[fltsim.0]
title=AerC-3
sim=AerC-3
model=
panel=
sound=
texture=
ui_manufacturer=Aeronca
kb_checklists=
prop_anim_ratio=1.76
description=The C-3 was one of the first affordable general aviation aircraft.
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[General]
atc_type=Aeronca
atc_model=
editable=0
performance=Span: 36'\nLength: 20'\nTop Speed:82 mph\nCruise Speed: 70mph\nRange:200 miles\nCeiling:12000 ft.\nGross Weight:877 lbs\nPower: 36 hp Aeronca 2 cylinder\nDesigner: Paul Clawson\nDate:10\/2005
[weight_and_balance]
// ACM V2.5
max_gross_weight = 877
empty_weight = 466
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 1346
empty_weight_roll_MOI = 948
empty_weight_yaw_MOI = 1967
empty_weight_coupled_MOI = 0
max_number_of_stations = 1
station_load.0 = 170, 0, 0, 0
station_load.1 = 170, 1, 0, 0
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.100000
engine.0 = 4.3, 0, 0.39,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 0
Center1 = 3, 0, 0.35, 8, 0
RightMain = 0, 0, 0, 0, 0
[contact_points]
static_pitch = 12.5
static_cg_height = 3.2
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7
point.0 = 3, -12.4, 0, -0.8, 1181.1, 0, 0.2, 22, 0.304, 2.5, 0.695, 0, 0, 0, 0, 0
point.1 = 1, 1.2656, -2.5, -3.8851, 1574.8, 0, 0.6, 0, 0.304, 2.5, 0.686, 0, 0, 2, 0, 0
point.2 = 1, 1.3997, 2.5, -3.9123, 1574.8, 0, 0.6, 0, 0.304, 2.5, 0.682, 0, 0, 3, 0, 0
point.3 = 2, 0, -17.9561, 1.7233, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0, 17.5052, 1.4982, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -15.0118, 0, 0.8506, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 3.8413, 0, -2.447, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 142
wing_span = 36
wing_root_chord = 4.2
wing_dihedral = 3.0
wing_incidence = 0.0
wing_twist = -1.0
oswald_efficiency_factor = 0.4
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon = 1.2
wing_pos_apex_vert = 0.0
htail_area = 40.0
htail_span = 11.7
htail_pos_lon = -12.3
htail_pos_vert = 0.0
htail_incidence = 0.0
htail_sweep = 0.0
vtail_area = 18.0
vtail_span = 4.8
vtail_sweep = 0.0
vtail_pos_lon = -12.3
vtail_pos_vert = 0.0
elevator_area = 16.6
aileron_area = 18.3
rudder_area = 6.7
elevator_up_limit = 28.0
elevator_down_limit = 21.0
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 24.0
elevator_trim_limit = 19.5
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 1
[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
[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
[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=1.3 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.7 //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 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=2.5 //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=16 //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
[Views]
eyepoint=-0.40, 0.0, 0.9
[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
[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
[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)
max_indicated_speed=180.000000
[autopilot]
autopilot_available=0
flight_director_available=0
[brakes]
toe_brakes_scale=0.400000
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
