -10.0,  14.29, -0.40,  fx_navgre  ,
light.2 = 3,   4.1,   0.00, -1.90,  fx_navwhi  ,
light.3 = 2,  -9.8, -14.29, -0.40,  fx_strobe  ,
light.4 = 2,  -9.8,  14.29, -0.40,  fx_strobe  ,
light.5 = 2, -20.0,   0.00, 11.1,  fx_strobe  ,
light.6 = 1, -19.5,   0.00, 10.9,  fx_beacon  ,
light.7 = 1,  11.00,  0.00, -1.55,  fx_beacon  ,
light.8 = 4,  14.115,  0.00,  3.0,  fx_vclight1  ,

[brakes]
toe_brakes_scale=1.100000
parking_brake=1

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

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

[exits]
number_of_exits = 1 
exit_rate.0 = 0.4                               ;Percent per second 
exit_rate.1 = 0.4                               ;Percent per second

[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

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000
flap_limit_power=0.000
flap_limit_idle=0.000

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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