[fltsim.0] title=Cessna 208 Caravan Amphibian sim=Cessna208 model= panel= sound= texture= kb_checklists=Cessna208_Check kb_reference=Cessna208_ref atc_id=N700MS atc_id_color=0xff000000 ui_manufacturer=Cessna ui_type=C208 Caravan Amphibian ui_variation=Yellow with black visual_damage=1 description=If you're looking for a new flying challenge, you'll find it behind the controls of the Caravan Amphibian. The Amphibian is the largest single-engine floatplane currently manufactured and is a versatile aircraft for both passenger and cargo operations. The floats on the Amphibian contain landing gear, making it possible to land anywhere, water or land. [fltsim.1] title=Cessna 208 Caravan Amphibian Paint1 sim=Cessna208 model= panel= sound= texture=1 kb_checklists=Cessna208_Check kb_reference=Cessna208_ref atc_id_color=0xff000000 atc_id=N700MS atc_airline=Gaia atc_flight_number=1123 ui_manufacturer=Cessna ui_type=C208 Caravan Amphibian ui_variation=Gaia Airlines visual_damage=1 description=If you're looking for a new flying challenge, you'll find it behind the controls of the Caravan Amphibian. The Amphibian is the largest single-engine floatplane currently manufactured and is a versatile aircraft for both passenger and cargo operations. The floats on the Amphibian contain landing gear, making it possible to land anywhere, water or land. [fltsim.2] title=Cessna 208 Caravan Amphibian Paint2 sim=Cessna208 model= panel= sound= texture=2 kb_checklists=Cessna208_Check kb_reference=Cessna208_ref atc_id_color=0xff000000 atc_id=N700MS ui_manufacturer=Cessna ui_type=C208 Caravan Amphibian ui_variation=White with blue and gold visual_damage=1 description=If you're looking for a new flying challenge, you'll find it behind the controls of the Caravan Amphibian. The Amphibian is the largest single-engine floatplane currently manufactured and is a versatile aircraft for both passenger and cargo operations. The floats on the Amphibian contain landing gear, making it possible to land anywhere, water or land. [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 Range\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=8035 // (pounds) empty_weight=4265 // (pounds) reference_datum_position=13.1, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-14.2, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -11.3, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -11.3, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=170, -13.9, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=170, -13.9, 1.5, 0.0 //Rear Passenger 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 flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // 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 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.8 //Propeller Diameter, (feet) propeller_blades=3 //Number of propeller blades propeller_moi=19 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.4 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=88.0 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [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, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 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] //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=1, -1.15, -5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.80, 4.0, 4.0, 0, 0.0, 0.0 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, 0.0, 0.0 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, 0.0, 0.0 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, 0.0, 0.0 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=0.983 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.344 //feet, altitude of CG when at rest on the ground [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 [SMOKESYSTEM] smoke.0=0.00,3.00,0.00, fx_engsmoke [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks 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 [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=0.0 //Degrees, wing leading edge wing_pos_apex_lon=-14.0 //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 [Reference Speeds] flaps_up_stall_speed=66.0 //Knots True (KTAS) full_flaps_stall_speed=52.8 //Knots True (KTAS) cruise_speed=143.0 //Knots True (KTAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [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
