[fltsim.0]
title=Latecoere 631
sim=Late 631
model=
panel=
sound=
texture=
panel=
sound=
kb_checklists=
kb_reference=
atc_id=L631
ui_manufacturer=Latecoere
ui_type=Late 631
ui_variation=Flying Boat
description=The prototype Late 631 flew for the first time on 4 November 1942. It was a graceful high-wing monoplane flying-boat powered by six 1,950 hp radial engines. Accommodation was provided for 46 passengers in two- or four-berth cabins. However this aircraft was confiscated by the Germans during the occupation of France.
[General]
performance= ENGINE\t6 x Wright Cycl. GR 2600-A5B, 1,950 hp\n WEIGHTS\n Take-off weight\t71350 kg\t157301 lb\n Empty weight\t32332 kg\t71280 lb\n DIMENSIONS\n Wingspan\t57.4 m\t188 ft 4 in\n Length\t43.5 m\t143 ft 9 in\n Wing area\t350.0 m2\t3767.37 sq ft\n PERFORMANCE\n Max. speed\t405 km\/h\t252 mph\n Cruise speed\t320 km\/h\t199 mph\n Range w\/max.fuel\t6000 km\t3728 miles\n \n GMAX by A.F.Scrub November 2010\n \n \n \n \n
station_load.0 =0.000000,0.000000,0.000000,0.000000
station_load.1 = 0, 0, 0, 0
station_load.2 = 0, 0, 0, 0
station_load.3 = 0, 0, 0, 0
station_load.4 = 0, 0, 0, 0
performance= \n \n \n \n \n \n
Category=airplane
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, 12.85, -90.73, 12.83, fx_navredh ,
light.1 = 3, 12.85, 90.73, 12.83, fx_navgreh ,
light.2 = 3, -66.21, 0.00, 6.40, fx_navwhth ,
light.3 = 2, -63.53, -21.73, 20.50, fx_strobeh ,
light.4 = 2, -63.53, 21.73, 20.50, fx_strobeh ,
light.5 = 1, -71.00, 0.00, 3.90, fx_beaconh ,
[Views]
eyepoint= 37.33, 0.00, 4.50 //Longitudinal, Lateral, Vertical (feet)
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.000
min_throttle_limit = -0.250000
engine.0 = 14.000, 13.700, 7.400
engine.1 = 14.000, -13.700, 7.400
engine.2 = 12.000, 28.200, 9.200
engine.3 = 12.000, -28.200, 9.200
engine.4 = 10.000, -42.200, 11.200
engine.5 = 10.000, 42.200, 11.200
[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup = fx_engstrt_jenny
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
LeftMain = 0.000, -12.000, 0.000, 1760.000, 0.000
RightMain = 0.000, 12.000, 0.000, 1760.000, 0.000
//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
[contact_points]
//gear
point.0=1, 39.0, 0.0, -7.0, 2500, 0.0, 2.5, 52.0, 0.5, 2.5, 0.5, 5.0, 5.0, 0.0, 0.0, 0.0
point.1=1,2.0, -41.0, -7.0, 2500, 1.0, 2.5, 0.0, 0.5, 2.5, 0.5, 7.5, 7.5, 3.0, 0.0, 0.0
point.2=1,2.0, 41.0, -7.0, 2500, 2.0, 2.5, 0.0, 0.5, 2.5, 0.5, 7.5, 7.5, 3.0, 0.0, 0.0
//floats
point.3 = 4, 30.724, 0, -7, 3500, 0, 0, 65, 0.25, 2.5, 0.9, 0, 0, 0, 0, 0
point.4 = 4, -8, 3, -7, 5000, 0, 0, 0, 0.5, 2.5, 0.9, 0, 0, 0, 0, 0
point.5 = 4, -8, -3, -7, 5000, 0, 0, 0, 0.5, 2.5, 0.9, 0, 0, 0, 0, 0
static_pitch=0.000
static_cg_height=7.0
gear_system_type=0
[keyboard_response]
elevator = 350.000000, 450.000000
aileron = 400.000000, 400.000000
rudder = 200.000000, 400.000000
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
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]
wing_area = 2867.000
wing_span = 152.000
wing_root_chord = 30.000
wing_dihedral = 2.000
wing_incidence = 2.000
wing_twist = 0.000
oswald_efficiency_factor = 0.800
wing_winglets_flag = 0
wing_sweep = 8.000
wing_pos_apex_lon = 6.000
wing_pos_apex_vert = 4.000
htail_area = 594.000
htail_span = 45.450
htail_pos_lon = -47.220
htail_pos_vert = 9.000
htail_incidence = 0.000
htail_sweep = 22.000
vtail_area = 375.000
vtail_span = 17.000
vtail_sweep = 45.000
vtail_pos_lon = -48.840
vtail_pos_vert = 8.430
elevator_area = 153.000
aileron_area = 163.000
rudder_area = 142.000
elevator_up_limit = 18.000
elevator_down_limit = 15.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1,1
electric_always_available = 0
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=5.500
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=2.00 //1.750 //1.500
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.0
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[piston_engine]
power_scalar=1.100
cylinder_displacement= 180.000
compression_ratio= 6.700
number_of_cylinders= 14
max_rated_rpm= 3000.000
max_rated_hp= 1950.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 47.000
min_design_mp= 10.000
critical_altitude= 5000
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
magneto_order_left_right_both = 1 //sets the order of the magneto switch direction
[propeller]
thrust_scalar=1.420
propeller_type= 0
propeller_diameter= 13.000
propeller_blades= 3
propeller_moi= 60.200
beta_max= 30.000
beta_min= 15.000
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.500
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 82.000
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
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[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=3,0
[Reference Speeds]
flaps_up_stall_speed= 100.000
full_flaps_stall_speed= 80.000
cruise_speed= 158.000
max_indicated_speed=259.000000
[autopilot]
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=31.512679
flap_limit_idle=31.512679
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Tailhook]
tailhook_length=1
tailhook_position=0.0, 0.0, 10.0
cable_force_adjust_1.0
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.13 ;Percent per second
[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=11442.000000
empty_weight_pitch_MOI = 1017509
empty_weight_roll_MOI = 1066725
empty_weight_yaw_MOI = 1786469
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 1
max_gross_weight=157301.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
