[fltsim.0]
title=AAF-111C_1SQ_01
sim=f111
model=clean
panel=
sound=
texture=1_129
kb_checklists=
kb_reference=
atc_id=A8-129
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=1Sq A8-129
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=TB1

[fltsim.1]
title=AAF-111C_1SQ_02
sim=f111
model=gbu
panel=
sound=
texture=1_130
kb_checklists=
kb_reference=
atc_id=A8-130
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=1Sq A8-130
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=TB2

[fltsim.2]
title=AAF-111C_1SQ_03
sim=f111
model=gbu
panel=
sound=
texture=1_135
kb_checklists=
kb_reference=
atc_id=A8-135
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=1Sq A8-135
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=TB3

[fltsim.3]
title=AAF-111C_1SQ_04
sim=f111
model=gbu
panel=
sound=
texture=1_137
kb_checklists=
kb_reference=
atc_id=A8-137
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=1Sq A8-137
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=TB4


[fltsim.4]
title=AAF-111C_6SQ_01
sim=f111
model=tanks
panel=
sound=
texture=6_131
kb_checklists=
kb_reference=
atc_id=A8-131
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=6Sq A8-131
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=V086

[fltsim.5]
title=AAF-111C_6SQ_02
sim=f111
model=tanks
panel=
sound=
texture=6_133
kb_checklists=
kb_reference=
atc_id=A8-133
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=6Sq A8-133
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=V086

[fltsim.6]
title=AAF-111C_6SQ_03
sim=f111
model=tanks
panel=
sound=
texture=6_134
kb_checklists=
kb_reference=
atc_id=A8-134
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=6Sq A8-134
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=V086

[fltsim.7]
title=AAF-111C_6SQ_04
sim=f111
model=gbu
panel=
sound=
texture=6_136
kb_checklists=
kb_reference=
atc_id=A8-136
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=6Sq A8-136
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=V086


[fltsim.8]
title=AAF-111C_AR_01
sim=f111
model=gbu
panel=
sound=
texture=A_145
kb_checklists=
kb_reference=
atc_id=A8-145
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=Ard A8-145
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=433W

[fltsim.9]
title=AAF-111C_AR_02
sim=f111
model=gbu
panel=
sound=
texture=A_146
kb_checklists=
kb_reference=
atc_id=A8-146
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=Ard A8-146
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=433W

[fltsim.10]
title=AAF-111C_AR_03
sim=f111
model=gbu
panel=
sound=
texture=A_147
kb_checklists=
kb_reference=
atc_id=A8-147
ui_manufacturer=General Dynamics
ui_type=AI F-111C
ui_variation=Ard A8-147
description=" "
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=MIL_COMBAT
atc_parking_codes=433W

[General]
atc_type=SILENT
atc_model=F111
editable=0
performance=Cruise Speed\tMach .81\nMaximum Range\t2,200 nm\nService Ceiling\t51,000 ft\nMax Gross Weight\t20,450 lb\nSeating\t\tUp to 9\nUseful Load\t2,650 lb\n
Category=airplane

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight = 100000.000
empty_weight = 47175.000

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

max_number_of_stations = 50


;Moments of Inertia
empty_weight_pitch_MOI  = 2000000.000
empty_weight_roll_MOI   = 60000.000
empty_weight_yaw_MOI    = 220000.000
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   =1.000
induced_drag_scalar    =0.501
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =2.002
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =0.509
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 1
Engine.0 = -26.000, -2.800, 0.000
Engine.1 = -26.000, 2.800, 0.000
fuel_flow_scalar = 1.000
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.500
inlet_area = 6.000
rated_N2_rpm = 29920.000
static_thrust = 25000.000
afterburner_available = 1
reverser_available = 0.000

[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
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5,  17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2,  17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 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, 24.200, 0.000, -7.000, 1500.000, 0.000, 1.000, 45.000, 0.120, 3.500, 0.900, 4.000, 4.000, 0.000, 220.000, 250.000
point.1= 1.000, -2.000, -5.000, -7.200, 2000.000, 1.000, 2.000, 0.000, 1.000, 2.500, 0.700, 5.000, 5.000, 2.000, 220.000, 250.000
point.2= 1.000, -2.000, 5.000, -7.200, 2000.000, 2.000, 2.000, 0.000, 1.000, 2.500, 0.700, 5.000, 5.000, 3.000, 220.000, 250.000

point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -54.000, 0.000, 2.830, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

max_number_of_points = 21

static_pitch= 0.000
static_cg_height= 6.500
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 50.0     //Flap angle that activates warning at idle
flap_limit_power   = 50.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.885  //Brake scalar
auto_brakes=4

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

[Views]
eyepoint=24.63, -1.16, 2.85 





[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, 5=landing

light.1 = 1,   14.0,   0.00,  4.1, fx_beaconh,
light.2 = 4,  26.27,   0.00,  3.13, fx_vclight_red.fx,,
light.3 = 2,  -24.50,  -2.60,  -0.65, Copy of fx_f16_ab.fx
light.4 = 2,  -24.50,   2.60,  -0.65, Copy of fx_f16_ab.fx
light.5 = 1,   7.0,   0.00,  -3.0, fx_beaconh,
light.6 = 3, -30.0, 0, 11.0, fx_navwhi
light.7 = 3, 14.7, -5.6, 2.3, fx_navred
light.8 = 3, 14.8, 5.6, 2.3, fx_navgre

//light.9 = 2,  -48.50,  -2.60,  -0.65, fx_eng_exhaust_gry,
//light.10 = 2,  -48.50,   2.60,  -0.65, fx_eng_exhaust_gry,
light.9 = 2,  -48.50,  -2.60,  -0.65, fx_nicksmokeAI_sm_lear,
light.10 = 2,  -48.50,   2.60,  -0.65, fx_nicksmokeAI_sm_lear,

[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=0,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=0
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=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[fuel]
Center1    = 13.000, 0.000, 0.000, 2800.000, 0.000
LeftMain  = 0.000, -8.000, 0.000, 389.000, 0.000
RightMain = 0.000, 8.000, 0.000, 389.000, 0.000
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0
Center2= -10.000, 0.000, 0.000, 1383.000, 0.000

[airplane_geometry]
wing_area               = 500.000
wing_span               = 32.000
wing_root_chord         = 15.000
wing_dihedral           = 0.000
wing_incidence          = 2.000
wing_twist              = 0.000
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 0
wing_sweep              = 35.000
wing_pos_apex_lon       = 15.000
wing_pos_apex_vert      = 0.000
htail_area              = 190.000
htail_span              = 30.000
htail_pos_lon           = -40.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 50.000
vtail_area              = 140.000
vtail_span              = 9.000
vtail_sweep             = 50.000
vtail_pos_lon           = -40.000
vtail_pos_vert          = 3.000
elevator_area           = 190.000
aileron_area            = 190.000
rudder_area             = 70.000
elevator_up_limit       = 20.000
elevator_down_limit     = 15.000
aileron_up_limit        = 20.000
aileron_down_limit      = 20.000
rudder_limit            = 20.000
elevator_trim_limit     = 15.000
spoiler_limit           = 60.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed    = 170.000
full_flaps_stall_speed  = 140.000
cruise_speed            = 540.000
max_mach                = 2.50
max_indicated_speed     = 1700                  //Red line (KIAS)

[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

[stall_warning]
type=2
stick_shaker=1



[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 8.000
system_type= 1
damaging-speed= 999.000
blowout-speed= 999.000
lift_scalar= 1.000
drag_scalar= 0.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
flaps-position.3= 40.000, 0.000
flaps-position.4= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 8.000
system_type= 1
damaging-speed= 999.000
blowout-speed= 999.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 20.000, 0.000
flaps-position.4= 40.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.900
extending-time= 4.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 1.000, 0.000
flaps-position.4= 1.000, 0.000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0