[fltsim.0] title=P50_II sim=P50_II model= panel= sound= texture= kb_checklists= ui_manufacturer=Piaggio ui_type= P50 ui_variation= II-MM370 atc_heavy=0 atc_id= atc_airline= atc_flight_number= description=Notes:Prototype with 4 radial engines in traditional position\nfirst flight in 1938\nFather of the more famouse Piaggio P108B\nfor description see file [General] performance=Length: 64.11 ft\nSpan: 84.71 ft\nWeight: empty 29,040 lbs \nPower: 4 x Piaggio P XI RC40-1,000 hp each\nAverage climb rate to 13,100 ft in 15 min\nMax speed 279 mph. atc_type= atc_model= editable=1 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, -0.200 empty_weight_CG_position=0.000, 0.000, -0.200 max_number_of_stations=50 station_load.0= 0.000000,0.000000,0.000000,0.000000 ; upkeep weapon use 10000 lbs /station_load.1= 0.000000,0.000000,0.000000,0.000000 ; empty_weight_roll_MOI=388864.000 empty_weight_pitch_MOI=448839.000 empty_weight_yaw_MOI=629754.000 empty_weight_coupled_MOI=400.000 empty_weight=39000.000 max_gross_weight=65000.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [tailhook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=1.0 [folding_wings] wing_fold_system_type =1 ;0=None fold_rates = 0.12,0.11 [flight_tuning] cruise_lift_scalar=1.50 parasite_drag_scalar=3.00 induced_drag_scalar=3.00 elevator_effectiveness=1.000 aileron_effectiveness=1.250 rudder_effectiveness=1.000 pitch_stability=1.700 roll_stability=1.000 yaw_stability=1.100 elevator_trim_effectiveness=1.750 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Reference Speeds] ;TAS flaps_up_stall_speed=95.000 full_flaps_stall_speed=76.000 cruise_speed=138.00 ; Heavily loaded cruise_speed=150.00 ; lightly loaded max_indicated_speed=274.765625 [GeneralEngineData] engine_type=0 Engine.0=14.167, -24.583, 0.000 Engine.1=15.833, -11.833, 0.000 Engine.2=15.833, 11.833, 0.000 Engine.3=14.167, 24.583, 0.000 fuel_flow_scalar=1.288 min_throttle_limit=0.000000 [piston_engine] cylinder_displacement=137.400000 compression_ratio=6.000000 number_of_cylinders=12 max_rated_rpm=3000.000000 turbocharged=1 min_design_mp=1.000000 emergency_boost_type=1 emergency_boost_mp_offset=1.000000 emergency_boost_gain_offset=1.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=12.0350000 fuel_air_auto_mixture=1 auto_ignition=0 max_rpm_friction_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.00000 idle_rpm_friction_scalar=1.000000 //================================== max_rated_hp=1460.000 power_scalar=0.562 max_design_mp=52.5000000 ;58.4-5.9 lost due to altitude critical_altitude=6000 ; M Gear max_rpm_mechanical_efficiency_scalar=1.1372 [fuel] RightMain= 0.000000,0.000000,0.000000,1392.000000,0.000000 ;#1 LeftMain= 0.000000,0.000000,0.000000,920.000000,0.000000 ;DB #2 fuel_type=1.000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=1301.000 wing_span=102.000 wing_root_chord=12.750 wing_dihedral=4.999 wing_incidence=0.000 wing_twist=0.500 oswald_efficiency_factor=5.007 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=237.000 htail_span=45.000 htail_pos_lon=-41.667 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=248.000 vtail_span=17.956 vtail_sweep=0.000 vtail_pos_lon=-42.333 vtail_pos_vert=1.500 elevator_area=101.910 aileron_area=130.100 rudder_area=86.800 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=59.989 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=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) point.0=1.000, -35.917, 0.000, -5.333, 1574.803, 0.000, 0.862, 55.860, 0.340, 2.500, 0.708, 15.000, 10.000, 0.000, 0.000, 0.000 point.1=1.000, 5.917, -11.917, -10.333, 1574.803, 1.000, 0.862, 0.000, 0.453, 2.500, 0.708, 15.000, 10.000, 2.000, 0.000, 0.000 point.2=1.000, 5.917, 11.917, -10.333, 1574.803, 2.000, 0.862, 0.000, 0.453, 2.500, 0.708, 15.000, 10.000, 3.000, 0.000, 0.000 point.3=2.000, -2.833, -50.583, 3.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -2.833, 50.583, 3.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -35.917, 0.000, -4.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 23.833, 0.000, -2.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=6.800 static_cg_height= 9.3000 static_pitch=6.900 static_cg_height= 9.5000 gear_system_type=0 [propeller] propeller_type=0 propeller_diameter=10.333 propeller_blades=3 thrust_scalar=2.100 propeller_moi=28.963 beta_max=49.000 beta_min=15.000 min_gov_rpm=600.000 prop_tc=0.100 gear_reduction_ratio=1.300 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 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 [electrical] electric_always_available=1 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit // x, z, y light.0=4,22.46,-0.50,-1.30, fx_vclight_s403.fx [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] //eyepoint=22.46,-1.10,-1.30 eyepoint=22.46,-0.50,-1.30 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=500.000 autothrottle_available=0 pitch_takeoff_ga=8.000 use_no_default_bank=1 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 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=0 Com.1=1, 0 Com.2=0, 0 Nav.1=1, 0, 1 Nav.2=0, 0, 1 ; with glide slope, not activated for PD Lancaster Adf.1=1 Adf.2=0 Transponder.1=1 Marker.1=1 [Flaps.0] type=1 span-outboard=0.500 extending-time=8.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=0.900 drag_scalar=1.000 flaps-position.0 = 0 flaps-position.1 = 8, 200 flaps-position.2 = 20, 200 flaps-position.3 = 30, 180 flaps-position.4 = 42, 150 [direction_indicators] direction_indicator.0=1,0 [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 [brakes] toe_brakes_scale=1.0000 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 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