[fltsim.0]
title=Caudron C561
sim=Caudron C561
model=C561
panel=
sound=
texture=C561
kb_checklists=
ui_manufacturer=Caudron C561
ui_type=C561
description=The Caudron C561 was a racing plane of\n the 1930s.

[General]
atc_type=Caudron
atc_model=
editable=1
performance="Engine: Renault 456, 360 hp. Wingspan : 6,75 m. Length : 8,05 m. Heigth : 1,80 m. Empty weight 535 kg. Gross weight 911 kg. Max speed : 500 km/h. Crew : 1."
GMAX by A.F.Scrub

[pitot_static]
vertical_speed_time_constant = 2

[weight_and_balance]

// ACM V2.5
max_gross_weight = 4923
empty_weight = 3300
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.5, 0, 0
empty_weight_pitch_MOI = 6000
empty_weight_roll_MOI = 3000
empty_weight_yaw_MOI = 8000
empty_weight_coupled_MOI = 0
CG_forward_limit = 0
CG_aft_limit = 1
max_number_of_stations = 1

station_load.0 = 170, -6.63, 0, 0.25


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1
min_throttle_limit = 0
engine.0 = 6.92, 0, 0

[Radios] // availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 0
Com.2 = 0
Nav.1 = 0
Nav.2 = 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 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 = 1
Center1 = 0, 0, 0, 215, 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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[contact_points]
static_pitch = 12
static_cg_height = 3.5
tailwheel_lock = 1
gear_system_type = 1
max_number_of_points = 7

point.0 = 1, -11.85, 0, -1.10, 1600, 0, 0.62, 45, 0.25, 2.5, 0.7, 0, 0, 0, 0, 0
point.1 = 1, 2.95, -3.50, -4.45, 1800, 1, 0.9, 0, 0.3, 2.5, 0.7, 8, 8, 2.00,0.00,0.00
point.2 = 1, 2.95, 3.50, -4.45, 1800, 2, 0.9, 0, 0.3, 2.5, 0.7, 8, 8, 3.00,0.00,0.00
point.3 = 2, 0, -15.9, -0.457, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 5
point.4 = 2, 0, 15.9, -0.457, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 6
point.5 = 2, -17.5306, 0, -0.0326, 2400, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 9
point.6 = 2, 5.9643, 0, -1.81, 2400, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 4


[keyboard_response]
elevator = 350, 500
aileron = 450, 1000
rudder = 200, 1000


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0143,0.0143,0,2.4337,0.4810,0.4810,0.0577,2.4442,0.9909,0.9909
//ACM_AREAW2// 0.0865,2.3536,1.3998,1.3998,0.1444,2.2774,1.7654,1.7654,0.1732,2.2156
//ACM_AREAW3// 2.2609,2.2609,0.2166,2.1394,3.1465,3.1465,0.2599,1.9766,4.0897,4.0897
//ACM_AREAW4// 0.3754,1.8137,4.4987,4.4987,0.4043,1.6219,4.8354,4.8354,0.6353,1.1559
//ACM_AREAH1// 0,0,0,0.7372,0.1449,0.1449,0.0430,0.7294,0.2605,0.2605
//ACM_AREAH2// 0.0789,0.7292,0.3389,0.3389,0.1072,0.7289,0.4914,0.4914,0.1579,0.7358
//ACM_AREAH3// 0.6883,0.6883,0.2084,0.7429,0.9591,0.9591,0.2739,0.7279,1.1633,1.1633
//ACM_AREAH4// 0.3319,0.7128,1.5449,1.5449,0.4341,0.7197,1.6678,1.6678,0.5662,0.7121
//ACM_AREAV1// -0.0059,-0.0059,0.1182,1.3379,0.2301,0.2301,0.1300,1.3061,0.2414,0.2414
//ACM_AREAV2// 0.1242,0.6413,0.4774,0.4774,0.2011,0.6509,0.6543,0.6543,0.2779,0.6486
//ACM_AREAV3// 0.8195,0.8195,0.3312,0.6406,0.9963,0.9963,0.3844,0.6324,1.1733,1.1733
//ACM_AREAV4// 0.4435,0.6420,1.3207,1.3207,0.4909,0.6399,1.4975,1.4975,0.5559,0.6377
//ACM_CAREAW1// 2.6817,2.6817,1.5525,2.0390,3.0071,3.0071,1.5116,2.0100,3.1505,3.1505
//ACM_CAREAW2// 1.4933,1.9858,3.2804,3.2804,1.4797,1.9569,3.4558,3.4558,1.4615,1.9279
//ACM_CAREAW3// 3.6401,3.6401,1.4434,1.8946,3.8654,3.8654,1.4206,1.8566,4.0998,4.0998
//ACM_CAREAW4// 1.3933,1.8278,4.3116,4.3116,1.3707,1.7444,4.5096,4.5096,1.3525,1.6110
//ACM_CAREAH1// 0.2185,0.2185,0.7358,1.2151,0.2856,0.2856,0.7268,1.1885,0.3276,0.3276
//ACM_CAREAH2// 0.7330,1.1787,0.4404,0.4404,0.7240,1.1554,0.5835,0.5835,0.7228,1.1396
//ACM_CAREAH3// 0.7113,0.7113,0.7214,1.1086,0.9528,0.9528,0.7239,1.0587,1.1641,1.1641
//ACM_CAREAH4// 0.7188,1.0202,1.2888,1.2888,0.7257,0.9872,1.4745,1.4745,0.7285,0.9402
//ACM_CAREAV1// 0.2484,0.2484,0.6597,1.2932,0.3720,0.3720,0.6597,1.2950,0.4898,0.4898
//ACM_CAREAV2// 0.6539,1.2850,0.6312,0.6312,0.6480,1.2691,0.7609,0.7609,0.6480,1.2532
//ACM_CAREAV3// 0.8845,0.8845,0.6420,1.2079,1.0319,1.0319,0.6480,1.1742,1.1911,1.1911
//ACM_CAREAV4// 0.6420,1.1051,1.3797,1.3797,0.6360,1.0182,1.5448,1.5448,0.6360,0.8722
wing_area = 191
wing_span = 31.89
wing_root_chord = 7.69
wing_dihedral = 7
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 5
wing_pos_apex_lon = 2.24
wing_pos_apex_vert = -0.90
htail_area = 17
htail_span = 11.02
htail_pos_lon = -14.94
htail_pos_vert = 0.76
htail_incidence = 0
htail_sweep = 165
vtail_area = 7
vtail_span = 5.16
vtail_sweep = 20
vtail_pos_lon = -14.20
vtail_pos_vert = 1.01
elevator_area = 9.60
aileron_area = 15.8
rudder_area = 7.35
elevator_up_limit = 30
elevator_down_limit = 20
aileron_up_limit = 15
aileron_down_limit = 15
rudder_limit = 30
elevator_trim_limit = 18
spoiler_limit = 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 = 160
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1
parasite_drag_scalar=1
induced_drag_scalar=1
elevator_effectiveness=1
aileron_effectiveness=1
rudder_effectiveness=1
pitch_stability=1
roll_stability=1
yaw_stability=1
elevator_trim_effectiveness=1
aileron_trim_effectiveness=1
rudder_trim_effectiveness=1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 0.9
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1

[piston_engine]
power_scalar=1
cylinder_displacement=109.5
compression_ratio=6.50
number_of_cylinders=14
max_rated_rpm=2700
max_rated_hp=1000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.22
turbocharged=1
max_design_mp=52
min_design_mp=1
critical_altitude=5000
emergency_boost_type=0
emergency_boost_mp_offset=0
emergency_boost_gain_offset=0
fuel_air_auto_mixture=1
auto_ignition=0
emergency_boost_duration=0
max_rpm_mechanical_efficiency_scalar=1
idle_rpm_mechanical_efficiency_scalar=1
max_rpm_friction_scalar=1
idle_rpm_friction_scalar=1.5

[propeller]
thrust_scalar=1
propeller_type=0
propeller_diameter=10
propeller_blades=3
propeller_moi=40.4
beta_max=65
beta_min=15
min_gov_rpm=375
prop_tc=0.01
gear_reduction_ratio=1.25
fixed_pitch_beta=25
low_speed_theory_limit=80
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0
beta_feather=0
power_absorbed_cf=0
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0
minimum_reverse_beta=0
rotation = 1

[Views]
eyepoint=-4.90, 0.00, 1.4


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 0.43, -12.5, -2.3, fx_navred ,
light.1 = 3, 0.43, 12.5, -2.3, fx_navgre ,
light.2 = 4, -4.75, 0.00, -0.82, fx_vclight,


[flaps.0] //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 6
flaps-position.0 = 0
flaps-position.1 = 15, 169
flaps-position.2 = 25, 162
flaps-position.3 = 35, 155
flaps-position.4 = 45, 147
damaging-speed = 180
blowout-speed = 200
system_type = 0
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 1

[direction_indicators]
direction_indicator.0=1, 0

[Reference Speeds]
flaps_up_stall_speed=68.6
full_flaps_stall_speed=56.5
cruise_speed=148
max_indicated_speed = 350
max_mach = 0.6

[gear_warning_system]
gear_warning_available = 0 //1
pct_throttle_limit = 0.1
flap_limit_idle = 33.75
flap_limit_power = 16.875

[brakes]
toe_brakes_scale = 0.65
parking_brake = 1
differential_braking_scale = 1.0




[stall_warning] // 0 = None, 1 = Suction, 2 = Electric.
type = 0

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

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

[direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind
direction_indicator.0=1, 0

[airspeed_indicators]
airspeed_indicator.0 = 1, 0

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.944444

[autopilot]
autopilot_available=1
flight_director_available=1
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