[fltsim.0] title=EMB-120 Luxair sim=EMB120nb model= panel= sound= texture= kb_checklists= description=Embraer EMB-120ER for FS2002\nAircraft by Nick Botamer\/PROJECT ERJ\nhttp:\/\/www.project-erj.com\nFlight Model by Sam Chin\/Nick Botamer\nCopyright 2003, All Rights Reserved. ui_manufacturer=Embraer ui_type=EMB-120 ui_variation=Luxair atc_airline=Luxair atc_id=LX-LGM atc_flight_number= atc_heavy=0 [General] performance=MTOW 26,433 lbs\nMLW 25,794 lbs\nZFW 20,610 lbs\nPower: 1800 shp PW118A\nTakeoff Power: 1980 shp\nStall Speeds: 120\/89 kts\nMmo\/Mo: 0.52M\/250kts\nRange: 1570nm + reserve\nEconomic cruise 270kts FL250\nMax cruise 310kts atc_type=EMBRAER atc_model= [WEIGHT_AND_BALANCE] reference_datum_position = 0.000,0.000,0.000 empty_weight_CG_position = 0.000,0.000,0.000 empty_weight_roll_MOI = 213440.0 empty_weight_pitch_MOI = 168681.0 empty_weight_yaw_MOI = 244114.0 empty_weight_coupled_MOI = 1300.0 empty_weight = 16507.0 max_number_of_stations = 13 // weight Fore/Aft Lft/Rt Up/Dn station_load.0 = 400, 19.000, 0.000, 3.000 //pilots station_load.1 = 200, 16.000, -1.650, 3.000 //flight attendant // PAYLOAD FOLLOWS // MAX PAYLOAD 6313 lb // MAX PAYLOAD WITH FULL FUEL 3992 lb station_load.2 = 170, 11.500, 0.000, 3.000 //Row 1 - 2 Pax station_load.3 = 340, 9.000, 0.000, 3.000 //Row 2 - 3 Pax station_load.4 = 340, 6.500, 0.000, 3.000 //Row 3 - 3 Pax station_load.5 = 340, 4.000, 0.000, 3.000 //Row 4 - 3 Pax station_load.6 = 340, 1.200, 0.000, 3.000 //Row 5 - 3 Pax station_load.7 = 340, -1.500, 0.000, 3.000 //Row 6 - 3 Pax station_load.8 = 340, -4.000, 0.000, 3.000 //Row 7 - 3 Pax station_load.9 = 340, -8.300, 0.000, 3.000 //Row 8 - 3 Pax station_load.10 = 340, -10.800, 0.000, 3.000 //Row 9 - 3 Pax station_load.11 = 340, -13.500, 0.000, 3.000 //Row 10 - 4 Pax station_load.12 = 520, -19.000, 0.000, 3.000 //baggage // ZFW = 16507 lb + // Fuel = 5906 lb + // Payload = 3750 lb = // TOTAL = 26163 lb CAN NOT BE MORE THAN 26609 lb MAX RAMP WEIGHT [fuel] // MGTOW FUEL QUANTITY = 440.7 gal per tank 5906lb total // MAX PAYLOAD FUEL QUANTITY = 192.4 gal per tank 2579lb total LeftMain = 0.000, -14.500, -1.000, 440.7, 3.0 RightMain = 0.000, 14.500, -1.000, 440.7, 3.0 fuel_type = 2 number_of_tank_selectors = 1 //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, 25.738, 0.000, -3.991, 2500.0, 0, 0.696, 45.0, 0.75, 1.667, 0.850, 6.0, 7.5, 0.000, 250, 275 point.1=1, -2.000, -10.000, -4.500, 2500.0, 1, 1.064, 0.0, 1.00, 2.000, 0.700, 8.0, 8.0, 2.000, 250, 275 point.2=1, -2.000, 10.000, -4.500, 2500.0, 2, 1.064, 0.0, 1.00, 2.000, 0.700, 7.0, 7.0, 3.000, 250, 275 point.3=2, 1.152, -32.500, 3.845, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 5.000, 000, 000 point.4=2, 1.152, 32.500, 3.845, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 6.000, 000, 000 point.5=2, -30.340, 0.000, 4.700, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 9.000, 000, 000 point.6=2, 30.300, 0.000, 1.200, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 4.000, 000, 000 static_pitch=-1.000 static_cg_height=4.334 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 3.09, -31.90, 3.79, fx_navred , light.1 = 3, 3.09, 31.90, 3.79, fx_navgre , light.2 = 3, -36.05, 0.00, 15.37, fx_navwhi , light.3 = 2, 3.02, -32.21, 3.79, fx_strobe , light.4 = 2, 3.02, 32.21, 3.79, fx_strobe , light.5 = 2, -36.05, 0.00, 15.37, fx_strobe , light.6 = 1, -0.29, 0.00, 7.85, fx_beacon , light.7 = 1, 3.22, 0.00, -0.50, fx_beacon , light.8 = 4, 17.92, 0.00, 5.26, fx_vclight, [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [Flaps.0] type = 1 span-outboard = 0.500 extending-time = 13.000 system_type = 0 damaging-speed = 250.0 blowout-speed = 300.0 lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar = 1.0 flaps-position.0= 0.0 flaps-position.1= 15.0 flaps-position.2= 25.0 flaps-position.3= 45.0 [flight_tuning] cruise_lift_scalar = 1.000 pitch_stability = 1.500 roll_stability = 1.000 yaw_stability = 1.000 parasite_drag_scalar = 0.850 induced_drag_scalar = 0.850 elevator_effectiveness = 0.750 aileron_effectiveness = 0.925 rudder_effectiveness = 0.850 elevator_trim_effectiveness = 1.200 aileron_trim_effectiveness = 1.000 rudder_trim_effectiveness = 1.000 [airplane_geometry] wing_area = 425.000000 wing_span = 64.833333 wing_root_chord = 6.583333 wing_dihedral = 6.300659 wing_incidence = 1.299756 wing_twist = 1.499634 oswald_efficiency_factor = 0.909222 wing_winglets_flag = 0 wing_sweep = 0.000000 wing_pos_apex_lon = 0.000000 wing_pos_apex_vert = 0.000000 htail_area = 105.000000 htail_span = 22.000000 htail_pos_lon = -32.000000 htail_pos_vert = 0.000000 htail_incidence = 0.000000 htail_sweep = 0.000000 vtail_area = 89.000000 vtail_span = 10.756393 vtail_sweep = 0.000000 vtail_pos_lon = -30.833333 vtail_pos_vert = 5.833333 elevator_area = 26.250000 aileron_area = 17.000000 rudder_area = 15.130000 elevator_up_limit = 27.501974 elevator_down_limit = 20.626481 aileron_up_limit = 19.480565 aileron_down_limit = 14.896903 rudder_limit = 23.491270 elevator_trim_limit = 19.480565 spoiler_limit = 0.000000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000000 min_ailerons_for_spoilerons = 0.000000 min_flaps_for_spoilerons = 0.000000 [GeneralEngineData] engine_type = 5 Engine.0 = 8.833, -13.583, 0.000 Engine.1 = 8.833, 13.583, 0.000 fuel_flow_scalar = 0.75 [TurbineEngineData] fuel_flow_gain = 0.009 inlet_area = 1.0 rated_N2_rpm = 33300 static_thrust = 230 afterburner_available = 0 [propeller] thrust_scalar = 1.0 propeller_type = 0 propeller_diameter = 10.6 propeller_blades = 4 propeller_moi = 30 beta_max = 45.0 beta_min = 15.0 min_gov_rpm = 16653 prop_tc = 0.004 gear_reduction_ratio = 25.62 fixed_pitch_beta = 0 low_speed_theory_limit = 80 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 1 min_rpm_for_feather = 600 beta_feather = 79.2 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 1 minimum_on_ground_beta = 1.0 minimum_reverse_beta = -15.0 [turboprop_engine] power_scalar = 1.0 maximum_torque = 7272 [Reference Speeds] flaps_up_stall_speed = 120.000000 full_flaps_stall_speed = 96.000000 cruise_speed = 359.547707 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [Views] eyepoint = 0.00, -1.70, 5.77 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 1000.000000 autothrottle_available = 1 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 0 autothrottle_max_rpm = 90.000000 pitch_takeoff_ga = 8.000000 [direction_indicators] direction_indicator.0 = 3,0 [pitot_static] vertical_speed_time_constant = 150 [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