[fltsim.0] title=Emb 110P FAB sim=Emb 110P model=P panel= sound= texture=FAB description=The EMB-110 Bandeirante is a non-pressurized, Aircraft designed for short-haul passenger and cargo transport. It is powered by two Pratt & Whitney PT6A-34 turboprop engines rated at 750 shp. The EMB-110 can operate from unprepared airstrips without ground support equipment. ui_manufacturer=Embraer ui_type=Emb 110 P ui_variation=Forca Aerea Brasileira kb_checklists=Emb_110P_check.htm kb_reference=Emb_110P_ref.htm atc_id=2154 atc_airline=Air Force atc_flight_number=2154 atc_heavy=0 [fltsim.1] title=Emb 110P HAS sim=Emb 110P model=P panel= sound= texture=HAS description=The EMB-110 Bandeirante is a non-pressurized, Aircraft designed for short-haul passenger and cargo transport. It is powered by two Pratt & Whitney PT6A-34 turboprop engines rated at 750 shp. The EMB-110 can operate from unprepared airstrips without ground support equipment. ui_manufacturer=Embraer ui_type=Emb 110 P ui_variation=Harolds Air Service kb_checklists=Emb_110P_check.htm kb_reference=Emb_110P_ref.htm atc_id=N605W atc_airline=Harolds Air atc_flight_number= atc_heavy=0 [General] atc_type=Bandeirante atc_model=110 editable=1 performance=Cruise Speed\nNorm 205 kts\t236 mph 379 km\/h\nMax 223 kts\t257 mph\t 413 km\/h\n\nEngines\t\nPratt & Whitney PT6A-34 750 shp\n\nMaximum Range\t\n1,080 nm 1,243 m\t 2,001 km\n\nService Ceiling\t\n26,000 ft 8,000 m\n\nFuel Capacity\t\n454.4 U.S. gal 1,720 L\n\nMaximum Takeoff Weight \n12,489 lb\t 5,670 kg\n\nLength\t\n53.5 ft\t 15.1 m\n\nWingspan\t\n50.3 ft\t 15.33 m\n\nHeight\t\n16.1 ft\t 4.92 m\n\nSeating\t\nUp to 18\n\nUseful Load\t\n4,745 lb\t 2,154 kg [WEIGHT_AND_BALANCE] max_gross_weight = 12489.000 empty_weight = 6348.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations = 20 station_load.0 =340.00, 9.00, 0.00, 0.00, Pilot & co-pilo station_load.1 =510.00, 5.20, 0.00, 0.00, Passenger station_load.2 =510.00, 2.50, 0.00, 0.00, Passenger station_load.3 =510.00, 0.00, 0.00, 0.00, Passenger station_load.4 =510.00, -2.50, 0.00, 0.00, Passenger station_load.5 =510.00, -5.00, 0.00, 0.00, Passenger station_load.6 =510.00, -7.50, 0.00, 0.00, Passenger station_load.7 =285.00, -9.60, 0.00, 0.00, Baggage ;Moments of Inertia empty_weight_pitch_MOI = 23654.000 empty_weight_roll_MOI = 10822.000 empty_weight_yaw_MOI = 26204.000 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 =0.951 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 = 7.500, -8.100, 0.000 Engine.1 = 7.500, 8.100, 0.000 fuel_flow_scalar = 0.560 min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar =1.000 propeller_type = 0 propeller_diameter = 7.960 propeller_blades = 3 propeller_moi = 15.000 beta_max = 58.000 beta_min = 15.200 min_gov_rpm = 15520.000 prop_tc = 0.004 gear_reduction_ratio = 14.200 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 = 86.800 power_absorbed_cf = 0.900 defeathering_accumulators_available= 1 prop_reverse_available = 1.000 minimum_on_ground_beta = 1.000 minimum_reverse_beta = -14.000 [TurbineEngineData] fuel_flow_gain = 0.011 inlet_area = 1.000 rated_N2_rpm = 33000.000 static_thrust = 393.000 afterburner_available = 0 [turboprop_engine] power_scalar =1.000 maximum_torque = 2384.160 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, 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, 55, 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= 1.00, 16.20, 0.00, -5.61, 1181.00, 0.00, 0.50, 60.00, 0.30, 2.50, 0.952, 4.80, 4.80, 0.00, 180.00, 185.00 point.1= 1.00, -1.67, -8.58, -5.83, 1574.00, 1.00, 0.59, 0.00, 0.64, 2.50, 0.815, 4.50, 5.20, 2.00, 180.00, 185.00 point.2= 1.00, -1.67, 8.58, -5.83, 1574.00, 2.00, 0.59, 0.00, 0.64, 2.50, 0.815, 4.80, 4.90, 3.00, 180.00, 185.00 point.3= 2.00, 0.00, -26.10, 1.46, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4= 2.00, 0.00, 26.10, 1.46, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5= 2.00, -24.70, 0.00, -0.50, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.6= 2.00, 23.55, 0.00, -1.65, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 point.7= 2.00, 3.50, -8.10, -3.05, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 point.8= 2.00, 3.50, 8.10, -3.05, 787.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 static_pitch = 0.400 static_cg_height = 5.480 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.95 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = 13.70, -1.18, 2.55 //for model C = 9.70, -1.18, 2.55 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Audio.2 = 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 = 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 [airspeed_indicators] //airspeed_indicator.0 = 1.060, -2.00 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.06, -26.10, 1.52, fx_navred , light.1 = 3, 0.06, 26.10, 1.52, fx_navgre , light.2 = 3, -27.30, 0.00, 2.10, fx_navwhi , light.3 = 2, 0.04, -26.10, 1.52, fx_strobe , light.4 = 2, 0.04, 26.10, 1.52, fx_strobe , light.5 = 1, -26.10, 0.00, 12.45, fx_beacon , light.6 = 1, -8.17, 0.00, -2.21, fx_beacon , light.7 = 2, -27.30, 0.00, 2.10, fx_strobe , light.8 = 4, 10.75, 0.00, 1.75, fx_vclight, light.9 = 5, 1.23, -16.63, 0.40, fx_landing light.10= 5, 1.23, 16.63, 0.40, fx_landing [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain = 0.000, -4.500, 0.000, 227.200, 7.100 RightMain = 0.000, 4.500, 0.000, 227.200, 7.100 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 306.000 wing_span = 50.300 wing_root_chord = 6.600 wing_dihedral = 6.000 wing_incidence = 1.000 wing_twist = -1.500 oswald_efficiency_factor= 0.700 wing_winglets_flag = 0 wing_sweep = 1.000 wing_pos_apex_lon = 2.100 wing_pos_apex_vert = 0.000 htail_area = 122.000 htail_span = 26.200 htail_pos_lon = -23.800 htail_pos_vert = 0.000 htail_incidence = 0.500 htail_sweep = 3.000 vtail_area = 60.100 vtail_span = 9.400 vtail_sweep = 20.000 vtail_pos_lon = -24.000 vtail_pos_vert = 4.200 elevator_area = 52.000 aileron_area = 15.200 rudder_area = 24.220 elevator_up_limit = 19.000 elevator_down_limit = 16.500 aileron_up_limit = 18.000 aileron_down_limit = 15.000 rudder_limit = 28.000 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 = 96.000 full_flaps_stall_speed = 76.800 cruise_speed = 223.000 max_mach = 0.58 max_indicated_speed = 263 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 700.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [forcefeedback] stick_shaker_magnitude=3000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=2000 ; 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=5000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=5000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 [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= 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