//Fly Synthesis Texan Club 550 LSA
//FSX FD Ver 1.0, 8 Nov 2012

//Ref 1: Texan Club 550 LSA POH_TC_LSA Rev 0 03/12/09
//Ref 2: Jane's ATWA 2002-2003 ed.
//Ref 3: Rotax 912ULS specs from Zenith Aircraft Co (www.zenithair.com)
//Ref 4: Texan Club 550 LSA 3-view drawing
//Ref 5: Texan Club 550 Pilot Report

[fltsim.0]

title = Texan Club 550 LSA "WEFLY Team"
sim = Texan
model = 
panel = 
sound = 
texture = WF

visual_damage = 0

kb_checklists = Fly_Synthesis_Check
kb_reference = Fly_Synthesis_ref


atc_heavy = 0
atc_airline = 
atc_flight_number = 
atc_id_enable = 1
atc_id = I-8945
atc_id_color = 0x00000000
atc_id_font = Verdana,-11,1,600,0

ui_manufacturer = Fly Synthesis
ui_type = Texan Club 550 LSA
ui_variation = "WEFLY! Team"
ui_typerole = Light sport aircraft
ui_createdby = Massimo Taccoli

Description = The Fly Synthesis Texan Club 550 LSA is a low-wing light sport aircraft built of composite materials. It offers good visibility, excellent handling, and is a pleasure to fly. It's low speed capabilities make it an ideal aircraft for small airstrips.

[fltsim.1]

title = Texan Club 550 LSA "Standard colors"
sim = Texan
model = 
panel = 
sound = 
texture = STD

visual_damage = 0

kb_checklists = Fly_Synthesis_Check
kb_reference = Fly_Synthesis_ref


atc_heavy = 0
atc_airline = 
atc_flight_number = 
atc_id_enable = 1
atc_id = I-7963
atc_id_color = 0x00000000
atc_id_font = Verdana,-11,1,600,0

ui_manufacturer = Fly Synthesis
ui_type = Texan Club 550 LSA
ui_variation = "I-7963"
ui_typerole = Light sport aircraft
ui_createdby = Massimo Taccoli

Description = The Fly Synthesis Texan Club 550 LSA is a low-wing light sport aircraft built of composite materials. It offers good visibility, excellent handling, and is a pleasure to fly. It's low speed capabilities make it an ideal aircraft for small airstrips.


[fltsim.2]

title = Texan Club 550 LSA "I-A115"
sim = Texan
model = 
panel = 
sound = 
texture = A115

visual_damage = 0

kb_checklists = Fly_Synthesis_Check
kb_reference = Fly_Synthesis_ref

atc_heavy = 0
atc_airline = 
atc_flight_number = 
atc_id_enable = 1
atc_id = I-A115
atc_id_color = 0x00000000
atc_id_font = Verdana,-11,1,600,0

ui_manufacturer = Fly Synthesis
ui_type = Texan Club 550 LSA
ui_variation = "I-A115"
ui_typerole = Light sport aircraft
ui_createdby = Massimo Taccoli

Description = The Fly Synthesis Texan Club 550 LSA is a low-wing light sport aircraft built of composite materials. It offers good visibility, excellent handling, and is a pleasure to fly. It's low speed capabilities make it an ideal aircraft for small airstrips.

[General]

Performance = Length: 6.99 m.\nHeight: 2.40 m.\nWing Span: 8.60 m.\nWing Area: 11.80 sq m.\nEngine: Rotax 912 ULS 4-cyl.\nTakeoff Power: 98.6 hp at 5,800 RPM at sea level.Max Continuous Power: 92.5 hp at 5,500 RPM at sea level\nProp: 1.75 m 3-blade fixed pitch.\nEmpty Weight: 305 kg.\nMTO Weight: 550 kg.\nMax Speed (Vne): 129 kt.\nMax Cruise Speed: 94 kt.\nClean Stall Speed: 34 kt.\nStall (full flaps): 32 kt.\nInitial Climb Rate: 1,181 fpm at sea level.\nFuel consumption (cruise): 5.3 gph.

atc_type = Experimental
atc_model = Texan Club 550
editable = 0

Category = airplane

[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
hi_alpha_on_roll = 1.0
hi_alpha_on_yaw = 1.0
p_factor_on_yaw = 1.0
torque_on_roll = 0.3
gyro_precession_on_roll = 0.3
gyro_precession_on_yaw = 0.3

[Weight_And_Balance]

reference_datum_position = -0.31, 0.0, -1.45		//WRT Model Datum location
empty_weight_CG_position = 0.00, 0.0,  1.45		//On thrust line

CG_forward_limit = 0.03						//Ref 1
CG_aft_limit = -0.06						//Ref 1

empty_weight = 672.4						//Ref 1
max_gross_weight = 1212.5						//Ref 1

empty_weight_roll_MOI = 255.5					///MOIs calc as per Goodrick
empty_weight_pitch_MOI = 313.6
empty_weight_yaw_MOI = 527.1
empty_weight_coupled_MOI = 0.0

max_number_of_stations = 3

station_load.0 = 170.0, 0.0, -0.9, 1.45, L Seat		//Ref 4
station_load.1 = 170.0, 0.0,  0.9, 1.45, R Seat		//Ref 4
station_load.2 = 0.1, 0.0,  0.0, 1.45, Baggage		//Ref 4 (Max 16 kg)

[Fuel]

fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1

LeftMain = 0.0, -4.25, 0.4, 13.2, 0.5				//Ref 1
RightMain = 0.0,  4.25, 0.4, 13.2, 0.5				//Ref 1

[Contact_points]

static_pitch = -0.70
static_cg_height = 3.86

gear_system_type = 4
tailwheel_lock = 0

max_number_of_points = 7

point.0 = 1,   4.647,   0.00, -2.359, 1575, 0, 0.45, 30.0, 0.15, 2.50, 0.95, 0.0, 0.0, 0, 0.0, 0.0
point.1 = 1,  -0.638,  -2.79, -2.428, 1575, 1, 0.55,  0.0, 0.33, 1.25, 0.95, 0.0, 0.0, 2, 0.0, 0.0
point.2 = 1,  -0.638,   2.79, -2.428, 1575, 2, 0.55,  0.0, 0.33, 1.25, 0.95, 0.0, 0.0, 3, 0.0, 0.0
point.3 = 2,  -1.900, -14.05,  1.300, 1575, 0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 5, 0.0, 0.0
point.4 = 2,  -1.900,  14.05,  1.300, 1575, 0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 6, 0.0, 0.0
point.5 = 2, -15.400,   0.00,  0.920, 1575, 0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 9, 0.0, 0.0
point.6 = 2,   7.400,   0.00,  1.500, 1575, 0, 0.00,  0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 4, 0.0, 0.0

[Brakes]

parking_brake = 1
auto_brakes = 0
toe_brakes_scale = 0.5
differential_braking_scale = 1.0

[Views]

eyepoint = -1.0, -0.9, 2.8					//ACM

[Airplane_geometry]

wing_winglets_flag = 0
spoilerons_available = 0
spoiler_handle_available = 0
auto_spoiler_available = 0
wing_area = 127.013			//Ref 1
wing_span = 28.215			//Ref 1
wing_root_chord = 4.590			//Ref 1
wing_dihedral = 5.500			//Ref 4
wing_incidence = 1.000			//Ref
wing_twist = -1.000			//Ref
oswald_efficiency_factor = 0.870			//Perfect wing= 1.0
wing_sweep = 0.000			//Ref 4
wing_pos_apex_lon = 1.377			//Defined (30% MAC fwd of Datum)
wing_pos_apex_vert = 0.000			//Defined
htail_area = 20.989			//Ref 1
htail_span = 9.842			//Ref 1
htail_pos_lon = -13.420			//Ref 4
htail_pos_vert = 1.167			//Ref 4
htail_incidence = 0.000			//
htail_sweep = 0.000			//Ref 4
vtail_area = 12.378			//Ref 1
vtail_span = 4.000			//Ref 4
vtail_sweep = 37.600			//Ref 4
vtail_pos_lon = -10.500			//Ref 4
vtail_pos_vert = 1.667			//Ref 4
elevator_area = 20.989			//Ref 1
aileron_area = 12.443			//Ref 1
rudder_area = 6.458			//Ref 1
elevator_up_limit = 16.000			//Ref 1
elevator_down_limit = 11.000			//Ref 1
aileron_up_limit = 22.000			//Ref 1
aileron_down_limit = 17.000			//Ref 1
rudder_limit = 18.000			//Ref 1
elevator_trim_limit = 20.000
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
positive_g_limit_flaps_up = 3.800			//Ref 1
positive_g_limit_flaps_down = 2.000			//Ref 1
negative_g_limit_flaps_up = -1.900			//Ref 1
negative_g_limit_flaps_down = -1.500
load_safety_factor = 1.500			//Design G load safety factor

[Flaps.0]

type = 1
system_type = 0
span-outboard = 0.5
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
extending-time = 2.0
damaging-speed = 90.0
blowout-speed = 95.0

flaps-position.0 = 0.0					//Ref 1
flaps-position.1 = 15.0, 85.0				//Ref 1
flaps-position.2 = 30.0, 75.0				//Ref 1
flaps-position.3 = 45.0, 65.0				//Ref 1

[GeneralEngineData]

engine_type = 0
fuel_flow_scalar = 0.86					//Ref 5
min_throttle_limit = 0.05

engine.0 = 6.4, 0.0, 1.45					//Ref 4

[Piston_engine]

power_scalar = 1.0
max_rpm_mechanical_efficiency_scalar = 1.0
idle_rpm_mechanical_efficiency_scalar = 1.0
max_rpm_friction_scalar = 1.0
idle_rpm_friction_scalar = 1.0
fuel_metering_type = 1		//Ref 3
cooling_type = 0  		//Ref 3
turbocharged = 0
emergency_boost_type = 0
fuel_air_auto_mixture = 1
auto_ignition = 0
number_of_cylinders = 4		//Ref 3
cylinder_displacement = 20.65	//Ref 3
compression_ratio = 10.50	//Ref 3
max_rated_rpm = 5800.00	//Ref 3
max_rated_hp = 98.60	//Ref 3
normalized_starter_torque = 0.30
max_design_mp = 0.00
min_design_mp = 0.00
critical_altitude = 0.00
emergency_boost_mp_offset = 0.00
emergency_boost_gain_offset = 0.00

[Propeller]

thrust_scalar = 1.0
rotation = 1
propeller_type = 1
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available = 0
prop_auto_feathering_available = 0
defeathering_accumulators_available = 0
prop_reverse_available = 0
propeller_blades = 3
propeller_diameter = 5.74	//Ref 1
propeller_moi = 5.00
beta_max = 0.00
beta_min = 0.00
fixed_pitch_beta = 23.00
beta_feather = 0.00
minimum_on_ground_beta = 0.00
minimum_reverse_beta = 0.00
min_gov_rpm = 0.00
prop_tc = 0.10
gear_reduction_ratio = 2.43	//Ref 3
low_speed_theory_limit = 80.00
min_rpm_for_feather = 0.00
power_absorbed_cf = 0.00

[Electrical]

engine_generator_map = 1
electric_always_available = 0
max_battery_voltage = 12.0			//Ref 1
generator_alternator_voltage = 13.5			//Ref 1
max_generator_alternator_amps = 18.5			//Ref 3

additional_system = 0,  5.0, 10.0
autopilot = 0,  5.0, 10.0
avionics_bus = 0,  5.0, 10.0
avionics = 1,  2.0, 10.0
flap_motor = 0,  5.0, 10.0
fuel_pump = 0,  5.0, 10.0
light_nav = 0,  5.0, 10.0
light_beacon = 0,  2.0, 10.0
light_landing = 0,  2.0, 10.0
light_taxi = 0,  2.0, 10.0
light_strobe = 0,  2.0, 10.0
light_panel = 0,  2.0, 10.0
marker_beacon = 1,  2.0, 10.0
pitot_heat = 0,  2.0, 10.0
starter1 = 0, 20.0, 10.0

[Lights]

light.0 = 3,  -0.35, -13.85,  1.35, fx_navred
light.1 = 3,  -0.35,  13.85,  1.35, fx_navgre
light.2 = 3, -14.40,   0.00,  6.05, fx_navwhi
light.3 = 4,   0.68,   0.00,  2.00, fx_vclight

[Radios]

Audio.1 = 1
Com.1 = 1, 1
Com.2 = 0, 0
Nav.1 = 1, 1, 1
Nav.2 = 0, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1

[Hydraulic_system]

electric_pumps = 0
engine_map = 1,0,0,0
normal_pressure = 0.0

[Deice_system]

structural_deice_type = 0

[Pneumatic_system]

max_pressure = 0.0
bleed_air_scalar = 0.0

[Vacuum_system]

vacuum_type = 1
engine_map = 1,0,0,0
max_pressure = 5.15
electric_backup_pressure = 5.15

[Effects]

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

[Exits]

number_of_exits = 1
exit_rate.0 = 0.3

[Gear_warning_system]

gear_warning_available = 0
pct_throttle_limit = 0.0
flap_limit_power = 0.0
flap_limit_idle = 0.0

[Stall_warning]

type = 1
stick_shaker = 1

[Pitot_static]

vertical_speed_time_constant = 2.0			//Incr value causea a more instantaneous VSI reaction
pitot_heat = 1.0

[Airspeed_indicators]

airspeed_indicator.0 = 1,0

[Altimeters]

altimeter.0 = 1

[Attitude_indicators]

attitude_indicator.0 = 2

[Direction_indicators]

direction_indicator.0 = 2,0

[Turn_indicators]

turn_indicator.0 = 2,2

[Autopilot]

autopilot_available = 1
flight_director_available = 1
default_pitch_mode = 0
default_bank_mode = 0
autothrottle_available = 1
autothrottle_arming_required = 0
autothrottle_takeoff_ga = 1.0
autothrottle_max_rpm = 5600.0
max_throttle_rate = 0.1
default_vertical_speed = 700.0
pitch_takeoff_ga = 8.0
max_pitch = 10.0
max_pitch_acceleration = 1.0
max_pitch_velocity_lo_alt = 2.0
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000.0
max_pitch_velocity_hi_alt_breakpoint = 28000.0
max_bank = 25.0
max_bank_acceleration = 1.8
max_bank_velocity = 3.0
nav_proportional_control = 9.0
nav_integrator_control = 0.25
nav_derivative_control = 0.0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0.0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0.0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0.0
yaw_damper_gain = 0.0

[Forcefeedback]

stick_shaker_magnitude = 3000		//0 - 10000
stick_shaker_direction = 0		//0 - 35999 degrees
stick_shaker_period = 111111		//in microseconds
ground_bumps_magnitude1 = 3250		//0 - 10000
ground_bumps_angle1 = 8900		//0 - 35999 degrees
ground_bumps_intercept1 = 5.00
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 = 1.000
crash_magnitude1 = 10000		//0 - 10000
crash_direction1 = 1000		//0 - 35999 degrees
crash_magnitude2 = 10000		//0 - 10000
crash_direction2 = 9000		//0 - 35999 degrees
crash_period2 = 75000		//in microseconds
crash_duration2 = 2500000		//in microseconds

[Keyboard_response]

elevator = 150.0, 250.0
aileron = 150.0, 250.0
rudder = 150.0, 250.0

[Reference Speeds]

full_flaps_stall_speed = 32.0			//Ref 1
flaps_up_stall_speed = 34.0			//Ref 1
cruise_speed = 94.0			//Ref 1
max_indicated_speed = 129.0			//Ref 1

[CameraDefinition.0]

Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 8.0, 0.8, 0.0
InitialPbh = 5, 0, 280
XyzAdjust = TRUE
Category = Aircraft
ClipMode = Minimum

[CameraDefinition.1]

Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -8.0, 0.8, 0.0
InitialPbh = 5, 0, 80
XyzAdjust = TRUE
Category = Aircraft
ClipMode = Minimum

[CameraDefinition.2]

Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0.0, 1.0, -15.0
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum

[CameraDefinition.3]

Title = "Nose"
Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720}
Description = Looking back from the nose of the engine toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0.0, 0.8, 9.0
InitialPbh = 20, 0, 180
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = FALSE
ClipMode = Minimum

[CameraDefinition.001]

Title = "Right Seat"
Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .7
SmoothZoomTime = 2.0
ZoomPanScalar = 0.75
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare = FALSE
Category = Cockpit
PitchPanRate = 20
HeadingPanRate = 60
InitialXyz = 0.6, 0.0, 0.0
InitialPbh = 0, 0, 0