[fltsim.0] title=BA88 FIGHTER sim=BA88_F model= panel= sound= texture= kb_checklists= ui_manufacturer=Breda ui_type=BA88 ui_variation=Fighter description=History of the aircarft: see description in main folder\nThis model: 7°gruppo,5° stormo Regia Aeronautica, based at Castel Benito (Libia) during 1940\n [fltsim.1] title=BA88 TRAINER sim=BA88_T model=T panel= sound= texture=T kb_checklists= ui_manufacturer=Breda ui_type=BA88 ui_variation=Trainer description=History of the aircarft: see description in main folder\nThis aircarft: training unit in Lonate Pozzolo (Varese) during 1936\n [WEIGHT_AND_BALANCE] empty_weight= 13068.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=170.000000, -3.000000, 0.000000, 3.000000, longitudinal empty_weight_roll_MOI=80989.000000 empty_weight_pitch_MOI=102454.000000 empty_weight_yaw_MOI=190603.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=19857.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1 = 3, -1.14, -25.88, 0.0, fx_navred light.2 = 3, -1.14, 25.88, 0.0, fx_navgre light.3=4, 0.95, 9.65, -4.50 , fx_sm95_scarico //dx eng 0 light.4=4, 0.95, 5.60, -4.50, fx_sm95_scarico //sx eng 0 light.5=4, 0.95,-5.60, -4.50, fx_sm95_scarico //dx eng 1 light.6=4, 0.95,-9.65, -4.50, fx_sm95_scarico //sx eng 1 light.7=4, 1.30,0.00,0.100, fx_vclight_YELLOW //cabina [Moments of Inertia] empty_weight_pitch_MOI= 23052.000 empty_weight_roll_MOI= 15602.000 empty_weight_yaw_MOI= 30691.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 19857.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =0.701 rudder_effectiveness =1.000 pitch_stability =0.701 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [piston_engine] //power_scalar =0.954 power_scalar =1 cylinder_displacement= 130.700 compression_ratio= 6.000 number_of_cylinders= 14 max_rated_rpm= 2400.000 max_rated_hp= 840.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 46.000 min_design_mp= 1.000 critical_altitude= 17000.000 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 [propeller] thrust_scalar=1.000 rotation= -1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW propeller_type= 0 propeller_diameter= 9.500 propeller_blades= 3 propeller_moi= 23.000 beta_max= 45.000 beta_min= 25.000 min_gov_rpm= 1800.000 prop_tc= 0.010 gear_reduction_ratio= 1.710 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 1 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 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [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, -19.580, 0.000,-6.00, 1574.800, 0.000, 0.190, 30.900, 0.150, 2.500, 1.020, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, 2.500, -10.410, -9.000, 1574.800, 1.000, 0.590, 0.000, 0.210, 2.500, 1.010, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, 2.500, 10.410, -9.000, 1574.800, 2.000, 0.590, 0.000, 0.210, 2.500, 1.010, 5.000, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.660, -34.160, -3.910, 1574.800, 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, 0.660, 34.160, -3.910, 1574.800, 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, -38.660, 0.000, -3.830, 1574.800, 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, 15.910, -0.080, -3.000, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 11.124 static_cg_height= 8.600 gear_system_type= 0 tailwheel_lock = 0 [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 [Views] eyepoint=0.40,0.000000,0.75 [fuel] LeftMain= 0.000, -4.200, 0.300, 110.000, 0.000 RightMain= 0.000, 4.200, 0.300, 110.000, 0.000 fuel_type= 1.000 number_of_tank_selectors= 1 electric_pump= 0 [airplane_geometry] wing_area= 529.000 wing_span= 51.167 wing_root_chord= 8.083 wing_dihedral= 5.999 wing_incidence= 0.000 wing_twist= 1.000 oswald_efficiency_factor= 0.726 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 77.000 htail_span= 17.167 htail_pos_lon= -24.250 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 37.000 vtail_span= 6.935 vtail_sweep= 0.000 vtail_pos_lon= -24.250 vtail_pos_vert= 10.667 elevator_area= 31.810 aileron_area= 22.900 rudder_area= 13.950 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 [brakes] toe_brakes_scale= 1.000 parking_brake= 1 [gear_warning_system] gear_warning_available= 0 pct_throttle_limit= 0.000 flap_limit_power= 0.000 flap_limit_idle= 0.000 [GeneralEngineData] engine_type= 0 Engine.0= 8.333, -9.167, -1.250 Engine.1= 8.333, 9.167, -1.250 fuel_flow_scalar= 1.000 min_throttle_limit= 0.000 [Reference Speeds] flaps_up_stall_speed= 70.000 full_flaps_stall_speed= 56.000 cruise_speed= 238.000 max_indicated_speed= 265.00 [keyboard_response] elevator= 150.000, 250.000 aileron= 150.000, 250.000 rudder= 150.000, 250.000 [General] performance=Length: 10.60 m\nSpan: 15.6 m\nWeight: 6750 kg\nPower: 2 x 1000 hp Piaggio P.XI RC 40\nRange: 1800 km\nCeiling: 8500m\nmax speed :490km/h\n cruise speed:440 km/h\nmin speed: 110km/h\n atc_type= atc_model= [autopilot] autopilot_available= 1 flight_director_available= 0 default_vertical_speed= 700.000 autothrottle_available= 0 pitch_takeoff_ga= 8.000 max_pitch= 10.000 max_pitch_acceleration= 1.000 max_pitch_velocity_lo_alt= 2.000 max_pitch_velocity_hi_alt= 1.500 max_pitch_velocity_lo_alt_breakpoint= 20000.000 max_pitch_velocity_hi_alt_breakpoint= 28000.000 max_bank= 25.000 max_bank_acceleration= 1.800 max_bank_velocity= 3.000 max_throttle_rate= 0.100 nav_proportional_control= 9.000 nav_integrator_control= 0.250 nav_derivative_control= 0.000 nav_integrator_boundary= 2.500 nav_derivative_boundary= 0.000 gs_proportional_control= 9.520 gs_integrator_control= 0.260 gs_derivative_control= 0.000 gs_integrator_boundary= 0.700 gs_derivative_boundary= 0.000 yaw_damper_gain= 0.000 [hydraulic_system] electric_pumps= 0 engine_map= 1, 1, 0, 0 normal_pressure= 6.931 [stall_warning] type= 1 [attitude_indicators] attitude_indicator.0= 1 [turn_indicators] turn_indicator.0= 1, 0 [Flaps.0] type= 1 span-outboard= 0.125 extending-time= 5.000 system_type= 0 damaging-speed= 191.000 blowout-speed= 290.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 25.000, 0.000 flaps-position.2= 50.000, 0.000 [direction_indicators] direction_indicator.0=1,0
