[fltsim.0] title=Bonanza A35 sim=Bonanza 35 model= panel= sound= texture= kb_checklists=1948-35-Check-list description=The famous V-tailed Bonanza.. This model is a 1948 (A35), manufactured during the second year of production. This model was identical to the Straight 35 of 1947 with one exception, a the steeralbe nose wheel. The Bonanza came was the first airplane of its time to come fully equipped for both day and night VFR flight as well as instrument flying from the factory. The 35 is a 4 seat configuration, a 2550 lb gross weight (1558 lb EW and a 185 hp engine. The designed cruise speed is 160 mph with a reasonable fuel flow of 10 gph, although the ad's of the day claimed a cruise speed as much as 184 mph. ui_manufacturer=VFD-BeechCraft ui_type=Bonanza ui_variation=1948-35 atc_heavy=0 atc_id= atc_airline= atc_flight_number performance=Cruise Speed\t160 mph\nMaximum Range\t750 statute miles\nService Ceiling\t17,100 ft\nMax Gross Weight\t2,650 lb\nSeating\t\t4\nUseful Load\t1,070 lb\n [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [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=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [GeneralEngineData] engine_type= 0 Engine.0= 8.333, -0.100, 0.000 fuel_flow_scalar= 0.900 min_throttle_limit=0.005000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 7.330 propeller_blades= 2 propeller_moi= 5.000 beta_max= 43.000 beta_min= 15.000 min_gov_rpm= 1100.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 20.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0.000 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [piston_engine] power_scalar=1.000 cylinder_displacement= 91.667 compression_ratio= 7.100 number_of_cylinders= 6 max_rated_rpm= 2300.000 max_rated_hp= 185.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [flight_tuning] pitch_stability=1.111 roll_stability=1.000 yaw_stability=1.101 parasite_drag_scalar=0.910 induced_drag_scalar=1.059 elevator_effectiveness=0.669 aileron_effectiveness=1.250 rudder_effectiveness=0.893 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.500 rudder_trim_effectiveness =1.000 cruise_lift_scalar=1.000 [WEIGHT_AND_BALANCE] max_gross_weight= 2550.000 empty_weight= 1558.000 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position= 0.350, 0.000, 0.000 max_number_of_stations=50 station_load.0=200.000000, -0.500000, -1.200000, 0.000000, Pilot station_load.1=200.000000, -0.500000, 1.200000, 0.000000, Front Passenger station_load.2=160.000000, -3.250000, -1.200000, 0.000000, Left Mid Psgr station_load.3=160.000000, -3.250000, 1.200000, 0.000000, Right Mid Psgr station_load.6="80.000000,-5.00000,0.000000,0.000000, cargo" //120lb capacity empty_weight_roll_MOI= 1677.000 empty_weight_pitch_MOI= 2081.000 empty_weight_yaw_MOI= 3468.000 empty_weight_coupled_MOI= 60.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.4=0.000000, 0.000000, 0.000000, 0.000000, Station 5 [fuel] LeftMain= 0.250, -13.333, 0.000, 20.000, 17.000 RightMain= 0.250, 13.333, 0.000, 20.000, 17.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area= 178.000 wing_span= 32.800 wing_root_chord= 5.400 wing_dihedral= 5.999 wing_incidence= 3.000 wing_twist= -0.994 oswald_efficiency_factor= 1.4 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 1.229 wing_pos_apex_vert= 0.000 htail_area= 40.000 htail_span= 11.167 htail_pos_lon= -14.583 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 24.000 vtail_span= 5.586 vtail_sweep= 0.000 vtail_pos_lon= -13.083 vtail_pos_vert= 1.500 elevator_area= 17.200 aileron_area= 18.100 rudder_area= 6.650 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 90.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [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 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 0, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [contact_points] point.0= 1.000, 6.583, 0.000, -4.480, 1574.803, 0.000, 0.525, 34.740, 0.350, 2.500, 0.850, 3.000, 4.500, 0.000, 0.000, 0.000 point.1= 1.000, -1.400, -4.833, -4.450, 1574.803, 1.000, 0.525, 0.000, 0.360, 2.500, 0.900, 5.000, 7.200, 2.000, 0.000, 0.000 point.2= 1.000, -1.400, 4.833, -4.450, 1574.803, 2.000, 0.525, 0.000, 0.360, 2.500, 0.900, 5.000, 7.200, 3.000, 0.000, 0.000 point.3 = 2, -16.530, 0.061, -1.265, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.4 = 2, 7.004, -0.053, -1.064, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.5 = 2, 0.903, 17.674, -0.381, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.6 = 2, 0.905, -17.967, -0.369, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.7 = 2, -16.530, 0.061, -1.265, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.8 = -0.50, 5.50, -4.23, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.9 = -0.50, -5.57, -4.23, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.10 = 6.30, 0.00, -4.23, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.11 = -0.50, 5.50, -4.23, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 point.12 = -0.50, -5.57, -4.23, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0 static_pitch = .1345 //degrees (pitch when loaded on ground) static_cg_height = 4.318 //feet, altitude of CG when at rest on the ground gear_system_type = 0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit , 5=landing light.1 = 2 , -17.7600 , 0.000000 , 0.0400, fx_strobe , light.4 = 3 , 0.970000 , 17.799000 , 0.107000 , fx_navgre , light.5 = 3 , 0.97000 , -17.799900 , -0.059243 , fx_navred , light.8 = 4 , -0.59, 0.00, 2.43, fx_vclight [Reference Speeds] flaps_up_stall_speed= 64.000 full_flaps_stall_speed= 55.000 cruise_speed= 160 max_indicated_speed=200.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint= -1.065000, -0.806000, 1.083000 , //(feet) longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=000.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [direction_indicators] direction_indicator.0=1,0 [brakes] toe_brakes_scale=0.700000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=15.996982 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [General] performance=\nCruise Speed\t160 mph\nMaximum Range\t750 sm\nService Ceiling\t15,000 ft\nMax Gross Weight\t2,550 lb\nSeating\t\t4\nUseful Load\t1,092 lb\n atc_type=BEECH AIRCRAFT atc_model=Bonanza [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 110.000 blowout-speed= 125.000 lift_scalar= 1.250 drag_scalar= 1.300 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.331, 0.000 flaps-position.2= 20.662, 0.000
