// Floatplane AI configuration files
// by Holger Sandmann, hsandman@sfu.ca
// FS9 Version, January 2004
[fltsim.0]
title=AI Cessna 208 Caravan Amphibian Yellow
sim=Cessna208
model=
panel=
sound=
texture=
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id=N208YB
atc_id_color=0xff000000
atc_parking_types=RAMP
atc_parking_codes=G003
ui_manufacturer=AI Floatplane
ui_type="C208 Caravan Amphibian Yellow"
ui_variation="Yellow with black"
description=AI C208AMPH\n\n! Not For Commercial Use !\n! Only For AI Traffic !\n\nDesigner: Microsoft Default Model
[fltsim.1]
title=AI Cessna 208 Caravan Amphibian Gaia
sim=Cessna208
model=
panel=
sound=
texture=1
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id_color=0xff000000
atc_id=N208GA
atc_airline=Gaia
atc_flight_number=1123
atc_parking_types=RAMP
atc_parking_codes=G003
ui_manufacturer=AI Floatplane
ui_type="C208 Caravan Amphibian Gaia"
ui_variation="Gaia Airlines"
description=AI C208AMPH\n\n! Not For Commercial Use !\n! Only For AI Traffic !\n\nDesigner: Microsoft Default Model
[fltsim.2]
title=AI Cessna 208 Caravan Amphibian Blue
sim=Cessna208
model=
panel=
sound=
texture=2
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id_color=0xff000000
atc_id=N208GB
atc_parking_types=RAMP
atc_parking_codes=G003
ui_manufacturer=AI Floatplane
ui_type="C208 Caravan Amphibian Blue"
ui_variation="White with blue and gold"
description=AI C208AMPH\n\n! Not For Commercial Use !\n! Only For AI Traffic !\n\nDesigner: Microsoft Default Model
[General]
atc_type=Cessna
atc_model=C208
editable=0
performance="Maximum Speed\n175 KIAS 324 km\/hr\n\nCruise Speed\n143 KIAS (8,000 lb) 265 km\/h\n130 KIAS (6,400 lb) 241 km\/h\n117 KIAS (5,200 lb) 216 km\/h\n\nEngine\nPratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp\n\nPropeller\nThree-Bladed, Constant Speed, Full Feathering, Reversible McCauley, 106-inch diameter\n\nMaximum Endurance\n4.6 hours maximum cruise at 10,000 ft\n5.7 hours maximum cruise at 20,000 ft\n6.8 hours maximum range at 10,000 ft\n8.0 hours maximum range at 20,000 ft\n\nService Ceiling\n20,000 ft 6,096 m\n\nFuel Capacity\n335 gal 1,268 L\n\nEmpty Weight\n4,895 lb 2,220 kg\n\nMaximum Gross Weight\n8,035 lb 3,645 kg\n\nUseful Load\n3,140 lb 1,424 kg\n\nLength\n41 ft, 7 in\t 12.7 m\n\nWingspan\n52 ft, 1 in\t 15.8 m\n\nHeight\n15 ft, 5-1\/2 in 4.8 m\n\nSeating\nUp to 14"
[WEIGHT_AND_BALANCE]
max_gross_weight = 8000 // (pounds)
empty_weight = 4895 // (pounds)
reference_datum_position = 13.1, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -13.6, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170.0, -11.3, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, -11.3, 1.5, 0.0, Passenger 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "160.0, -13.9, -2.0, 0.0, Passenger 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "160.0, -13.9, 2.0, 0.0, Passenger 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0.0, -18.8, -2.0, 0.0, Passenger 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "0.0, -18.8, 2.0, 0.0, Passenger 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = " 50.0, -21.0, 0.0, 0.0, Cargo Zone 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "25.0, -23.5, 0.0, 0.0, Cargo Zone 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0.0, -25.6, 0.0, 0.0, Cargo Zone 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0.0, -27.5, 0.0, 0.0, Cargo Zone 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "0.0, -9.9, -5.3, -6.5, Left Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "0.0, -9.9, 5.3, -6.5, Right Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 7241.36
empty_weight_roll_MOI = 5618.57
empty_weight_yaw_MOI = 10431.43
empty_weight_coupled_MOI = 0.0
[Flaps.0]
type=1
span-outboard=0.5 // Percent span for flap position
extending-time=5.7 // Seconds, time to fully extend
system_type=0 // 0 = electrical
damaging-speed = 175 // KIAS
blowout-speed = 175 // KIAS
flaps-position.0= 0 // degrees
flaps-position.1=10,175 // degrees
flaps-position.2=20,150 // degrees
flaps-position.3=30,125 // degrees
[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
[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -1.3, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.12 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar=1.8 //Propeller thrust scalar
propeller_type=0
propeller_diameter=8.830000
propeller_blades=4
propeller_moi=80.000000
beta_max=45.000000
beta_min=15.600000
min_gov_rpm=25520.000000
prop_tc=0.004000
gear_reduction_ratio=17.368000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=700.000000
beta_feather=88.000000
power_absorbed_cf=0.900000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=1.000000
minimum_reverse_beta=-14.000000
[TurbineEngineData]
fuel_flow_gain = 0.011 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 33000 //RPM, second stage compressor rated value
static_thrust = 158 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar = 1.0 //Scalar on Turboprop power
maximum_torque = 1865 //Maximum torque available (ft-lbs)
[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
[contact_points]
point.0=4, -1.20, -5.250, -5.300, 5600, 0, 0.319, 0.0, 0.800, 2.500, 0.800, 4.0, 4.0, 0, 175.0, 175.0
point.1=4, -1.20, 5.250, -5.300, 5600, 0, 0.319, 0.0, 0.800, 2.500, 0.800, 4.0, 4.0, 1, 175.0, 175.0
point.2=4, -28.40, -5.250, -3.600, 5600, 0, 0.319, 0.0, 0.800, 2.500, 0.800, 4.0, 4.0, 2, 175.0, 175.0
point.3=4, -28.40, 5.250, -3.600, 5600, 0, 0.319, 0.0, 0.800, 2.500, 0.800, 4.0, 4.0, 3, 175.0, 175.0
point.4=1, -8.10, -5.350, -5.500, 5600, 0, 0.519, 90.0, 0.800, 2.500, 0.600, 4.0, 4.0, 0, 175.0, 175.0
point.5=1, -8.10, 5.350, -5.500, 5600, 0, 0.519, 90.0, 0.800, 2.500, 0.600, 4.0, 4.0, 0, 175.0, 175.0
point.6=1, -20.10, -5.350, -3.800, 5600, 1, 0.519, 90.0, 0.800, 2.500, 0.600, 4.0, 4.0, 0, 175.0, 175.0
point.7=1, -20.10, 5.350, -3.800, 5600, 2, 0.519, 90.0, 0.800, 2.500, 0.600, 4.0, 4.0, 0, 175.0, 175.0
//point.0=1, -1.15, -5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.80, 4.0, 4.0, 0, 175.0, 175.0
//point.1=1, -1.15, 5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.80, 4.0, 4.0, 1, 175.0, 175.0
//point.2=1, -16.40, -5.250, -7.700, 1600, 1, 1.50, 0.0, 0.4, 2.5, 0.80, 4.0, 4.0, 2, 175.0, 175.0
//point.3=1, -16.40, 5.250, -7.700, 1600, 2, 1.50, 0.0, 0.4, 2.5, 0.80, 4.0, 4.0, 3, 175.0, 175.0
//point.4=4, -4.00, -5.250, -5.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
//point.5=4, -4.00, 5.250, -5.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
//point.6=4, -26.35, -5.250, -4.800, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
//point.7=4, -26.35, 5.250, -4.800, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
//point.8=2, -12.90, -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.9=2, -12.90 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.10=2, -36.23, 0.00, 0.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
//point.11=2, -0.50, 0.00, -2.17, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
//point.12=2, -38.00, 0.00, 9.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
//point.13=5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0
//point.14=5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0
max_number_of_points=21
static_pitch=0.000000
static_cg_height=5.344 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 2 //Amphib
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 20.1 //Flap angle that activates warning at idle
flap_limit_power = 13.0 //Flap angle that activates warning at above idle
[brakes]
toe_brakes_scale=0.335704
parking_brake=0
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,0,0,0 //pump on Eng1
[Views]
eyepoint= -10.5, -1.4, 2.4 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, -12.80, -25.98, 2.72, fx_navred ,
light.1=3, -12.80, 25.98, 2.72, fx_navgre ,
light.2=3, -38.62, 0.00, 1.84, fx_navwhi ,
light.3=2, -13.17, -25.98, 2.72, fx_strobe ,
light.4=2, -13.17, 25.98, 2.72, fx_strobe ,
light.5=1, -36.20, 0.00, 9.15, fx_beacon ,
light.6=4, -9.49, 0.00, 0.98, 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
[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=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0 = 1.16, -22.0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_spray
concrete=fx_AI_floatplane_spray-and-wake
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[fuel]
LeftMain = -15.3, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -15.3, 1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 279.0 //Square feet
wing_span = 52.1 //Feet
wing_root_chord = 6.4 //Feet
wing_dihedral = 3.9 //Degrees
wing_incidence = 2.5 //Degrees
wing_twist = -1.7 //Degrees
oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 2.96 //Degrees, wing leading edge
wing_pos_apex_lon = -12.3 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 39.0 //Square feet
htail_span = 11.7 //Feet
htail_pos_lon = -27.8 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 2.0 //Degrees
htail_sweep = 5.0 //Degrees, horizontal tail leading edge
vtail_area = 18.0 //Square feet
vtail_span = 4.8 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -25.7 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 20.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 1 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
spoiler_handle_available = 0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only
[Reference Speeds]
flaps_up_stall_speed = 72.0 //Knots True (KCAS)
full_flaps_stall_speed = 58.0 //Knots True (KCAS)
cruise_speed = 143.0 //Knots True (KTAS)
max_mach = 0.60
max_indicated_speed = 175 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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
[stall_warning]
type=2
