[fltsim.0] title=Beechcraft C-45F IAF sim=C45FIAF model= panel= sound= texture= kb_checklists=C45FIAF_check kb_reference=C45FIAF_ref kb_notes=C45FIAF_notes atc_id= ui_manufacturer=Beechcraft ui_type=C-45F IAF ui_variation=46 Stormo description=This Beech C45 F was one of 27 that , at the end of WWII, USAF, from an air base in Germany, sended in Italy and repainted with the colours of the new Italian Air Forces. Entered in service in July 1950 with the 46°stormo in Pisa AB. [General] atc_type= atc_model= editable=1 performance=DIMENSIONS:\nWing span: 49 ft 8 in / 15.14 m.\nLength: 35 ft 3 in / 10.7 m\nHeight: 9 ft 4 in / 2.84 m.\n\nWEIGHTS:\nEmpty equipped: 5,845 lb / 2,650 kg\nMax. takeoff: 9,900 lb / 4,490 kg\n\nPERFORMANCE:\nMax. cruising speed: 191 kt / 354 kph\nEconomical cruise: 160 kt / 298 kph\nInitial climb: 1,400 ft per min.\nService ceiling: 21,400 ft\nRange: 1,330 nm / 2,460 km with maximum fuel\n [WEIGHT_AND_BALANCE] max_gross_weight = 9900.000 empty_weight = 5845.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 1.870, 0.000, 0.000 max_number_of_stations =50 station_load.0 = 170, 3.94, -0.98, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170, 3.94, 0.98, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 170, 1.44, -1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 170, 1.44, 1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 170, -1.97, -1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 170, -1.97, 1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = 170, -4.92, -1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = 170, -4.92, 1.31, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = 900, -7.48, 0.00, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 11500.000 empty_weight_roll_MOI = 10500.000 empty_weight_yaw_MOI = 22000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.500 parasite_drag_scalar =1.300 induced_drag_scalar =1.300 elevator_effectiveness =0.500 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [GeneralEngineData] engine_type = 0 Engine.0 = 6.60, -6.600, 0.000 Engine.1 = 6.60, 6.600, 0.000 fuel_flow_scalar = 1.00 min_throttle_limit = 0.00 //Minimum percent throttle. Generally negative for turbine reverser master_ignition_switch = 1 //Master Ignition Switch [piston_engine] power_scalar =0.954 cylinder_displacement= 108.110 compression_ratio= 6.300 number_of_cylinders= 9 max_rated_rpm= 2250.000 max_rated_hp= 450.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 47.000 min_design_mp= 0.000 min_design_mp= 1.000 critical_altitude= 12000.000 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=0.600 idle_rpm_friction_scalar=2.200 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 [propeller] thrust_scalar =0.954 propeller_type= 0 propeller_diameter= 8.260 propeller_blades= 2 propeller_moi= 24.000 beta_max= 86.000 beta_min= 13.000 min_gov_rpm= 600.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 0.000 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 [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, -19.137, 0.000, -1.500, 1600, 0, 0.633, 40, 0.52, 2.5, 1.0, 3.0, 3.0, 0, 152, 180 point.1 = 1, 3.543, -6.437, -6.250, 1600, 1, 0.886, 0, 0.60, 2.5, 1.0, 7.1, 7.3, 2, 152, 200 point.2 = 1, 3.543, 6.437, -6.250, 1600, 2, 0.886, 0, 0.60, 2.5, 1.0, 7.1, 7.3, 2, 152, 200 //SCRAPES point.3= 2, -0.69, -23.79, 0.59, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4= 2, -0.69, 23.79, 0.59, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5= 2, -20.60, -7.58, 0.66, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6= 2, -20.60, 7.58, 0.66, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.7= 2, 11.02, 0.00, 0.23, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch = 12.283 static_cg_height = 5.062 gear_system_type=0 tailwheel_lock = 1 [Views] eyepoint = 3.812, -1.211, 2.333 //Longitudinal, Lateral, Vertical (feet) [gear_warning_system] gear_warning_available = 0 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.65 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 732.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 5.00, 0.00, 2.25, fx_vclight //fuse light.1 = 4, 0.00, 0.00, 2.25, fx_vclight //vcfuse avanti //light.2 = 4, -3.50, 0.00, 2.25, fx_vclight //vcfuse dietro light.3 = 3, 2.50, -25.00, 0.20, fx_navred light.4 = 3, 2.95, 25.00, 0.20, fx_navgre light.5=2, 2.50, -25.00, 0.20 , fx_strobe //strobe rosso light.6=2, 2.95, 25.00, 0.20, fx_strobe //strobe verde light.7=1, -16.57,0.00,2.85, fx_beaconh //beacon light.8=2, 0.0,0.0,-2.74, fx_strobe //strobe sotto light.9=4, 10.0,0.00,1.55, fx_vclight_yellow //cabina light.10=4, 4.40,0.00,1.67,fx_vclight //vccabin light.11=3,-20.0,0.0,2.28, fx_navwhi //bianco [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 Adf.2 = 1 Transponder.1 = 1 Marker.1 = 1 [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 =200, 1000 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=1,0 direction_indicator.1=2,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=2,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt_jenny touchdown=fx_tchdwn_s, 1 [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, 5 , 17.0 //avionics = 1, 5 , 17.0 //pitot_heat = 0, 2 , 17.0 //additional_system = 0, 2 , 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 //starter2 = 0, 20, 17.0 //starter3 = 0, 20, 17.0 //starter4 = 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 max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 100 [fuel] Center1 = 6.0, 0.00, 0.0, 77.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = 0.0, -10.83, 0.0, 76.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = 0.0, 10.83, 0.0, 76.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = 0.0, -3.30, 0.0, 23.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = 0.0, 3.30, 0.0, 23.0, 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 [airplane_geometry] wing_area = 360.700 wing_span = 49.670 wing_root_chord = 11.083 wing_dihedral = 6.000 wing_incidence = 3.920 wing_twist = -3.530 oswald_efficiency_factor= 0.650 wing_winglets_flag = 0 wing_sweep = 13.220 wing_pos_apex_lon = 6.370 wing_pos_apex_vert = 0.000 htail_area = 87.330 htail_span = 14.970 htail_pos_lon = -16.730 htail_pos_vert = 2.460 htail_incidence = 0.000 htail_sweep = 13.810 vtail_area = 43.600 vtail_span = 5.420 vtail_sweep = 14.000 vtail_pos_lon = -18.560 vtail_pos_vert = 2.460 elevator_area = 34.930 aileron_area = 24.700 rudder_area = 21.800 elevator_up_limit = 35.000 elevator_down_limit = 25.000 aileron_up_limit = 38.500 aileron_down_limit = 21.000 rudder_limit = 25.000 elevator_trim_limit = 15.000 spoiler_limit = 0.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 67.500 full_flaps_stall_speed = 61.500 cruise_speed = 160.000 max_indicated_speed = 280 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 1 pitch_takeoff_ga=0.0 default_vertical_speed=700.000000 autothrottle_available=0 direction_indicator=1 attitude_indicator =1 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 = 0.0 default_bank_mode=2 //Default to Heading Hold [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 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=3500000 ; in microseconds [stall_warning] type=2 [exits] number_of_exits = 5 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 exit_rate.2 = 0.4 exit_rate.3 = 0.4 exit_rate.4 = 0.4 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 7.000 system_type= 0 damaging-speed= 180.000 blowout-speed= 225.000 lift_scalar= 0.500 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 5.000, 0.000 flaps-position.2= 10.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000 flaps-position.7= 35.000, 0.000 flaps-position.8= 40.000, 0.000 flaps-position.9= 45.000, 0.000 [SMOKESYSTEM] // dark engine smoke by the smoke key smoke.0=-3.44, 4.18, 9.30, fx_smoke_rx smoke.1=-3.44, 4.18, -9.30, fx_smoke_rx