[fltsim.0]
title=Aviat Husky A-1B FL
sim=Aviat Husky A-1B
model=
panel=
sound=
texture=
kb_checklists=Husky_check
kb_reference=Husky_ref
atc_id=N528J
ui_manufacturer=Aviat
ui_type=A-1B Husky w/floats
ui_variation=Blue w/Red
description=If the bush is calling, think of the Husky as your cell phone. It'll get you there. Way out there. Designed to carry two people in comfort along with an extraordinary load, the versatile, long range Husky can be flown in and out of primitive clearings, ponds, rivers, beaches, glaciers, sand dunes, and the occasional paved runway. Husky is synonymous with utility.\n
[fltsim.1]
title=Aviat Husky A-1B FL paint1
sim=Aviat Husky A-1B
model=
panel=
sound=
texture=1
kb_checklists=Husky_check
kb_reference=Husky_ref
atc_id=N360HU
ui_manufacturer=Aviat
ui_type=A-1B Husky w/floats
ui_variation=Red w/White
description=If the bush is calling, think of the Husky as your cell phone. It'll get you there. Way out there. Designed to carry two people in comfort along with an extraordinary load, the versatile, long range Husky can be flown in and out of primitive clearings, ponds, rivers, beaches, glaciers, sand dunes, and the occasional paved runway. Husky is synonymous with utility.\n
[fltsim.2]
title=Aviat Husky A-1B FL BFU
sim=Aviat Husky A-1B
model=
panel=
sound=
texture=bfu
kb_checklists=Husky_check
kb_reference=Husky_ref
atc_id=N123BU
ui_manufacturer=Aviat
ui_type=A-1B Husky w/floats
ui_variation=Bush Flying Unlimited
description=If the bush is calling, think of the Husky as your cell phone. It'll get you there. Way out there. Designed to carry two people in comfort along with an extraordinary load, the versatile, long range Husky can be flown in and out of primitive clearings, ponds, rivers, beaches, glaciers, sand dunes, and the occasional paved runway. Husky is synonymous with utility.\n
[fltsim.3]
title=Aviat Husky A-1B FL NAS
sim=Aviat Husky A-1B
model=
panel=
sound=
texture=nas
kb_checklists=Husky_check
kb_reference=Husky_ref
atc_id=N929NS
ui_manufacturer=Aviat
ui_type=A-1B Husky w/floats
ui_variation=Nightwolf Air Service
description=If the bush is calling, think of the Husky as your cell phone. It'll get you there. Way out there. Designed to carry two people in comfort along with an extraordinary load, the versatile, long range Husky can be flown in and out of primitive clearings, ponds, rivers, beaches, glaciers, sand dunes, and the occasional paved runway. Husky is synonymous with utility.\n
[General]
atc_type=Aviat
atc_model=A1B
editable=0
performance=Maximum Speed\t126 kts\nCruise Speed\t113 kts\nMaximum Range\t800 nm\nService Ceiling\t20,000 ft\nMax Gross Weight\t2,000 lb\nSeating\t\t2\nUseful Load\t810 lb\n
[WEIGHT_AND_BALANCE]
max_gross_weight=2200.000000 // (pounds)
empty_weight=1437.000000 // (pounds)
reference_datum_position=0.00,0.00,0.00 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-1.00,0.00,0.00 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0="218.00, 0.50, 0.00, 1.60, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="000.00,-0.59, 0.00, 1.60, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="000.00,-0.98, 0.00, 1.60, Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_roll_MOI=1937.000000
empty_weight_pitch_MOI=2300.000000
empty_weight_yaw_MOI=3160.000000
empty_weight_coupled_MOI=0.000000
[fuel]
LeftMain=-0.25, -2.10, 2.50,26.00,25.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-0.25, 2.10, 2.50, 26.00, 25.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1.00 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[flight_tuning]
cruise_lift_scalar=0.40
parasite_drag_scalar=1.1
induced_drag_scalar=0.55
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=1.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[airplane_geometry]
wing_area=183.000000 //Square feet
wing_span=35.500000 //Feet
wing_root_chord=4.916670 //Feet
wing_dihedral=1.735840 //Degrees
wing_incidence=1.499634 //Degrees
wing_twist=-2.999268 //Degrees
oswald_efficiency_factor=0.819935 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=0.000000 //Degrees, wing leading edge
wing_pos_apex_lon=1.229000 //Feet, longitudinal distance from reference point
wing_pos_apex_vert=0.000000 //Feet, vertical distance from reference point
htail_area=39.000000 //Square feet
htail_span=11.666667 //Feet
htail_pos_lon=-14.666667 //Feet, longitudinal distance from reference point
htail_pos_vert=0.000000 //Feet, vertical distance from reference point
htail_incidence=1.499634 //Degrees
htail_sweep=0.000000 //Degrees, horizontal tail leading edge
vtail_area=18.000000 //Square feet
vtail_span=4.837355 //Feet, tip to body
vtail_sweep=0.000000 //Degrees, vertical tail leading edge
vtail_pos_lon=-12.583333 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.500000 //Feet, vertical distance from reference point, positive going up
elevator_area=16.610000 //Square feet
aileron_area=18.300000 //Square feet
rudder_area=6.650000 //Square feet
elevator_up_limit=29.00 //Degrees
elevator_down_limit=15.00 //Degrees
aileron_up_limit=20.00 //Degrees
aileron_down_limit=20.00 //Degrees
rudder_limit=25.00 //Degrees
elevator_trim_limit=19.497754 //Degrees
spoiler_limit=90.000000 //Degrees
spoilerons_available=0 //Spoilerons Available?
aileron_to_spoileron_gain=0.000000 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0.000000 //Degrees
min_flaps_for_spoilerons=0.000000 //Minimum flap handle position when spoilerons activate
//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]
point.0=4, 2.35, -3.250, -3.25, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 1.00, 0.00, 0.00, 0.00, 0.00, 0.00
point.1=4, 2.35, 3.250, -3.25, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 1.00, 0.00, 0.00, 1.00, 0.00, 0.00
point.2=4, -8.00, -3.250, -2.60, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 1.00, 0.00, 0.00, 2.00, 0.00, 0.00
point.3=4, -8.00, 3.250, -2.60, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 1.00, 0.00, 0.00, 3.00, 0.00, 0.00
point.4=2, -3.16, -16.75, 3.00, 1573.93, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.5=2, -3.16, 16.75, 3.00, 1573.93, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.6=2, -14.91, 0.00, 1.16, 1573.93, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.7=2, 2.08, 0.00, 1.58, 1573.93, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.8=2, 0.00, -24.00, 4.00, 308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 7.00, 0.00, 0.00
point.9=2, -19.58, 0.00, 7.50, 30.03, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 8.00, 0.00, 0.00
point.10=5, -9.00, -3.000, -3.00, 1600.00, 0.00, 0.00, 50.00, 0.00, 0.00, 1.00, 1.10, 1.50, 0.00, 0.00, 0.00
point.11=5, -9.00, 3.000, -3.00, 1600.00, 0.00, 0.00, 50.00, 0.00, 0.00, 1.00, 1.10, 1.50, 0.00, 0.00, 0.00
max_number_of_points = 21
static_pitch=00.78 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=2.73 //feet, altitude of CG when at rest on the ground
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.68 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10.0 // degrees
flaps-position.2 = 20.0 // degrees
flaps-position.3 = 30.0 // degrees
damaging-speed = 120 // KIAS
blowout-speed = 150 // KIAS
lift_scalar = 1.6
drag_scalar = 1.0
pitch_scalar= 0.6
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 6.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.80 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.25 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm= 2700 //Max rated RPM
max_rated_hp= 180 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
propeller_type=0
propeller_diameter=6.33
propeller_blades=2
propeller_moi=5.700000
beta_max=29.000000
beta_min=11.700000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
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
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[Reference Speeds]
flaps_up_stall_speed=54.00 //Knots True (KTAS)
full_flaps_stall_speed=43.20 //Knots True (KTAS)
cruise_speed=121.00 //Knots True (KTAS)
max_indicated_speed=180.00 //Red line (KIAS)
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[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=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000
[Views]
eyepoint=-1.70 ,0.00, 2.75
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=2, -1.78, -16.81, 3.50, fx_strobe
light.1=2, -1.78, 16.81, 3.50, fx_strobe
light.2=4, -0.78, 0.00, 1.00, fx_vclighth
[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
[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=1,0
[stall_warning]
type=1
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
