[fltsim.0] title=Lancair Columbia 300 sim=Lancair300 model= panel= sound= texture= kb_checklists=Lancair300_check kb_reference=Lancair300_ref atc_id=N412LC ui_manufacturer=Lancair ui_type=300 ui_variation=White with blue description=This model depicts the Lancair Columbia 300 "New Spirit\n of St. Louis" as flown by Erik Lindbergh on May 2, 2002, during his non-stop\n Trans-Atlantic flight from New York Long Island Republic Airport (KFRG) to\n Paris Le Bourget (LFPB) thus duplicating the flight of his Grandfather,\n Charles A. Lindbergh on May 8, 1927 which took 33 1/2 hours. Erik's flight\n lasted 17 hours, 7 minutes. [General] atc_type=Lancair atc_model=300 editable=0 performance=All numbers are for the stock Lancair Columbia 300\n Lindbergh carried a total of 310 gallons of fuel in two long-range tanks\n plus the normal main tank.\n Maximum Speed (VNE)\t230 kts\n Cruise Speed\t\n195 kts\n Engine\t\nTeledyne Continental Motors IO-550-N 310 hp\n\nPropeller\t\nThree-bladed Hartzell constant speed\n\nMaximum Range\t\n1,010 nm\n\nService Ceiling\t\n18,000 ft\n\nFuel Capacity\t\n106 U.S. gal \n\nEmpty Weight\t\n2,250 lb\n\nMaximum Gross Weight\t\n3,400 lb\n\nUseful Load\t\n1,150 lb\n\nLength\t\n26.17 ft\n\nWingspan\t\n38 ft\n\nSeating\t\nUp to 4 [airplane_geometry] wing_area=142.0 //Square feet wing_span=38.0 //Feet wing_root_chord=5.3 //Feet wing_dihedral=7.2 //Degrees wing_incidence=2.0 //Degrees wing_twist=-2.0 //Degrees oswald_efficiency_factor=0.9 //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=-6.4 //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=27.0 //Square feet htail_span=12.5 //Feet htail_pos_lon=-12.9 //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=3.2 //Degrees htail_sweep=0.0 //Degrees, horizontal tail leading edge vtail_area=11.0 //Square feet vtail_span=3.8 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-12.6 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=1.3 //Feet, vertical distance from reference point, positive going up elevator_area=24.4 //Square feet aileron_area=10.6 //Square feet rudder_area=4.9 //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=0.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //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=80.0 //Knots True (KTAS) full_flaps_stall_speed=70.0 //Knots True (KTAS) cruise_speed=190.0 //Knots True (KTAS) [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=100.0, 180.0 aileron=200.0, 1000.0 rudder=200.0, 1000.0 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=170.000000,0.6200000,0.000000,0.000000 empty_weight=2250.000000 empty_weight_roll_MOI=1137.000000 empty_weight_pitch_MOI=1400.000000 empty_weight_yaw_MOI=2360.000000 empty_weight_coupled_MOI=0.000000 [fuel] LeftMain=-0.250000,-2.100000,2.500000,53.300000,3.000000 RightMain=-0.250000,2.100000,2.500000,53.000000,3.000000 fuel_type=1.000000 number_of_tank_selectors=1 //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=1.000, 6.009, 0.000, -2.939,1181.100, 0.000,0.658,33.660,0.296,2.500,0.794,0.000,0.000,0.000, 0.000,0.000 //nose gear wheel point.1=1.000,-0.489,-3.937,-2.939,1574.803,1.000,0.877,0.000,0.286,2.500,0.808,0.000,0.000,2.000, 0.000, 0.000 //left main wheel point.2=1.000,-0.489,3.825,-2.939,1574.803,2.000,0.877,0.000,0.286,2.500,0.808,0.000,0.000,3.000, 0.000,0.000 //right main wheel point.3=2.000,7.417,0.000,0.102,1574.803,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000 //nose scrape point point.4=2.000,-13.301,0.000,0.593,0.102,1574.803,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,9.000,0.000,0.000 //tail scrape point point.5=2.000,-1.632,-19.027,0.793,1574.803,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,5.000,0.000,0.000 //left wing scrape point point.6=2.000,-1.632,19.027,0.793,1574.803,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,6.000,0.000,0.000 /right wing scrape point max_number_of_points=21 static_pitch=1.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=3.265 //feet, altitude of CG when at rest on the ground //static_pitch=0.000000? //static_cg_height=3.015259? [Flaps.0] type=1 span-outboard=0.670000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=12.666187,0.000000 flaps-position.2=25.332374,0.000000 flaps-position.3=37.998561,0.000000 [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 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 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 [GeneralEngineData] engine_type=0 Engine.0=6.000000,0.000000,0.000000 fuel_flow_scalar=1.000000 [piston_engine] cylinder_displacement=91.666666 compression_ratio=8.500000 number_of_cylinders=6 max_rated_rpm=2700.000000 max_rated_hp=310.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=38.000000 min_design_mp=0.000000 critical_altitude=20000.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 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] propeller_type=1 propeller_diameter=6.25000 propeller_blades=3 propeller_moi=9.000000 beta_max=0.000000 beta_min=0.000000 min_gov_rpm=0.000000 prop_tc=0.000000 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_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Views] eyepoint=1.026000,-1.082000,2.985000 [direction_indicators] direction_indicator.0=1,0 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=900.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -1.59, -19.00, 1.09, fx_navred light.1=3, -1.59, 19.00, 1.09, fx_navgre light.2=3, -13.46, 0.00, 1.31, fx_navwhi light.3=2, -14.82, 0.00, 6.04, fx_strobe light.4=2, -1.59, -19.00, 1.09, fx_strobe light.5=2, -1.59, 19.00, 1.09, fx_strobe light.5=1, 5.274, 0.00, -0.76, fx_beaconh [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [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
