[fltsim.0] title=mpma_short sim=short1 model= panel= sound= texture= panel_alias=beech_king_air_350\panel sound_alias=beech_king_air_350\sound kb_checklists= kb_reference= atc_id_color=0xffffffffff atc_id=NTETP ui_manufacturer=AS Engineering ui_type=Multipurpose Aircraft with Modular Fuselage ui_variation=without container description=Multipurpose Aircraft with Modular Fuselage\nFlight Model Author: Curro Perez atc_heavy=0 atc_airline=Global Freightways atc_flight_number= [General] atc_type=EXPERIMENTAL atc_model= performance=Longitud total: 23.3 m.\nEnvergadura: 26.3 m.\nAltura total: 7.5 m.\nLongitud cockpit: 4.4 m.\nLongitud rampa: 6.5 m.\nMotores: 2 x 8000 Turboprop\nCombustible: 1400 US Gallons\nPeso Max.: 18.000 Kg. [WEIGHT_AND_BALANCE] max_gross_weight= 26800.000 empty_weight= 17520.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= -3.800, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 5.000, -2.000, 0.000 station_load.1= 170.000, 5.000, 2.000, 0.000 station_load.2= 170.000, -2.100, -2.000, 0.000 station_load.3= 170.000, -2.100, 2.000, 0.000 station_load.4= 170.000, -5.300, -2.000, 0.000 station_load.5= 170.000, -5.300, 2.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 78765.000 empty_weight_roll_MOI= 86437.000 empty_weight_yaw_MOI= 159624.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 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 [GeneralEngineData] engine_type= 5 Engine.0= 5.500, -17.000, 1.600 Engine.1= 5.500, 17.000, 1.600 fuel_flow_scalar= 1.000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 12.000 propeller_blades= 4 propeller_moi= 60.000 beta_max= 45.000 beta_min= 15.200 min_gov_rpm= 25520.000 prop_tc= 0.004 gear_reduction_ratio= 17.600 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= 1 min_rpm_for_feather= 700.000 beta_feather= 79.300 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 29920.000 static_thrust= 150.000 afterburner_available= 0 [turboprop_engine] power_scalar=1.000 maximum_torque= 8000.000 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 [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 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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) [contact_points] point.0= 1.000, 28.800, 0.000, -8.500, 1181.000, 0.000, 0.596, 39.900, 0.296, 2.500, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000 point.1= 1.000, -6.500, -11.500, -8.500, 1574.000, 1.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000 point.2= 1.000, -6.500, 11.500, -8.500, 1574.000, 2.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000 point.3= 2.000, -4.600, -42.640, 3.930, 787.000, 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, -4.600, 42.640, 3.930, 787.000, 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, -44.200, 0.000, 4.900, 787.000, 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, -25.000, 0.000, -4.200, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -1.000 static_cg_height= 4.300 [Views] eyepoint=4.54, -1.20, 3.25 [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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.56, -28.41, 1.97, fx_navred , light.1=3, 0.56, 28.41, 1.97, fx_navgre , light.2=3, -31.20, 0.00, 9.09, fx_navwhi , light.3=2, 0.89, -27.89, 1.77, fx_strobe , light.4=2, 0.89, 27.89, 1.77, fx_strobe , light.5=1, -25.49, 0.00, 9.74, fx_beacon , light.6=2, -4.55, 0.00, -1.85, fx_strobe , light.7=4, 5.91, 0.00, 1.64, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= 2.600, -13.000, 4.000, 700.000, 0.000 LeftAux= 2.600, -13.000, 4.000, 10.000, 0.000 RightMain= 2.600, 13.000, 4.000, 700.000, 0.000 RightAux= 2.600, 13.000, 4.000, 10.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 700.000 wing_span= 86.000 wing_root_chord= 11.000 wing_dihedral= 1.000 wing_incidence= 1.000 wing_twist= -1.500 oswald_efficiency_factor= 0.700 wing_winglets_flag= 1 wing_sweep= 9.000 wing_pos_apex_lon= 1.600 wing_pos_apex_vert= 4.200 htail_area= 178.000 htail_span= 27.000 htail_pos_lon= -36.000 htail_pos_vert= 4.200 htail_incidence= 0.500 htail_sweep= 9.000 vtail_area= 180.000 vtail_span= 13.000 vtail_sweep= 18.000 vtail_pos_lon= -32.000 vtail_pos_vert= 10.000 elevator_area= 78.000 aileron_area= 28.000 rudder_area= 14.000 elevator_up_limit= 27.000 elevator_down_limit= 20.000 aileron_up_limit= 18.000 aileron_down_limit= 18.000 rudder_limit= 20.000 elevator_trim_limit= 19.000 spoiler_limit= 60.000 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= 96.000 full_flaps_stall_speed= 76.800 cruise_speed= 315.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=0 pitch_takeoff_ga=8.000 [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 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 20.000, 0.000 flaps-position.2= 40.000, 0.000