[fltsim.0]
title=AeroncaK United States
sim=AeroncaK 
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Aeronca
ui_type="Model K"
ui_variation="A: NC17481 U.S."
description="A two seat, high wing monoplane with strut bracing that replaced the cartoonish, pylon-braced C series after the 1937 flood. These airplanes were fully enclosed and were equipped with yoke control and side-by-side seating, advanced features in its' class. The K (straight K) still used the 2 cylinder boxer twin engine until recieving its' CofA with the modern, opposed 4 cylinder powerplants coming into vogue in the late '30s. The KC, KCA, KLA and others of the series led directly into the Aeronca Chief aircraft."


[fltsim.1]
title=AeroncaK Canada
sim=AeroncaK 
model=
panel=
sound=
texture=1
kb_checklists=
ui_manufacturer=Aeronca
ui_type="Model K"
ui_variation="B: CF-BJZ Canada"
description="A two seat, high wing monoplane with strut bracing that replaced the cartoonish, pylon-braced C series after the 1937 flood. These airplanes were fully enclosed and were equipped with yoke control and side-by-side seating, advanced features in its' class. The K (straight K) still used the 2 cylinder boxer twin engine until recieving its' CofA with the modern, opposed 4 cylinder powerplants coming into vogue in the late '30s. The KC, KCA, KLA and others of the series led directly into the Aeronca Chief aircraft."



[General]
atc_type=Aeronca
atc_model=K
editable=0
performance="Engine:\nAeronca E-113c 37-hp 2 cylinder, air cooled \nMaximum Speed:\n78-80 mph    60 kts	\nCruise Speed:\n70-72 mph   50 kts\nService Ceiling:\n11,500 ft,	3,505 m\nMaximum Range:\n175 mi @ 4 Gal/Hr  \nFuel Capacity:\n10 Gal U.S. 	\nEmpty Weight:\n590 lb	\nUseful Load:\n450 lb \nGross Weight:\n1,040 lb \nLength:\n21 ft 	\nWingspan:\n36 ft \nSeating:\n2"


[WEIGHT_AND_BALANCE]
max_gross_weight = 1220                         // (pounds)
empty_weight =  680                             // (pounds)

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

max_number_of_stations =50

station_load.0 = "170.0, -3.25, 0.00, 0.00, Pilot"       //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1 =   "0.0, -0.75, 0.00, 0.00, Passenger"   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =  "20.0, -4.40, 0.00, 0.00, Baggage"     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI   = 313.8
empty_weight_roll_MOI    = 313.9
empty_weight_yaw_MOI     = 642.2
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
p_factor_on_yaw          = 0.3
torque_on_roll           = 0.3
gyro_precession_on_yaw   = 0.3
gyro_precession_on_pitch = 0.3

[Flaps.0]
type= 0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 5.8, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //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= 42.75                    //Cubic inches per cylinder
compression_ratio= 7.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2300                             //Max rated RPM
max_rated_hp= 65                                //Max rated HP
fuel_metering_type= 1                           //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 = 0.89                             //Propeller thrust scalar
propeller_type= 1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.05                         //Propeller Diameter, (feet)
propeller_blades= 2                             //Number of propeller blades
propeller_moi= 3.78                             //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= 0.1                                    //Prop time-constant
gear_reduction_ratio= 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta= 13.75                            //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 in feather
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)


        //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,  -15.00,   0.0, -1.05, 1200, 0, 0.238,  30.0, 0.300, 2.5, 0.20, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1,    1.24,  -3.0, -5.00, 1600, 1, 0.728,   0.0, 0.54, 2.5, 0.65, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1,    1.24,   3.0, -5.00, 1600, 2, 0.728,   0.0, 0.54, 2.5, 0.65, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2,   -1.00, -17.7,  1.80,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,   -1.00,  17.7,  1.80,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2,  -14.40,   0.0,  4.50,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,    5.40,   0.0, -2.20,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch = 15.0
static_cg_height = 4.3

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.5  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = -1.684, -0.686, 1.241

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0 = 3,  -0.23, -17.93, 2.73, fx_navred
light.1 = 3,  -0.23,  17.93, 2.73, fx_navgre
light.5 = 4,  -2.27,   0.00, 1.45, fx_vclight

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 0
Com.1         = 1, 0
Nav.1         = 0, 0, 0
Adf.1         = 0
Transponder.1 = 0
Marker.1      = 0

[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 =200, 1000
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=0,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 0 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

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

[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 0

[fuel]
Center1 = 2.8, 0.0, 0.0, 10.0, 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=0

[airplane_geometry]
wing_area               = 178.5                 //Square feet
wing_span               = 35.2                  //Feet
wing_root_chord         = 5.25                  //Feet
wing_dihedral           = 1.1                   //Degrees
wing_incidence          = 2.5                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.6                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = 1.31                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 2.1                   //Feet, vertical distance from reference point, positive going up

htail_area              = 18.2                  //Square feet
htail_span              = 9.6                   //Feet
htail_pos_lon           = -13.4                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 1.3                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = -0.8                   //Degrees
htail_sweep             = 30.0                  //Degrees, horizontal tail leading edge

vtail_area              = 13.0                  //Square feet
vtail_span              = 4.44                  //Feet, tip to body
vtail_sweep             = 38.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -13.5                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.6                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 10.64                 //Square feet
aileron_area            = 9.6                   //Square feet
rudder_area             = 6.55                  //Square feet
elevator_up_limit       = 30.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 28.0                  //Degrees
elevator_trim_limit     = 10.0                   //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

[Reference Speeds]
flaps_up_stall_speed    = 33.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 33.0                  //Knots True (KTAS)
cruise_speed            = 63.0                  //Knots True (KTAS)
max_indicated_speed     = 106                   //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[stall_warning]
type=1