[fltsim.0]
title=Aeronca LC
sim=AeronLC
model=
panel=
sound=
texture=
atc_id=NC15282
ui_manufacturer=Aeronca Aircraft Company
ui_type=Aeronca LC
ui_variation=Aeronca LC
kb_checklists=Checklist
description=The Aeronca LC coupe low wing airplane featured a roomy cabin for two and excellent performance with a low cost from the factory at $3275. It was a superb form of transportation that could get you there fast with a top speed of 128 Knots. The landing gear featured large tires for smooth field landings and modern looking aerodynamic wheel skirts that made the LC model Aeronca stand out from all the other competition. This was a good rugged little plane that could get you there stylishly and yet affordably. Power was supplied by the Warner Scarab Jr. 5 cylinder radial engine with a Sinsinich wooden prop with brass lined blades. By William Ortis, Lionheart Creations Ltd. July 2004.
[fltsim.1]
title=Aeronca LC Yellow
sim=AeronLC
model=
panel=
sound=
texture=1
atc_id=NC15282
ui_manufacturer=Aeronca Aircraft Company
ui_type=Aeronca LC Yellow
ui_variation=Aeronca LC Yellow
kb_checklists=Checklist
description=The Aeronca LC coupe low wing airplane featured a roomy cabin for two and excellent performance with a low cost from the factory at $3275. It was a superb form of transportation that could get you there fast with a top speed of 128 Knots. The landing gear featured large tires for smooth field landings and modern looking aerodynamic wheel skirts that made the LC model Aeronca stand out from all the other competition. This was a good rugged little plane that could get you there stylishly and yet affordably. Power was supplied by the Warner Scarab Jr. 5 cylinder radial engine with a Sinsinich wooden prop with brass lined blades. By William Ortis, Lionheart Creations Ltd. July 2004.
[fltsim.2]
title=Aeronca LC Blue
sim=AeronLC
model=
panel=
sound=
texture=2
atc_id=NC 15282
ui_manufacturer=Aeronca Aircraft Company
ui_type=Aeronca LC Blue
ui_variation=Aeronca LC Blue
kb_checklists=Checklist
description=The Aeronca LC coupe low wing airplane featured a roomy cabin for two and excellent performance with a low cost from the factory at $3275. It was a superb form of transportation that could get you there fast with a top speed of 128 Knots. The landing gear featured large tires for smooth field landings and modern looking aerodynamic wheel skirts that made the LC model Aeronca stand out from all the other competition. This was a good rugged little plane that could get you there stylishly and yet affordably. Power was supplied by the Warner Scarab Jr. 5 cylinder radial engine with a Sinsinich wooden prop with brass lined blades. By William Ortis, Lionheart Creations Ltd. July 2004.
[fltsim.3]
title=Aeronca LC White
sim=AeronLC
model=
panel=
sound=
texture=3
atc_id=N17459
ui_manufacturer=Aeronca Aircraft Company
ui_type=Aeronca LC White
ui_variation=Aeronca LC White
kb_checklists=Checklist
description=The Aeronca LC coupe low wing airplane featured a roomy cabin for two and excellent performance with a low cost from the factory at $3275. It was a superb form of transportation that could get you there fast with a top speed of 128 Knots. The landing gear featured large tires for smooth field landings and modern looking aerodynamic wheel skirts that made the LC model Aeronca stand out from all the other competition. This was a good rugged little plane that could get you there stylishly and yet affordably. Power was supplied by the Warner Scarab Jr. 5 cylinder radial engine with a Sinsinich wooden prop with brass lined blades. By William Ortis, Lionheart Creations Ltd. July 2004.
[General]
performance=Engine Warner Scarab Jr. 5 Cyl. rated at 90 HP\nLength 22' 7" Height 7' Wingspan 36 ft. 4in"\n Gross Weight 1,680 lbs Empty Weight 1,034 lbs. Useful Load 849 lbs.\nPayload w/28 gal. Fuel 609 lbs.\nMaximum Speed 128 mph\nCruise Speed (sl.) 108 mph\nLanding Speed (with optional flaps) 49 mph\nService Ceiling 16,000 ft.\nFuel Capacity 28 gal.\nCruising Range 520 miles\nBy William Ortis, Lionheart Creations Ltd. July 2004
[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
[WEIGHT_AND_BALANCE]
empty_weight = 1680 // (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, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 11059.0
empty_weight_roll_MOI = 7243.0
empty_weight_yaw_MOI = 14484.0
empty_weight_coupled_MOI= 0.0
max_gross_weight=2775.000000
[flight_tuning]
cruise_lift_scalar = 1.6
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.2
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 2.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 2.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[piston_engine]
power_scalar = 0.40
cylinder_displacement=155.560000
compression_ratio=6.700000
number_of_cylinders=18
max_rated_rpm=2700.000000
max_rated_hp=2000.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=52.999999
min_design_mp=1.000000
critical_altitude=21500.000000
emergency_boost_type=1
emergency_boost_mp_offset=10.000000
emergency_boost_gain_offset=0.660000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
thrust_scalar = 0.60
propeller_type=0
propeller_diameter=13.330000
propeller_blades=3
propeller_moi=62.170000
beta_max=65.000000
beta_min=13.000000
min_gov_rpm=1800.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0= 1, -12.00, 0.00, -1.08, 3200.0, 0, 0.50,180.0, 0.25, 2.5, 0.90, 1.0, 4.00, 0, 0, 200 //tail wheel
point.1= 1, 1.80, -3.33, -4.00, 2200.0, 1, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 2, 0, 200 //left wheel
point.2= 1, 1.80, 3.33, -4.00, 2200.0, 2, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 3, 0, 200 //right wheel
point.3= 2, 0.00, -20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 //left wing
point.4= 2, 0.00, 20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 //Right wing
point.5= 2, -12.25, 0.00, 2.66, 2400.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 9 //tail
point.6= 2, 5.41, 0.00, -0.50, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 4 //belly
point.7= 2, 0.00, -5.43, -0.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 //left gull
point.8= 2, 0.00, 5.43, -0.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 //right gull
static_cg_height = 3.50 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch = 11.9 //degrees (pitch when loaded on ground)
gear_system_type=1
[Views]
eyepoint= -0.299262, -0.733026, 1.60 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.125 // 0.0 .. 1.0
extending-time=5 // seconds
flaps-position.0=0 // degrees, KIAS
flaps-position.1=16 // degrees, KIAS
flaps-position.2=32 // degrees, KIAS
flaps-position.3=48 // degrees, KIAS
damaging-speed=120 // KIAS
blowout-speed=140 // KIAS
[LSO]
LSOAdjustSpeed=1.2
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 1.22, -14.30, 0.10, fx_navred ,
light.1 = 3, 1.22, 14.30, 0.10, fx_navgre ,
light.2 = 4, -0.00, 0.00, 0.80, fx_vclight ,
light.3 = 3, -14.40, 0.05, 5.20,fx_navwhi
panel=0.00, 0.45, -2.00, fx_vclight
[fuel]
LeftMain=-0.970000,-12.250000,-1.610000,14.000000,0.000000
RightMain=-0.970000,12.250000,-1.610000,14.000000,0.000000
External1=1.940000,0.000000,-3.870000,175.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=314.000000
wing_span=41.000000
wing_root_chord=7.833333
wing_dihedral=13.595581
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.699202
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[GeneralEngineData]
engine_type=0
Engine.0=7.000000,0.000000,0.000000
fuel_flow_scalar=1.800000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=60.000000
full_flaps_stall_speed=44.000000
cruise_speed=106.521138
max_indicated_speed=128.500000
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
