[fltsim.0]
title=X04U-1 Corsair Floatplane
sim=X04U-1 Corsair Floatplane
model=
panel=
sound=
texture=
kb_checklists=
atc_id=
atc_airline=
atc_flight_number=
ui_manufacturer=Chance Vought
ui_type=X04U-1 Corsair Floatplane
ui_variation=X04U-1 Corsair Floatplane
description=Navy Observation Airplane. Only one X04U was built with the US Navy as its intended buyer. First flight was in 1931 and it was the first aircraft with a monocoque fuselage, metel and fabric covered metel wing structure. It could be either a land or seaplane. The prototype crashed before prodection started.
[General]
atc_type=
atc_model=
editable=1
performance="Maximum Speed : 170 mph. 148 kts.\nEngine : 640-hp RR. Kestrel II S\nMaximum Range : 430 mi \nService Ceiling : 20,700 ft \nFuel Capacity : 21 gal ??? \nEmpty Weight : 3,067 lb \nMaximum Gross Weight : 4464 lb \nLength : 29 ft, 7 in \nWingspan : 37 ft, 2 in \nHeight : 10 ft, 5 in \nSeating : 2\nUseful Load : 460 lb ?? "
[WEIGHT_AND_BALANCE]
max_gross_weight =4464.0
empty_weight =3067.00000
reference_datum_position = 0, 0, 0 // (feet) from FSim Ref. position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -2.500, 0.000, 0.000
max_number_of_stations =2
// Weight (lbs), long, lat, vert. positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI =3353.14684
empty_weight_roll_MOI =2245.30642
empty_weight_yaw_MOI =4801.09661
empty_weight_coupled_MOI =0.00000
station_load.0= 165, -2.900, 0.000, 0.500, Pilot
station_load.1= 165, -5.000, 0.000, 0.000, Co-Pilot
[flight_tuning]
cruise_lift_scalar =1.00000
parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.00000
roll_stability =1.00000
yaw_stability =1.00000
elevator_trim_effectiveness =1.00000
aileron_trim_effectiveness =1.00000
rudder_trim_effectiveness =1.00000
p_factor_on_yaw =0.50000
hi_alpha_on_roll =1.00000
hi_alpha_on_yaw =1.00000
torque_on_roll =1.00000
gyro_precession_on_roll =1.00000
gyro_precession_on_yaw =1.00000
[GeneralEngineData]
engine_type =0
Engine.0 =8.000, 0.000, 0.600
fuel_flow_scalar =1.38000
min_throttle_limit = 0.0 // Minimum percent throttle.
starter_type = 1 // 1 = Manual starter
[piston_engine]
power_scalar =1.00000
cylinder_displacement =108.00000
compression_ratio =6.00000
number_of_cylinders =12
max_rated_rpm =2750.00000
max_rated_hp =640.00000
fuel_metering_type =1
cooling_type =1
normalized_starter_torque =0.07920
turbocharged =1
max_design_mp =42.00000
min_design_mp =1.00000
critical_altitude =13500.00000
emergency_boost_type=0
emergency_boost_mp_offset=0.00000
emergency_boost_gain_offset=0.00000
emergency_boost_duration=0.00000
fuel_air_auto_mixture =0
auto_ignition =0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00000
max_rpm_friction_scalar=1.00000
idle_rpm_friction_scalar=1.00000
[propeller]
thrust_scalar =1.00000
propeller_type =1
propeller_diameter =12.50000
propeller_blades =2
propeller_moi =12.00000
gear_reduction_ratio =1.75000
fixed_pitch_beta =21.00000
low_speed_theory_limit =80.00000
beta_max=22.00000
beta_min=20.00000
min_gov_rpm=0.00000
prop_tc=0.00000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.00000
beta_feather=0.00000
power_absorbed_cf=0.00000
prop_reverse_available=0
minimum_on_ground_beta=0.00000
minimum_reverse_beta=0.00000
defeathering_accumulators_available=0
[airplane_geometry]
wing_area =444.00000
wing_span =37.00000
wing_root_chord =5.58000
wing_dihedral =3.50000
wing_incidence =0.00000
wing_twist =0.00000
oswald_efficiency_factor =0.60000
wing_winglets_flag =0
wing_sweep =1.00000
wing_pos_apex_lon =1.37082
wing_pos_apex_vert =0.85000
htail_area =28.45000
htail_span =12.07000
htail_pos_lon =-17.44000
htail_pos_vert =0.60000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =4.75000
vtail_span =2.13000
vtail_sweep =0.00000
vtail_pos_lon =-17.44000
vtail_pos_vert =0.91000
elevator_area =28.56000
aileron_area =39.74000
rudder_area =10.76000
elevator_up_limit =30.00000
elevator_down_limit =20.00000
aileron_up_limit =20.00000
aileron_down_limit =15.00000
rudder_limit =25.00000
elevator_trim_limit =19.50000
spoiler_limit =0.01000
spoilerons_available =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
[Reference Speeds]
flaps_up_stall_speed =47.96749
full_flaps_stall_speed =47.96749
cruise_speed =96.02187
max_indicated_speed =166.00000
max_mach=1.00000
[contact_points]
;Slew position.
static_pitch = 16.000
static_cg_height = 7.500
gear_system_type =4
max_number_of_points=13
tailwheel_lock=0
point.0= 4, -9.758, -0.582, -9.373, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 2
point.1= 4, -9.747, 0.697, -9.373, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 2
point.2= 4, 7.042, -1.809, -7.616, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 2
point.3= 4, 7.042, 1.997, -7.616, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 3
point.4= 4, -1.089, 14.144, -5.826, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 3
point.5= 4, -5.954, 14.144, -5.957, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 3
point.6= 4, -5.594, -14.068, -6.022, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 3
point.7= 4, -1.350, 14.068, -5.859, 1600, 0, 0.000, 0.000, 0.900, 2.500, 0.600, 0.000, 0.000, 3
point.8= 2, 9.100, 0.000, 0.000, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.9= 2, -20.600, 0.000, 1.100, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.10= 2, -18.800, 0.000, 4.400, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.11= 2, -2.500, -15.700, -1.600, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.12= 2, -2.500, 15.700, -1.600, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
[brakes]
parking_brake = 0 // Parking brake available
toe_brakes_scale =0.00000
differential_braking_scale = 0.0
[flaps.0] //Outboard Leading Edge Slat -{315}- -{320}- -{524}- -{1101}-
type = 2 // 2= L.E.
span-outboard = 0.33 // % as decimal.
extending-time = 0.3 // Dummy automatic.
damaging-speed = 200.0
blowout-speed = 220.0
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 1
system_type = 4 // None ( of the pre-defined.)
flaps-position.0 = 0.0
flaps-position.1 = 40.0 // 0.70 rad
//[TailHook]
//tailhook_length =0.0
//tailhook_position =0.0
//cable_force_adjust =0.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage
; BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage =26
generator_alternator_voltage =28.5
max_generator_alternator_amps= 60
light_panel = 0, 1, 6
light_landing = 0, 5, 17.0 // Dummy flares.
[Views]
eyepoint= -3.0, 0.0, 2.5 // (feet) long, lat, vert. distance from reference datum.
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -0.321, -15.543, 3.275, fx_navred
light.1 = 3, -0.289, 15.536, 3.055, fx_navgre
light.2 = 2, -18.344, -0.015, 0.199, fx_strobe
light.3 = 4, -4.62, 0, 1.5, fx_vclight
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[fuel]
Center1 = 1.000, 0.000, 1.100, 72.000, 0.000
Center2 = 0.000, 0.000, 3.000, 48.000, 0.000
fuel_type =1
number_of_tank_selectors =1
electric_pump=0
[Radios] // Only HF radio was fitted; this is the minimum to be able to use ATC in fs9.
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1 = 1
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 1
Marker.1 = 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[hydraulic_system]
normal_pressure =0.00000
[stall_warning]
type=0
[direction_indicators]
//1 Type: 0=None
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=0,0
[attitude_indicators]
//Type: 1=Vacuum Gyro
attitude_indicator.0 = 0
[turn_indicators]
//Type: 2= Vacuum Gyro
turn_indicator.0=2,2 // Turn AND Bank
[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
default_vertical_speed=1000.00000
autothrottle_takeoff_ga=1.00000
autothrottle_max_rpm=90.00000
pitch_takeoff_ga=8.00000
max_pitch=10.00000
max_pitch_acceleration=1.00000
max_pitch_velocity_lo_alt=2.00000
max_pitch_velocity_hi_alt=1.50000
max_pitch_velocity_lo_alt_breakpoint=20000.00000
max_pitch_velocity_hi_alt_breakpoint=28000.00000
max_bank=25.00000
max_bank_acceleration=1.80000
max_bank_velocity=3.00000
max_throttle_rate=0.10000
nav_proportional_control=9.00000
nav_integrator_control=0.25000
nav_derivative_control=0.00000
nav_integrator_boundary=2.50000
nav_derivative_boundary=0.00000
gs_proportional_control=9.52000
gs_integrator_control=0.26000
gs_derivative_control=0.00000
gs_integrator_boundary=0.70000
gs_derivative_boundary=0.00000
yaw_damper_gain=0.00000
[smokesystem]
smoke.0=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=22.50000
flap_limit_power=11.25000
[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
[AirWrench]
Aircraft_Length=27.75000
nose_position_lon=11.07000
Vmax_sl=153.40000
Vmax_ca=178.50000
V_rc=90.50000
Climb_Rate=2506.80000
Climb_Weight=4117.00000
Max_gforce=4.00000
Emergency_hp=640.00000
ActualIncidence=0.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=2
FlowCorrection=1.00000
Power_Correction=1.00000
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=228.53072
target_roll_rate=96.67494
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
Elevator_FF=130.00000
Aileron_FF=-150.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=191.02931
V_Zero_Control=382.05863
Spin_Stability=100.00000
Stall_Stability=100.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
spoiler_time=0.20000
afterburner_thrust=0.00000
mach_scale=1.00000
spoiler_type=1
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_type=1
flaps_cd_scalar=0.06029
flaps_cm_scalar=-0.06981
vfe_enabled=0
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=16.50000
oil_pressure=45.00000
oil_temperature=241.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=0
cfs1_flag=0
laminar_flow=0
fixed_wing_pos=0
AirWrenchVersion=1.01.31
