[fltsim.0] title=340A sim=340A model= panel= sound= texture= kb_checklists=340A_check kb_reference=340A_ref atc_id=G-AXZX atc_id_color=0xff000000 ui_manufacturer=Cessna ui_type=340A ui_variation="White, Blue and Gold" description=Cessna 340A\nTwin RAM Series VII 335hp tubrocharged TSIO-520-NB's\nDesigned with FSDS by Brian Novick\nAir file and flight dynamics by Tim Novick (modified by Roger Mole) [fltsim.1] title=340A White sim=340A model= panel= sound= texture=white kb_checklists=340A_check kb_reference=340A_ref atc_id=G-AXZX atc_id_color=0xff000000 ui_manufacturer=Cessna ui_type=340A ui_variation="White" description=Cessna 340A\nTwin RAM Series VII 335hp tubrocharged TSIO-520-NB's\nDesigned with FSDS by Brian Novick\nAir file and flight dynamics by Tim Novick (modified by Roger Mole) [General] atc_type=Cessna atc_model=340 editable=0 performance=Max Cruise Speed - 242 kts - Range 618 nm\nEconocruise - 170kt at 25,000 Ft - Range 1405 nm\nService Ceiling 26,800 ft\nInitial rate of climb - 1650ft/min\nEmpty weight - 3963, MTO - 6,430 lb\nSeating - Up to 6 [WEIGHT_AND_BALANCE] reference_datum_position= 1.40, 0.00, 0.00 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position= -0.3, 0.00, 0.00 max_number_of_stations=50 station_load.0= "170, 0.70, -0.80, 0.00, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1= "170, 0.70, 0.80, 0.00, Front Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2= "0, -2.10, -0.80, 0.00, Rear Passenger" station_load.3= "0, -2.10, 0.80, 0.00, Rear Passenger" station_load.4= "0, -5.10, -0.80, 0.00, Rear Passenger" station_load.5= "0, -5.10, 0.80, 0.00, Rear Passenger" station_load.6= "0, -8.00, 0.00, 0.00, Baggage" ;Moments of Inertia empty_weight=4448 empty_weight_roll_MOI=38800 empty_weight_pitch_MOI=72800 empty_weight_yaw_MOI=22500 empty_weight_coupled_MOI=0 max_gross_weight=6430 [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=1.9 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [fuel] LeftMain=-3.50, -3.00, 0.00, 78.00, 1.50 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = 0.0, -18.0, -0.0, 3.5, 0.0 RightMain=-3.50, 3.00, 0.00, 78.00, 1.50 RightAux = 0.0, 18.0, 0.0, 3.5, 0.0 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=198.00 wing_span=38.25 wing_root_chord=5.50 wing_dihedral=3.00 wing_incidence=1.0 wing_twist=-1.0 oswald_efficiency_factor=0.8 wing_winglets_flag=0 wing_sweep=0.00 wing_pos_apex_lon=0.0 wing_pos_apex_vert=1.4 htail_area=38.40//35.00 htail_span=17.40 htail_pos_lon=-20.00 htail_pos_vert=2.09 htail_incidence=0.5 htail_sweep=0.00 vtail_area=32.00 vtail_span=5.58 vtail_sweep=0.00 vtail_pos_lon=-17.50 vtail_pos_vert=6.00 elevator_area=23.20 aileron_area=16.22 rudder_area=11.00 elevator_up_limit=22.00 elevator_down_limit=20.00 aileron_up_limit=20.00 aileron_down_limit=20.00 rudder_limit=23.50 elevator_trim_limit=18.00 spoiler_limit=0.00 spoilerons_available=0 aileron_to_spoileron_gain=0.00 min_ailerons_for_spoilerons=0.00 min_flaps_for_spoilerons=0.00 //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, 8.20, 0.00, -4.1, 1574, 0, 0.70, 15.0, 0.20, 2.5, 0.9, 5.0, 5.0, 0.0, 165, 195 point.1=1, -1.89, -5.92, -4.4, 1574, 1, 0.70, 0.0, 0.50, 2.5, 0.9, 5.0, 5.0, 2.0, 165, 200 point.2=1, -1.89, 5.92, -4.4, 1574, 2, 0.70, 0.0, 0.50, 2.5, 0.9, 5.0, 5.0, 3.0, 165, 200 point.3=2, 2.16, -18.50, 0.75, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0 point.4=2, 2.16, 18.50, 0.75, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0 point.5=2, -16.83, 0.00, 1.16, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0 point.6=2, 10.00, 0.00, 1.16, 1574, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0 static_pitch= 0.0 static_cg_height=4.03 gear_system_type=0 [Flaps.0] type=1 span-outboard=0.50 extending-time=5 system_type=0 flaps-position.0=0 flaps-position.1=10 flaps-position.2=30 flaps-position.3=40 damaging-speed = 170 blowout-speed = 195 lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 [GeneralEngineData] engine_type=0 Engine.0=2.40, -6.97, -1.31//-0.30, -6.00, 0.00 Engine.1=2.40, 6.97, -1.31 fuel_flow_scalar=1.2 min_throttle_limit=-0.250000 [piston_engine] power_scalar = 1.0 cylinder_displacement=91.5 compression_ratio=8.50 number_of_cylinders=6 max_rated_rpm=2700 max_rated_hp=335 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.30 turbocharged=1 max_design_mp=38.5//48.0 min_design_mp=1.0 critical_altitude=26900//29800 emergency_boost_type=0 emergency_boost_mp_offset=0.00 emergency_boost_gain_offset=0.00 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1 idle_rpm_mechanical_efficiency_scalar=1 max_rpm_friction_scalar=1 idle_rpm_friction_scalar=1 [propeller] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=6.8//6.4 propeller_blades=3 propeller_moi=7.0 beta_max=45.00 beta_min=15.00 min_gov_rpm=1100 prop_tc=0.10 gear_reduction_ratio=1 fixed_pitch_beta=0 low_speed_theory_limit=80 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700 beta_feather=0 power_absorbed_cf=0.95 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.00 minimum_reverse_beta=0.00 [Reference Speeds] flaps_up_stall_speed=78 full_flaps_stall_speed=70 cruise_speed=232 max_indicated_speed=259.00 [keyboard_response] elevator=150,250 aileron=150,250 rudder=150,250 [Views] eyepoint=-2.90, -1.30, 2.35 //(feet) longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800 autothrottle_available=0 pitch_takeoff_ga=8.000000 default_pitch_mode=0 default_bank_mode=0 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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 startup=fx_engstrt [direction_indicators] direction_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.03, -18.10, 0.25, fx_navred light.1=3, 0.03, 18.10, 0.25, fx_navgre light.2=2, 0.05, -18.15, 0.25, fx_strobe light.3=2, 0.05, 18.15, 0.25, fx_strobe light.4=1, -26.16, 0.00, 9.40, fx_beacon light.5=4, -1.40, 0.00, 2.00, fx_vclight light.6=3, -25.40, 0.00, 2.80, fx_navwhih [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 [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 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=4000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=3700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=3700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1900 ; 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