[fltsim.0]
title=C172 AI
sim=Cessna172SP
model=
panel=
sound=
texture=1
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=N729WM
ui_manufacturer=AI
ui_type="C172SP Skyhawk"
ui_variation="White with blue"
atc_parking_codes=C172
atc_parking_types=RAMP
description="A stable"

[General]
atc_type=Cessna
atc_model=C172
editable=0
performance="Maximum Speed\n126 kts            203 km\/hr\n\nCruise Speed\n124 kts            200 km\/hr\n\nEngine\nTextron Lycoming IO-360-L2A 180 bhp\n\nPropeller\nTwo-Bladed Macauley Fixed Pitch\n\nMaximum Range\n638 nm            734 mi          1181 km\n\nService Ceiling\n14,000 ft\t         4267 m\n\nFuel Capacity\n56 gal\t          212 L\t \n\nEmpty Weight\n1,665 lb\t          1,002 kg\n\nMaximum Gross Weight\n2,550 lb\t          1,157 kg\n\nLength\n27 ft, 2 in          8.2 m\n\nWingspan\n36 ft, 1 in\t           11 m\n\nHeight\n8 ft, 11 in\t           2.72 m\n\nSeating\t           4\n\nUseful Load\n893 lb\t           405 kg\n"
Category=airplane


[WEIGHT_AND_BALANCE]
max_gross_weight = 2550                         // (pounds)
empty_weight = 1650                             // (pounds)

reference_datum_position     =  3.6, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -3.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = "170, -3.0, -1.5, 0.0, Pilot"                    // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -3.0,  1.5, 0.0, Front Passenger"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =   "0, -6.2, -1.5, 0.0, Rear Passenger"           // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =   "0, -6.2,  1.5, 0.0, Rear Passenger"           // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =   "0, -8.0,  0.0, 0.0, Baggage"                  // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 1400.0
empty_weight_roll_MOI   = 1137.0
empty_weight_yaw_MOI    = 2360.0
empty_weight_coupled_MOI= 0.0


[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

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.4, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.88                          //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 90.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 180                               //Max rated HP
fuel_metering_type= 0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0                                //Max design manifold pressure, (inHg)
min_design_mp= 0                                //Min design manifold pressure, (inHg)
critical_altitude= 0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.3                         //Propeller Diameter, (feet)
propeller_blades= 2                             //Number of propeller blades
propeller_moi= 5.0                              //Propeller moment of inertia
beta_max= 0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0                                  //Miminum governed RPM
prop_tc= 0                                      //Prop time-constant
gear_reduction_ratio= 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta= 20                            //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80                      //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 0                          //Minimum RPM for prop feathering
beta_feather= 0                                 //Feathering pitch angle (degrees)
power_absorbed_cf= 0                            //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0                         //Minimum pitch angle in reverse, (degrees)

[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
        //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
[contact_points]
point.0 = 1,  0.90,  0.00, -4.09, 1500, 0, 0.5, 22.0, 0.25,2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, -4.70, -4.50, -4.01, 3500, 1, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -4.70,  4.50, -4.01, 3500, 2, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -3.90, -18.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -3.90   18.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5=  2,-20.23,   0.0,  0.30, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6=  2,  1.48,   0.0, -2.17, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7=  2,-22.80,   0.0,  5.83, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.8=  2, -4.90,   0.0, -2.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8

max_number_of_points = 21

static_pitch=3.02                //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=3.765           //feet, altitude of CG when at rest on the ground

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68  //Brake scalar

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint= -3.95, -0.85, 2.1         //(feet) longitudinal, lateral, vertical distance from reference datum

[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        
light.0 = 3,  -2.88, -18.11, 2.95, fx_navred
light.1 = 3,  -2.88,  18.11, 2.95, fx_navgre
light.2 = 2,  -3.15, -18.31, 2.95, fx_strobe
light.3 = 2,  -3.15,  18.31, 2.95, fx_strobe
light.4 = 1, -20.60,   0.00, 6.33, fx_beacon
light.5 = 4,  -2.27,   0.00, 1.45, fx_vclight
               
[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 = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[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=1,0

[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=1,1    //Turn AND Bank

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

[fuel]
LeftMain  = -3.9, -2.1, 2.5, 26.5, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.9,  2.1, 2.5, 26.5, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1

[airplane_geometry]
wing_area               = 174.0                 //Square feet
wing_span               = 36.1                  //Feet
wing_root_chord         = 4.9                   //Feet
wing_dihedral           = 1.7                   //Degrees
wing_incidence          = 1.5                   //Degrees
wing_twist              = -3.0                  //Degrees
oswald_efficiency_factor= 0.68                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0                     //Degrees, wing leading edge
wing_pos_apex_lon       = -2.4                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 39.0                  //Square feet
htail_span              = 11.7                  //Feet
htail_pos_lon           = -18.3                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 3.2                   //Degrees
htail_sweep             = 10.0                  //Degrees, horizontal tail leading edge
vtail_area              = 18.0                  //Square feet
vtail_span              = 4.8                   //Feet, tip to body
vtail_sweep             = 40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -16.2                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.5                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 16.6                  //Square feet
aileron_area            = 18.3                  //Square feet
rudder_area             = 6.7                   //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 21.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 15.0                  //Degrees
rudder_limit            = 24.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000


[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 7                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 12.7                                 // degrees
flaps-position.2 = 25.3                                 // degrees
flaps-position.3 = 38                                   // degrees
damaging-speed   = 120                                  // KIAS
blowout-speed    = 150                                  // KIAS
lift_scalar = 1.0                                       
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None


[Reference Speeds]
flaps_up_stall_speed    = 53.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 48.0                  //Knots True (KTAS)
cruise_speed            = 115.0                 //Knots True (KTAS)
max_indicated_speed     = 163                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
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=9.00
nav_integrator_control=0.25
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 = 0.0


[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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=1
stick_shaker=0

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0