[fltsim.0]
title=Aeronca C-3
sim=Aeronca C-3
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=NC13881
atc_id_color=
ui_manufacturer=Aeronca
ui_type=C-3
ui_variation=
description=The Aeronca C-3 was one of the first affordable general aviation planes.
[General]
atc_type=Aeronca
atc_model=
editable=0
performance=Maximum Speed\82mph CruiseSpeed\70mph Range\200miles Gross Weight\877lbs Ceiling\12000 ft.
[WEIGHT_AND_BALANCE]
max_gross_weight = 877 // (pounds)
empty_weight = 466 // (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 =0.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI = 1346
empty_weight_roll_MOI = 948
empty_weight_yaw_MOI = 1967
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 = 2.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[Flaps.0]
type= 0
span-outboard= 0.5
extending-time= 0.0
system_type= 0
flaps-position.0= 0.0, 0.0
flaps-position.1= 0.0, 0.0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 4.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 50 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders=2 //Number of cylinders
max_rated_rpm= 2400 //Max rated RPM
max_rated_hp= 36 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
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= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 5.7 //Propeller moment of inertia
beta_max= 31.8 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //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)
//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, -12.4, 0.0, -0.8, 1181.1, 0, 0.519, 180.0, 0.304, 2.5, 0.695, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1, 1.4, -2.5, -3.8, 1574.8, 0, 0.519, 0.0, 0.304, 2.5, 0.686, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1, 1.4, 2.5, -3.8, 1574.8, 0, 0.519, 0.0, 0.304, 2.5, 0.682, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2, 0.0, -17.9, -2.1, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, 0.0, 17.9, -2.1, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -13.0, 0.0, 3.3, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 2.4, 0.0, -2.2, 787.4, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch = 12
static_cg_height = 3.1
[Views]
eyepoint = 0.0, 0.0, 1.0
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 0, 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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[electrical]
electric_always_available=1
[fuel]
LeftMain = 0.0, 0.0, 0.0, 20.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0, 0.0, 0.0, 20.0, 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
[airplane_geometry]
wing_area = 142 //Square feet
wing_span = 36 //Feet
wing_root_chord = 4.2 //Feet
wing_dihedral = 3.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.5 //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 = 1.2 //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 = 40.0 //Square feet
htail_span = 11.7 //Feet
htail_pos_lon = -12.3 //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 = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 18.0 //Square feet
vtail_span = 4.8 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -12.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 0.0 //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
[Reference Speeds]
flaps_up_stall_speed = 20.0 //Knots True (KTAS)
full_flaps_stall_speed = 20.0 //Knots True (KTAS)
cruise_speed = 70.0 //Knots True (KTAS)
[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
