[fltsim.0] title=Cessna 310 sim=Cessna 310 model= panel= sound= texture=songbird checklists= ui_manufacturer=Cessna ui_type=310 ui_model=c310 ui_variation=Sky King's Songbird atc_id=N5348A prop_anim_ratio=-1.90 description=This Cessna is one of the most recognizable twin engine aircraft to alot of 50 + adults today. Original was "b" model. "Out of the Blue of the Western Sky....". [General] atc_type=Cessna atc_model=310 editable=1 performance=Cruise Speed\n200 kts 370 km\/hr\n\nEngine\nTeledyne Continental Motors IO-550-C 300 hp\n\nPropeller\nThree-bladed McCauley constant-speed, variable pitch\n\nMaximum Range\n1,569 nm 2,906 km\n\nService Ceiling\n20,688 ft 6,306 km\n\nFuel Capacity\n142 gal 537 L\n\nMaximum Gross Weight\n5,524 lb 2,509 kg \n\nLength\n29 ft, 10 in 9.09 m\n\nWingspan\n37 ft, 10 in 11.53 m\n\nHeight\n9 ft, 9 in 2.97 m\n\nSeating Up to 6\n\nUseful Load\n1,634 lb 741 kg [WEIGHT_AND_BALANCE] max_gross_weight = 5500 empty_weight = 3900 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 1 station_load.0 = 200, -3, 0, 3, // Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight_pitch_MOI = 3900 empty_weight_roll_MOI = 2718 empty_weight_yaw_MOI = 4026 empty_weight_coupled_MOI = 0 reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 //station_load.0 = 170, -6.54, -1.20, 0.0 //Pilot Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //station_load.1 = 170, -6.54, 1.20, 0.0 //Co-Pilot Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //station_load.2 = 170, -9.80, -1.20, 0.0 //Passenger Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //station_load.3 = 170, -9.80, 1.20, 0.0 //Passenger Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //station_load.4 = 0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //station_load.5 = 0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //station_load.6 = 0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), //longitudinal, lateral, vertical positions from datum (feet) //;Moments of Inertia //empty_weight_pitch_MOI = 3905.65 //empty_weight_roll_MOI = 2718.64 ///empty_weight_yaw_MOI = 5291.04 //empty_weight_coupled_MOI= 0.0 [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 = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 4.0, -5.9, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 4.0, 5.9, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 0.9 //Fuel flow scalar min_throttle_limit=0.000000 [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 91.7 //Cubic inches per cylinder compression_ratio= 8.0 //Compression ratio number_of_cylinders= 6 //Number of cylinders max_rated_rpm= 2700.0 //Max rated RPM max_rated_hp= 300.0 //Max rated HP fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter 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= 0.0 //Max design manifold pressure, (inHg) min_design_mp= 1.0 //Min design manifold pressure, (inHg) critical_altitude= 0.0 //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= 0.0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0.0 //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] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.4 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 6.9 //Propeller moment of inertia beta_max= 45.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 15.2 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1100.0 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 1 //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= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering beta_feather= 82.5 //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= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees) [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 (0=Undamped, 1=Critically Damped) //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) //GEAR point.0 = 1, 8.5, 0.00, -3.7, 1600, 0, 0.633, 40, 0.42, 2.5, 0.80, 3.0, 5.0, 0, 152, 180 point.1 = 1, -2.0, -4.79, -3.2, 1600, 1, 0.886, 0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 152, 200 point.2 = 1, -2.0, 4.79, -3.2, 1600, 2, 0.886, 0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 152, 200 //SCRAPES point.3= 2, -6.20,-18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4= 2, -6.20, 18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5= 2,-24.04, 0.00, -0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6= 2, 0.40, 0.00, -1.24, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch = 1.091 //Degrees static_cg_height = 3.0815 //Feet gear_system_type=0 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.41 // 0.0 .. 1.0 extending-time = 4 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15 // degrees flaps-position.2 = 30 // degrees damaging-speed = 152 // KIAS blowout-speed = 250 // KIAS [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits = 3 exit_rate.0 = 0.4 ;Percent per second [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 [Views] eyepoint = 0.5, -0.6, 2.620 //Longitudinal, Lateral, Vertical (feet) [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -3.20, -17.50, 1.0, fx_navred , light.1 = 3, -3.20, 17.51, 1.0, fx_navgre , light.2 = 3, -16.33, 0.00, 1.0, fx_navwhi , light.3 = 2, -2.5, -17.50, 1.0, fx_strobe , light.4 = 2, -2.5, 17.51, 1.0, fx_strobe , light.5 = 1, -16.58, 0.00, 7.57, fx_beacon , light.6 = 2, -4.00, 0.00, -0.8, fx_strobe , light.7 = 4, 3.00, -1.40, 2.00, fx_vclight, light.8 = 4, 3.00, -0.50, 2.00, fx_vclight, light.9 = 4, 3.00, 0.50, 2.00, fx_vclight, light.10 = 4, 3.00, 1.50, 2.00, 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, 250 aileron = 100, 250 rudder = 100, 250 [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 [fuel] LeftMain = 0.5, -7.45, 0.0, 71.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = 0.5, 7.45, 0.0, 71.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area = 199.0 //Square feet wing_span = 37.8 //Feet wing_root_chord = 5.3 //Feet wing_dihedral = 6.9 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -1.0 //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 = 1.5 //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 = 60.0 //Square feet htail_span = 15.9 //Feet htail_pos_lon = -11.1 //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 = 0.5 //Degrees htail_sweep = 0.0 //Degrees, horizontal tail leading edge vtail_area = 88.0 //Square feet vtail_span = 10.7 //Feet, tip to body vtail_sweep = 0.0 //Degrees, vertical tail leading edge vtail_pos_lon =-7.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.1 //Feet, vertical distance from reference point, positive going up elevator_area = 20.0 //Square feet aileron_area = 11.3 //Square feet rudder_area = 10.5 //Square feet elevator_up_limit = 17.0 //Degrees elevator_down_limit = 15.5 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //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 = 96.0 //Knots True (KTAS) full_flaps_stall_speed = 76.8 //Knots True (KTAS) cruise_speed = 200.0 //Knots True (KTAS) max_indicated_speed=259.000000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 700.0 autothrottle_available= 0 pitch_takeoff_ga=8.000000 crash_duration2=2500000 ; in microseconds 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 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5# ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1# crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=31.512679 flap_limit_idle=31.512679 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0