[fltsim.0] title=MC94-AN sim=MC94_AN model= panel=ANFIBIO sound= texture= kb_checklists= atc_id= ui_manufacturer=Macchi ui_type=MC94 ui_variation=Anphibiam atc_heavy=0 atc_airline= atc_flight_number= description=Designed as commercial amphibian,the MC.94 flew in 1935.The prototype had retractable wheels which swung forward into the leading edges of the wings and the tail gear swung up under the rudder.This non areodynamic solution was abbandoned and only six flying boat entered in production,serving with Ala Littoria [General] atc_type= atc_model= editable=1 performance=Length: 16.2 meters\n Wing span:22.8 meters\nCeiling:6,000 meters\nMax Speed:292 km/h\n TOW 8,200 Kg\n\nEngines:2 x Alfa Romeo 126-R.C.10, 550kW [WEIGHT_AND_BALANCE] max_gross_weight = 35420.000 empty_weight = 21000.000 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 =800.000000, 0.000000, 0.000000, 0.000000, Station 1 station_load.4 = 0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = 0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 120000.000 empty_weight_roll_MOI = 200000.000 empty_weight_yaw_MOI = 250000.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.1=0.000000, 0.000000, 0.000000, 0.000000, Station 2 [flight_tuning] cruise_lift_scalar =1.202 parasite_drag_scalar =2.200 induced_drag_scalar =2.200 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =2.002 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.512 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type = 0 Engine.0 = 6.000, -7.000, 4.000 Engine.1 = 6.000, 7.000, 4.000 fuel_flow_scalar = 1.000 min_throttle_limit=-0.250000 [piston_engine] power_scalar =1.000 cylinder_displacement= 120.000 compression_ratio= 8.000 number_of_cylinders= 18 max_rated_rpm= 2700.000 max_rated_hp= 1200.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 47.000 min_design_mp= 10.000 critical_altitude= 7000.000 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 [propeller] thrust_scalar =1.091 propeller_type= 0 propeller_diameter= 8.500 propeller_blades= 3 propeller_moi= 16.000 beta_max= 45.000 beta_min= 15.000 min_gov_rpm= 1100.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 0 min_rpm_for_feather= 700.000 beta_feather= 82.000 power_absorbed_cf= 0.900 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 // 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0 = 1.000, -29.800, 0.000, -2.900, 3200.000, 0.000, 1.100, 40.000, 0.273, 2.500, 0.450, 3.000, 3.000, 0.000, 0.000, 0.000 point.1 = 1.000, 9.900, -5.500, -8.600, 3200.000, 1.000, 2.400, 0.000, 0.513, 2.500, 0.540, 4.100, 4.300, 2.000, 0.000, 0.000 point.2 = 1.000, 9.900, 5.500, -8.600, 3200.000, 2.000, 2.400, 0.000, 0.513, 2.500, 0.540, 4.300, 4.100, 3.000, 0.000, 0.000 //SCRAPES point.3= 2.000, 0.000, -50.000, 7.000, 3200.000, 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, 0.000, 50.000, 7.000, 3200.000, 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, -43.000, 0.000, 2.000, 3200.000, 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, 21.000, 0.000, 0.000, 3200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch = 0.000 static_cg_height = 9.000 //floats point.7= 4.000, 0.100, -45.800, 0.000, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.8= 4.000, 0.100, 45.800, 0.000, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.9= 4.000, 14.000, 0.000, -5.700, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.10= 4.000, 14.000, 0.000, -5.700, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.11= 4.000, 14.000, 0.000, -5.700, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.12= 4.000, 14.000, 0.000, -5.700, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.13= 4.000, 14.000, 0.000, -5.700, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.14= 4.000, 14.000, 0.000, -5.700, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.15= 4.000, -4.000, -4.000, -4.800, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 point.16= 4.000, -4.000, 4.000, -4.800, 10000.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000 max_number_of_points=25 gear_system_type=0 [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [Views] eyepoint =18.00, -0.50, 2.35 //Longitudinal, Lateral, Vertical (feet) [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 4.10, -38.70, 6.50, fx_navredh , light.1 = 3, 4.10, 38.70, 6.50, fx_navgreh , light.3 = 2, 4.10, -38.70, 6.500, fx_strobeh , //rosso light.4 = 2, 4.10, 38.70, 6.50, fx_strobeh , //verde light.5 = 1, -26.60, 0.00, 10.30, fx_beaconh , light.7 = 4, 11.43, 0.00, 2.25, fx_vclight, light.8 = 3, -28.80, 0.00, 0.00, fx_navwhih , //white light.9 = 4, 18.40, -0.80, 2.40, fx_vclight , //cabin light.10= 4, 19.20, -0.80, 2.30, fx_vclight_yellow, //VC light.11= 3, 9.20, 7.50, 8.00, fx_sm95_scarico, //0 light.12= 3, 9.20, -7.50, 8.00, fx_sm95_scarico, //1 light.13= 4, 5.300, 0.00, 0.00, fx_vclight , light.14= 4, -2.00, 0.00, 0.00, fx_vclight , [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 = 150, 250 aileron = 150, 250 rudder = 150, 250 [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=3,0 [fuel] LeftMain = 0.000, -12.000, 0.000, 700.000, 0.000 RightMain = 0.000, 12.000, 0.000, 700.000, 0.000 fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [EFFECTS] wake= fx_wake_ss water=fx_waterland dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area = 1400.000 wing_span = 104.000 wing_root_chord = 13.000 wing_dihedral = 2.000 wing_incidence = 0.000 wing_twist = 0.000 oswald_efficiency_factor= 0.800 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = 2.500 wing_pos_apex_vert = 6.000 htail_area = 200.000 htail_span = 30.000 htail_pos_lon = -32.000 htail_pos_vert = 3.000 htail_incidence = 0.000 htail_sweep = 5.000 vtail_area = 100.000 vtail_span = 10.000 vtail_sweep = 20.000 vtail_pos_lon = -35.000 vtail_pos_vert = 7.500 elevator_area = 42.000 aileron_area = 50.000 rudder_area = 40.000 elevator_up_limit = 17.000 elevator_down_limit = 15.000 aileron_up_limit = 18.000 aileron_down_limit = 18.000 rudder_limit = 30.000 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 = 90.000 full_flaps_stall_speed = 70.000 cruise_speed = 155.000 max_indicated_speed=181.000000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 700.0 autothrottle_available= 0 pitch_takeoff_ga= 8.000 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 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 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 [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 [Tailhook] tailhook_length=1 tailhook_position=0.0, 0.0, 10.0 cable_force_adjust_1.0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 21.000 system_type= 0 damaging-speed= 196.000 blowout-speed= 214.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 flaps-position.4= 40.000, 0.000 flaps-position.5= 50.000, 0.000