[fltsim.0]
title=F4U-1A Corsair "Big Hog"
sim=F4U1A_Corsair
model=
panel=
sound=
texture=bighog
KB_checklists=f4u1a_corsair_check
kb_reference =
atc_id =
ui_manufacturer = Chance Vought
ui_type = F4U-1A
ui_variation = F4U-1A Big Hog
description= This is a model of the "Big Hog" F4U-1A of VF-17 flow by squadron C.O., Cdr. Tommy Blackburn, Late 1943.
[fltsim.1]
title=F4U-1A Corsair "Sundowner"
sim=F4U1A_Corsair
model=
panel=
sound=
texture=
KB_checklists=f4u1a_corsair_check
kb_reference =
atc_id =
ui_manufacturer = Chance Vought
ui_type = F4U-1A
ui_variation = F4U-1A Sundowners
description=This is a Corsair from the famous Pacific fleet squadron V111, wearing one of the most recognisable insignia.
[General]
performance=Weight: 8,892\/14,000 lbs\nEngine: Pratt & Whitney R-2800-8\nDouble Wasp 18-cyl. radial air-\ncooled, 2,000 hp\nMax speed: 417 mph @ 19,900 ft\nCeiling: 36,900 ft\nInitial climb rate: 2,890 ft\/min\nRange: 1,596 miles or\nwith drop tanks, 2,215 miles\nUpgraded to FS9\/FSX by A.F.Scrub\nJanuary 2009\n
Category=airplane
[smokesystem]
//smoke.0= 0.00, -12.6, -20.70, fx_WingtipVortex
//smoke.1= 0.00, -12.6, 20.70, fx_WingtipVortex
smoke.0= 0.00, -1.6, -1.70, Fx_contrail_l
smoke.1= 0.00, -1.6, 1.70, Fx_contrail_l
[LIGHTS]
//#1=beacon #2=strobe #3=nav #10=reheat
//#4=cockpit #5=landing #6=taxi
//#7=recog #8=wing #9=logo
//---------------originals----------------------------
light.0=5, 1.40, -19.50, -0.00, fx_navred
light.1=5, 1.50, 19.50, -0.00, fx_navgre
light.2=5, -5.66, 0.00, -2.00, fx_beacon
light.3=5, -23.20, 0.00, 1.30, fx_beacon
light.4=5, 2.50, -8.50, -3.00, fx_landing
//------------ ExhaustFlames--------uses wing/taxi/logo
//index,type, long, lat, vert, fx_filename
light.5=8, 4.10, -1.70, -1.90, fx_engstrt_jenny
light.6=8, 4.10, 1.70, -1.90, fx_engstrt_jenny
light.7=6, 4.10, -1.95, -1.80, fx_radialpower
light.8=6, 4.10, 1.95, -1.80, fx_radialpower
light.9=9, 4.00, -0.10, -1.20, fx_smokePort
light.10=9, 4.00, 0.10, -1.20, fx_smokeStar
//------------ Guns ----------------------uses strobe
light.11=2, 2.15, 9.50, -1.90, fx_Wing_Guns
light.12=2, 2.15, -9.50, -1.90, fx_Wing_Guns
light.13=2, 2.15, 8.50, -1.90, fx_Wing_Guns
light.14=2, 2.15, -8.50, -1.90, fx_Wing_Guns
[WEIGHT_AND_BALANCE]
empty_weight = 8873 // (pounds)
reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 11059.0
empty_weight_roll_MOI = 7243.0
empty_weight_yaw_MOI = 14484.0
empty_weight_coupled_MOI=0.000000
max_gross_weight=13564.500000
[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]
cylinder_displacement=155.560000
compression_ratio=6.700000
number_of_cylinders=18
max_rated_rpm=2700.000000
max_rated_hp=2000.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=52.999999
min_design_mp=1.000000
critical_altitude=21500.000000
emergency_boost_type=1
emergency_boost_mp_offset=18.000000
emergency_boost_gain_offset=0.800000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
thrust_scalar = 1.0
propeller_type=0
propeller_diameter=13.330000
propeller_blades=4
propeller_moi=62.170000
beta_max=65.000000
beta_min=13.000000
min_gov_rpm=1800.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[contact_points]
//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)
point.0= 1, -18.00, 0.00, -3.35, 3200.0, 0, 0.50,180.0, 0.25, 2.5, 0.90, 1.0, 4.00, 0, 0, 200 //tail wheel
point.1= 1, 1.80, -5.93, -7.65, 2200.0, 1, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 2, 0, 200 //left wheel
point.2= 1, 1.80, 5.93, -7.65, 2200.0, 2, 1.35, 0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 3, 0, 200 //right wheel
point.3= 2, 0.00, -20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 //left wing
point.4= 2, 0.00, 20.00, -1.25, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 //Right wing
point.5= 2, -20.25, 0.00, -1.66, 2400.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 9 //tail
point.6= 2, 5.41, 0.00, -3.50, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 4 //belly
point.7= 2, 0.00, -5.43, -3.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 //left gull
point.8= 2, 0.00, 5.43, -3.75, 1200.0, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 //right gull
static_cg_height = 6.60 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch = 11.9 //degrees (pitch when loaded on ground)
gear_system_type=1
[Views]
eyepoint= -6.2, 0.00, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.125 // 0.0 .. 1.0
extending-time=5 // seconds
flaps-position.0=0 // degrees, KIAS
flaps-position.1=16 // degrees, KIAS
flaps-position.2=32 // degrees, KIAS
flaps-position.3=48 // degrees, KIAS
flaps-position.4=64 // degrees, KIAS
flaps-position.5=80 // degrees, KIAS
damaging-speed=201 // KIAS
blowout-speed=305 // KIAS
[LSO]
LSOAdjustSpeed=1.2
[fuel]
Center1=-1.940000,0.000000,-0.500000,187.000000,0.000000
Center2=-1.940000,0.000000,-0.500000,50.000000,0.000000
LeftMain=-0.970000,-12.250000,-1.610000,62.000000,0.000000
RightMain=-0.970000,12.250000,-1.610000,62.000000,0.000000
External1=1.940000,0.000000,-3.870000,175.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=314.000000
wing_span=41.000000
wing_root_chord=7.833333
wing_dihedral=13.595581
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.699202
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=0
spoiler_extension_time=3.000000
positive_g_limit_flaps_up=10.000000
positive_g_limit_flaps_down=10.000000
negative_g_limit_flaps_up=-10.000000
negative_g_limit_flaps_down=-10.000000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[GeneralEngineData]
engine_type=0
Engine.0=7.000000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=65.000000
full_flaps_stall_speed=52.000000
cruise_speed=250.000000
max_indicated_speed=760.500000
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
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
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[stall_warning]
type=0
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
