[fltsim.0]
title=Latécoère 300
sim=LAT300
model=
panel=
sound=
texture=
ui_manufacturer=
ui_type=
ui_variation=
description=The Latecoere 300 flew for the first time in 1931 and then \nhad to be rebuilt after sinking. It was flown again in 1932 as the \nCroix du Sud parasol-wing monoplane flying-boat with four 484.4kW \nHispano-Suiza 12NBr water-cooled engines in tandem pairs. \nOn 31 December 1933 it achieved an international record by covering  \ncovering 3,679km non-stop flight.\n

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
empty_weight=22000			
empty_weight_roll_MOI=670000
empty_weight_pitch_MOI=120000
empty_weight_yaw_MOI=725000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 33000.000

[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

[piston_engine]
power_scalar=1.3
cylinder_displacement= 183.000
compression_ratio= 7.200
number_of_cylinders= 12
max_rated_rpm= 2700.000
max_rated_hp= 800.000
fuel_metering_type= 0
cooling_type= 1
normalized_starter_torque= 0.035
turbocharged= 0
max_design_mp= 47.690
min_design_mp= 1.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar= 1.000
idle_rpm_mechanical_efficiency_scalar= 1.000
max_rpm_friction_scalar= 1.000
idle_rpm_friction_scalar= 1.000

[propeller]
thrust_scalar=1.3
rotation=1,1,-1,-1		//Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW
propeller_type= 0
propeller_diameter= 12.583
propeller_blades= 3
propeller_moi= 52.300
beta_max= 49.000
beta_min= 18.000
min_gov_rpm= 1400.000
prop_tc= 0.010
gear_reduction_ratio= 1.780
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 79.300
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[Flaps.0] 
type=1 
span-outboard=0.3 
extending-time=7.0 
flaps-position.0=0,0 
flaps-position.1=15
flaps-position.2=20 
flaps-position.3=30 
flaps-position.4=45 
lift_scalar=0.9 
drag_scalar=0.1
pitch_scalar=0.5

[contact_points]
//0  Class
//1  Longitudinal Position        
//2  Lateral Position          
//3  Vertical Position        
//4  Impact Damage Threshold     
//5  Brake Map 		        
//6  Wheel Radius	       
//7  Steer Angle		      
//8  Static Compression           
//9  Max/Static Compression Ratio
//10 Damping Ratio	         
//11 Extension Time	         
//12 Retraction Time	         
//13 Sound Type
//14 Airspeed limit for retraction 
//15 Airspeed that gear gets damage 

/      0     1      2      3        4     5    6      7     8     9     10    11   12   13   14   15
point.0=4, 20.00, 00.00,-10.20, 6000.50, 0.0, 0.00, 48.24, 1.27, 2.50, 0.29, 0.0, 0.0, 4.0, 0.0, 0.0
point.1=4, 10.00,-10.50,-10.10, 6000.50, 0.0, 0.00, 48.24, 1.27, 2.50, 0.29, 0.0, 0.0, 9.0, 0.0, 0.0
point.2=4, 10.00, 10.50,-10.10, 6000.50, 0.0, 0.00, 48.24, 1.27, 2.50, 0.29, 0.0, 0.0, 9.0, 0.0, 0.0
point.3=4,-20.75, 00.00,-10.00, 6000.50, 0.0, 0.00, 48.24, 1.27, 2.50, 0.29, 0.0, 0.0, 4.0, 0.0, 0.0
point.4=2, 30.00, 00.00, -0.77, 2200.00, 0.0, 0.00, 00.00, 0.00, 0.00, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0
point.5=2, 22.75, 00.00, -7.21, 2200.00, 0.0, 0.00, 00.00, 0.00, 0.00, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0
point.6=2,  0.00,-10.16, -7.44, 2200.00, 0.0, 0.00, 00.00, 0.00, 0.00, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0
point.7=2,  0.00, 10.16, -7.44, 2200.00, 0.0, 0.00, 00.00, 0.00, 0.00, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0

static_pitch=0.000000
static_cg_height=10.500

[autopilot]
autopilot_available=1
use_no_default_bank=1
use_no_default_pitch=1 
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=0.000000
pitch_takeoff_ga=8.000000
default_pitch_mode= 0
default_bank_mode= 0
max_pitch= 10.000
max_pitch_acceleration= 1.000
max_pitch_velocity_lo_alt= 2.000
max_pitch_velocity_hi_alt= 1.500
max_pitch_velocity_lo_alt_breakpoint= 20000.000
max_pitch_velocity_hi_alt_breakpoint= 28000.000
max_bank= 25.000
max_bank_acceleration= 1.800
max_bank_velocity= 3.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 0.000

[EFFECTS]

[direction_indicators]
direction_indicator.0=1,0

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[Reference Speeds]		
flaps_up_stall_speed=120
full_flaps_stall_speed=86
cruise_speed=220
max_indicated_speed= 259.000

[Views]
eyepoint=22.24, -2.115, 3.816

[exits]
number_of_exits=1
exit_rate.0=0.1

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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,  4.850, -78.500, 6.00, fx_navred ,
light.1=3,  4.850,  78.500, 6.00, fx_navgre ,
light.2=3, 15.600,  22.000, 4.000, fx_navwhi ,
light.3=3, 15.600, -22.000, 4.000, fx_navwhi ,
light.4=1,-70.000,  00.000, 20.500, fx_beacon ,

[fuel]
Center1= 0.000, 0.000, 0.600, 250.000, 0.000
LeftMain= -2.300, -4.000, 0.140, 500.000, 0.000
LeftAux= 0.000, -4.000, -1.000, 200.000, 0.000
RightMain= -2.300, 4.000, 0.140, 500.000, 0.000
RightAux= 0.000, 4.000, -1.000, 200.000, 0.000
fuel_type= 1.000
number_of_tank_selectors= 1
electric_pump= 0

[airplane_geometry]
wing_area= 2799.000
wing_span= 145.000
wing_root_chord= 14.750
wing_dihedral= 0.000
wing_incidence= 1.500
wing_twist= 0.000
oswald_efficiency_factor= 0.579
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 500.000
htail_span= 29.167
htail_pos_lon= -40.000
htail_pos_vert= 0.000
htail_incidence= 1.500
htail_sweep= 0.000
vtail_area= 300.000
vtail_span= 19.748
vtail_sweep= 0.000
vtail_pos_lon= -40.000
vtail_pos_vert= 21.250
elevator_area= 94.410
aileron_area= 80.250
rudder_area= 39.490
elevator_up_limit= 28.000
elevator_down_limit= 22.999
aileron_up_limit= 26.001
aileron_down_limit= 18.999
rudder_limit= 28.000
elevator_trim_limit= 19.996
spoiler_limit= 39.248
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[brakes]
toe_brakes_scale= 0.488
parking_brake= 1

[GeneralEngineData]
engine_type= 0
Engine.0= -1.667, 8.333, 9.167
Engine.1= -1.667, 8.333, 9.167
Engine.2= -1.667, 8.333, 8.083
Engine.3= -1.667, 8.333, 8.083
fuel_flow_scalar= 1.000
min_throttle_limit= 0.000

[General]
performance=CREW 4 \nENGINE 4 x HS 12 Ydrs 2, 685kW \nWEIGHT \nTake-off weight 23000 kg 50707 lb \nEmpty weight 11300 kg 24912 lb \nDIMENSIONS \nwingspan 44.2 m 145 ft 0 in \nLength 25.8 m 84 ft 8 in \nHeight 25.8 m 84 ft 8 in \nWing area 260.0 m2 2798.61 sq ft \nPERFORMANCE \nMax. speed 210 km\/h 130 mph \nCruise speed 160 km\/h 99 mph \nCeiling 4600 m 15100 ft \nRange w\/max.fuel 4800 km 2983 miles \n

[hydraulic_system]
electric_pumps= 0
engine_map= 1,  1,  1,  1
normal_pressure= 6.931

[stall_warning]
type= 0

[attitude_indicators]
attitude_indicator.0= 1

[turn_indicators]
turn_indicator.0= 1,  0
