[fltsim.0]
title=FW-58BW Floatplane
sim=FW-58BW
model=
panel=
sound=
texture=float
checklists=
ui_manufacturer=Focke Wulf
ui_type=Weihe_floatplane
description=Twin-engined Focke-Wulf FW58-C 'Weihe' rescue floatplane, 1935, with transparent nose for fore gunner, and open rear gunner position.
[General]
performance=Length: 45 ft 11 in\nSpan: 68 ft 10 in \/ Area: 506 sq ft\nPower: 2x240 Hp Argus As10C V8 inv.\nTop Speed: 143 Kt \/ Landing: 46 Kt\nMTOW: 6446 lb Empty: 5291 lb\nCeiling: 17000 ft \/ Range: 432 nm\n\nGMAX model by A.F.Scrub\nDecember 2011
Category=airplane
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=6780.000000
empty_weight_roll_MOI=29100.000000
empty_weight_pitch_MOI=114000.000000
empty_weight_yaw_MOI=312000.000000
empty_weight_coupled_MOI=9700.000000
max_gross_weight=10170.000000
[fuel]
LeftMain=-0.666667,-15.000000,1.500000,60.000000,0.000000
RightMain=-0.666667,15.000000,1.500000,60.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=506.000000
wing_span=69.000000
wing_root_chord=7.333333
wing_dihedral=4.273682
wing_incidence=0.274658
wing_twist=0.675659
oswald_efficiency_factor=0.960193
wing_winglets_flag=65
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=120.000000
htail_span=40.000000
htail_pos_lon=-30.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=90.000000
vtail_span=10.816654
vtail_sweep=0.000000
vtail_pos_lon=-30.000000
vtail_pos_vert=15.000000
elevator_area=20.000000
aileron_area=28.500000
rudder_area=8.750000
elevator_up_limit=23.376678
elevator_down_limit=22.345354
aileron_up_limit=22.918312
aileron_down_limit=18.907607
rudder_limit=22.202115
elevator_trim_limit=25.210143
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=5.000000
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
[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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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 = 4, 25.00, -5.050, -13.150, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
point.1 = 4, 25.00, 5.050, -13.150, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
point.2 = 4, -3.35, -5.050, -12.950, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
point.3 = 4, -3.35, 5.050, -12.950, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
point.4 = 2, -10.90, -26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.5 = 2, -10.90 26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.6=2.000000,15.333333,0.000000,-4.500000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=10.511857
[brakes]
toe_brakes_scale=0.640889
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
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=13.330818,0.000000
flaps-position.2=26.661636,0.000000
flaps-position.3=39.992454,0.000000
[GeneralEngineData]
engine_type=0
Engine.0=10.000000,7.000000,0.250000
Engine.1=10.000000,-7.000000,0.250000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
master_ignition_switch = 1
[piston_engine]
number_of_engines=2
power_scalar=1.1
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
cylinder_displacement=120.800000
compression_ratio=8.000000
number_of_cylinders=8
max_rated_rpm=2780.000000
max_rated_hp=240.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
[propeller]
number_of_propellers=2
rotation= -1,-1
propeller_type=0
propeller_diameter=8.000000
propeller_blades=2
propeller_moi=8.960000
beta_max=32.285714
beta_min=15.000000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
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
[Reference Speeds]
flaps_up_stall_speed=63.000000
full_flaps_stall_speed=50.400000
cruise_speed=129.949412
max_indicated_speed=185.671875
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=8.575545,-0.602342,1.075049
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
[TailHook]
tailhook_length=4
tailhook_position=-15.0, 0.0, -4.0
cable_force_adjust=1.0
[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, 6.70, -34.00, -0.00, fx_navred ,
light.1=5, 6.70, 34.00, -0.00, fx_navgre ,
light.2=5, -2.00, 0.00, -4.00, fx_beacon ,
light.3=5, 11.30, -14.10, -3.90, fx_landing ,
light.4=5, -20.00, 0.00, 5.50, fx_strobeh ,
//------------ ExhaustFlames--------uses wing/taxi/logo
//index,type, long, lat, vert, fx_filename
light.5=6, 13.50, 4.80, -4.50, fx_V12_IDLE_starb
light.6=9, 13.50, 4.80, -4.50, fx_V12_Exhaust
light.7=6, 13.50, 7.80, -4.50, fx_V12_IDLE_starb
light.8=9, 13.50, 7.80, -4.50, fx_V12_Exhaust
light.9=6, 13.50, -4.80, -4.50, fx_V12_IDLE_port
light.10=9, 13.50, -4.80, -4.50, fx_V12_Exhaust
light.11=6, 13.50, -7.80, -4.50, fx_V12_IDLE_port
light.12=9, 13.50, -7.80, -4.50, fx_V12_Exhaust
[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
[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
