[fltsim.0]
title=P47 Senta a Pua
sim=P47DT
model=
panel=
sound=
texture=1
kb_checklists=
description=FS2002\2004 P-47D Painted By Cristiano Magnani

ui_manufacturer=Republic
ui_type=1st Brazilian Fighter Squadron
ui_variation=P-47D
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=


[General]
atc_type=
atc_model=
performance=Engine: Pratt & Whitney R-2800-59\nHorsepower: 2000\/2430 in War Emergency setting\nPropeller: Curtis Electric C542S with 13' diameter\nSpan: 40' 9 5\/16''\nLength: 36' 1 3\/4''\nHeight: 14' 8 1\/16''\nWeight: 10,000 lbs empty, 17,500 lbs maximum\nSpeed: 426 mph @ 30,000feet\nCeiling: 42,000 feet\nRange: 1030 miles @ 10,000 feet\nArmament: Eight .50 calibre machine guns plus 2500 lbs ordnance\n

[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
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=1.0
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[WEIGHT_AND_BALANCE]
empty_weight=8873.000

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000

max_number_of_stations=50

station_load.0=170.000, -3.000, 0.000, 3.000

;Moments of Inertia
empty_weight_pitch_MOI=11059.000
empty_weight_roll_MOI=7243.000
empty_weight_yaw_MOI=14484.000
empty_weight_coupled_MOI=0.000
max_gross_weight=12259.000
CG_forward_limit=0.000
CG_aft_limit=1.000


[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=1.0
cylinder_displacement=155.560
compression_ratio=6.700
number_of_cylinders=18
max_rated_rpm=2700.000
max_rated_hp=2000.000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.035
turbocharged=1
max_design_mp=53.000
min_design_mp=1.000
critical_altitude=21500.000
emergency_boost_type=1
emergency_boost_mp_offset=10.000
emergency_boost_gain_offset=0.660
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=13.330
propeller_blades=3
propeller_moi=62.170
beta_max=65.000
beta_min=13.000
min_gov_rpm=1800.000
prop_tc=0.010
gear_reduction_ratio=2.000
fixed_pitch_beta=0.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000
beta_feather=0.000
power_absorbed_cf=0.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000

[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

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=900.0
autothrottle_available=0
pitch_takeoff_ga=8.0
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

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=0, 0
Nav.1=1, 0, 0
Nav.2=0, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=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=1.000, -18.000, 0.000, -3.700, 3200.000, 0.000, 0.500, 180.000, 0.250, 2.500, 0.900, 1.000, 4.000, 0.000, 0.000, 337.611
point.1=1.000, 1.800, -5.930, -8.500, 2200.000, 1.000, 1.350, 0.000, 0.540, 2.500, 0.760, 5.500, 4.500, 2.000, 0.000, 337.611
point.2=1.000, 1.800, 5.930, -8.500, 2200.000, 2.000, 1.350, 0.000, 0.540, 2.500, 0.760, 5.500, 4.500, 3.000, 0.000, 337.611
point.3=2.000, 0.000, -20.000, -1.250, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2.000, 0.000, 20.000, -1.250, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2.000, -20.250, 0.000, -1.660, 2400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2.000, 5.410, 0.000, -3.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7=2.000, 0.000, -5.430, -3.750, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.8=2.000, 0.000, 5.430, -3.750, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

static_cg_height=7.000
static_pitch=13.900
gear_system_type=1

[Views]
eyepoint=-6.2, 0.00, 3.55      //(feet) longitudinal, lateral, vertical distance from reference datum

[LSO]
LSOAdjustSpeed=1.2


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
panel=0.00, 0.45, -2.00, fx_vclight


[fuel]
Center1=-1.940, 0.000, -0.500, 187.000, 0.000
Center2=-1.940, 0.000, -0.500, 50.000, 0.000
LeftMain=-0.970, -12.250, -1.610, 62.000, 0.000
RightMain=-0.970, 12.250, -1.610, 62.000, 0.000
External1=1.940, 0.000, -3.870, 175.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=314.000
wing_span=41.000
wing_root_chord=7.833
wing_dihedral=13.596
wing_incidence=1.000
wing_twist=0.000
oswald_efficiency_factor=0.699
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=24.000
htail_span=11.000
htail_pos_lon=-18.833
htail_pos_vert=0.000
htail_incidence=-1.000
htail_sweep=0.000
vtail_area=15.000
vtail_span=4.416
vtail_sweep=0.000
vtail_pos_lon=-18.833
vtail_pos_vert=0.583
elevator_area=13.000
aileron_area=20.400
rudder_area=13.060
elevator_up_limit=26.001
elevator_down_limit=26.001
aileron_up_limit=21.497
aileron_down_limit=20.346
rudder_limit=28.997
elevator_trim_limit=19.996
spoiler_limit=59.989
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
[GeneralEngineData]
engine_type=0
Engine.0=7.000, 0.000, 0.000
fuel_flow_scalar=1.000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=65.000
full_flaps_stall_speed=52.000
cruise_speed=288.725
max_indicated_speed=760.500000
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=100.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
[direction_indicators]
direction_indicator.0=1,0

[Flaps.0]
type=1
span-outboard=0.125
extending-time=5.000
system_type=0
damaging-speed=201.000
blowout-speed=305.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=10.000, 0.000
flaps-position.2=20.000, 0.000
flaps-position.3=35.000, 0.000
flaps-position.4=40.000, 0.000
flaps-position.5=55.000, 0.000

[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

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556

[stall_warning]
type=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[fltsim.1]
title=P47 Senta a Pua
sim=P47DT
model=
panel=
sound=
texture=1
kb_checklists=
description=FS2002\/2004 P-47D-25 model\nBy JRLucariny\nhttp:\/\/lucariny.sites.uol.com.br\nA P-47D-25 assigned to the 1st Grupo de Caça, Força Aerea Brasileira, and attached to the 350th Fighter Group in Italy during 1944.

ui_manufacturer=Republic
ui_type=1st Brazilian Fighter Squadron
ui_variation=P-47 Cris
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=