// BAE146-100 For FSX, Version 19, September 2010 // FSDS model, panel design, XML gauge design by Jean-Pierre Brisard // FD and Master Textures by Bob May // Copyright 2011 - Premier Aircraft Design [fltsim.0] title=BAE1461_United sim=bae146-100 model=100 panel=BAE1461_x sound=0 texture=united_gray kb_checklists=bae146_check kb_reference=bae146_ref atc_id=N683AW atc_airline=united atc_flight_number=2413 atc_heavy=0 atc_parking_types=ramp, gate ui_manufacturer=British Aerospace ui_type=BAE146-100 ui_variation=United Express (Historical gray) description=The BAe 146 is a medium-sized commercial aircraft which was manufactured in the United Kingdom by British Aerospace (which later became part of BAE Systems). Production ran from 1983 until 2002. Manufacture of the improved version known as the Avro RJ began in 1992.The BAe 146/Avro RJ is a high-wing cantilever monoplane with a T-tail. It has four turbofan jet engines mounted on pylons underneath the wings, and has retractable tricycle landing gear. The aircraft has very quiet operation, and has been marketed under the name Whisperjet. It sees wide usage at small city-based airports. In its primary role it serves as a regional jet, short-haul airliner or regional airliner. The BAe 146/Avro RJ is in wide use among European airlines, such as Brussels Airlines, Swiss International Air Lines and Lufthansa. The freight-carrying version has the designation "QT" (Quiet Trader), while a convertible version is designated "QC". The BAe 146 comes in -100, -200 and -300 models. The equivalent Avro RJ versions are designated RJ70, RJ85, and RJ100. [General] atc_type=BRITISHAEROSPACE atc_model=BA46 editable=1 performance="Cruise Speed \n432 kts TAS 520 mph 885 km\/h\n\nEngines \n4 x Textron Lycoming ALF 502R-5 Turbofans\n\nMaximum Range \n1808 nm \n\nService Ceiling \n33, 089 ft \ category=airplane [Views] eyepoint = 23.00,-1.6,-3.5 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight =93000.0 empty_weight =42684.00000 reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -2.000, -0.000, -0.000 max_number_of_stations =3 ;Moments of Inertia empty_weight_roll_MOI =208369.45000 empty_weight_pitch_MOI =582071.04000 empty_weight_yaw_MOI =557909.19000 empty_weight_coupled_MOI =0.00000 station_load.0= 180, -0.000, -2.000, 8.000, Pilot station_load.1= 180, -0.000, 2.000, 8.000, Co-pilot station_load.2= 9000, -14.000, 0.000, -10.000, Pass/luggage [fuel] LeftMain = -0.000, -8.000, -4.000, 750.000, 0.000 RightMain = -0.000, 8.000, -4.000, 750.000, 0.000 Center1 = -0.000, 0.000, -7.000, 1500.000, 0.000 fuel_type =2 number_of_tank_selectors =1 electric_pump=1 fuel_dump_rate=0.02000 anemometer_pump=0 manual_pump=0 engine_driven_pump=0 [airplane_geometry] wing_area =932.00000 wing_span =86.00000 wing_root_chord =11.38000 wing_dihedral =-3.00000 wing_incidence =3.00000 wing_twist =-0.30000 oswald_efficiency_factor=0.78600 wing_winglets_flag =0 wing_sweep =37.50000 wing_pos_apex_lon =12.93364 wing_pos_apex_vert =0.00000 htail_area =153.82000 htail_span =32.75000 htail_pos_lon =-45.29000 htail_pos_vert =0.00000 htail_incidence =0.00000 htail_sweep =30.00000 vtail_area =131.54000 vtail_span =15.26000 vtail_sweep =30.00000 vtail_pos_lon =-43.18000 vtail_pos_vert =2.42000 elevator_area =57.50000 aileron_area =59.90000 rudder_area =39.17000 elevator_up_limit =25.00000 elevator_down_limit =25.00000 aileron_up_limit =20.00000 aileron_down_limit =20.00000 rudder_limit =30.00000 elevator_trim_limit =20.00000 spoiler_limit =45.00000 spoilerons_available =0 aileron_to_spoileron_gain =3.00000 min_ailerons_for_spoilerons =10.00000 min_flaps_for_spoilerons =0.00000 spoiler_extension_time=4.00000 spoiler_handle_available=1 auto_spoiler_available=0 positive_g_limit_flaps_up=3.70000 negative_g_limit_flaps_up=-2.96000 positive_g_limit_flaps_down=2.59000 negative_g_limit_flaps_down=-2.22000 load_safety_factor=1.00000 [Reference Speeds] flaps_up_stall_speed = 140.0 //Knots True (KTAS) full_flaps_stall_speed = 112.0 //Knots True (KTAS) cruise_speed =504.96229 max_mach =0.92000 max_indicated_speed =364.97016 [flaps.0] type= 1 system_type=1 span-outboard= 0.800 extending-time= 10.0 damaging-speed=300.0 blowout-speed=350.0 flaps-position.0=0.00 flaps-position.1=18.00 flaps-position.2=24.00 flaps-position.3=30.00 flaps-position.4=33.00 lift_scalar=1.00 drag_scalar=1.00 pitch_scalar=1.00 [flaps.1] type= 1 system_type=1 span-outboard= 0.800 extending-time= 5.0 damaging-speed=300.0 blowout-speed=350.0 flaps-position.0=0.00 flaps-position.2=5.00 flaps-position.3=10.00 flaps-position.4=15.00 lift_scalar=1.00 drag_scalar=1.00 pitch_scalar=1.00 [flight_tuning] cruise_lift_scalar =1.00000 parasite_drag_scalar =1.30000 induced_drag_scalar =1.40000 elevator_effectiveness =1.10000 aileron_effectiveness =1.00000 rudder_effectiveness =1.00000 pitch_stability =1.40000 roll_stability =1.00000 yaw_stability =1.00000 elevator_trim_effectiveness =1.00000 aileron_trim_effectiveness =1.00000 rudder_trim_effectiveness =1.00000 hi_alpha_on_roll=1.00000 hi_alpha_on_yaw=1.00000 p_factor_on_yaw=0.00000 torque_on_roll=0.00000 gyro_precession_on_roll=0.00000 gyro_precession_on_yaw=0.00000 [GeneralEngineData] engine_type =1 Engine.0 =2.000, -29.500, -0.000 Engine.1 =2.000, -18.900, -0.000 Engine.2 =2.000, 18.900, -0.000 Engine.3 =2.000, 29.500, -0.000 fuel_flow_scalar =1.00000 min_throttle_limit =-0.35000 [TurbineEngineData] fuel_flow_gain =0.00200 inlet_area =3.48500 rated_N2_rpm =29920.00000 static_thrust =6970.00000 afterburner_available =0 reverser_available =0 afterburner_throttle_threshold=0.00000 ThrustSpecificFuelConsumption=0.40000 AfterBurnThrustSpecificFuelConsumption=0.00000 [jet_engine] thrust_scalar =1.25000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm =90 autothrottle_takeoff_ga=1 pitch_takeoff_ga =8 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 max_throttle_rate=0.1 nav_proportional_control=12 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=25 gs_integrator_control=0.53 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 yaw_damper_gain =1 use_no_default_bank=1 use_no_default_pitch=1 default_pitch_mode=0 default_bank_mode=0 [contact_points] //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) static_pitch = -0.000 static_cg_height = 12.900 gear_system_type=0 max_number_of_points=10 tailwheel_lock=0 point.0= 1, 26.950, 0.000, -13.130, 3000, 0, 2.000, 70.000, 0.296, 2.5, 0.9516, 9.000, 8.000, 0, 219.9, 250.3 point.1= 1, -5.440, -8.700, -13.620, 4000, 1, 2.000, 0.000, 1.000, 2.500, 0.900, 11.000, 9.000, 2, 219.9, 250.3 point.2= 1, -5.440, 8.700, -13.620, 4000, 2, 2.000, 0.000, 1.000, 2.500, 0.900, 11.000, 9.000, 3, 219.9, 250.3 point.3= 2, 45.000, 0.000, 0.000, 2000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.4= 2, -15.000, 43.500, 0.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.5= 2, -15.000, -43.000, 0.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.6= 2, -55.000, 0.000, 18.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 point.7= 2, 0.000, 0.000, 8.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0 point.8= 2, 0.000, 0.000, -8.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0 point.9= 5, -1.000, 0.000, -1.333, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 [gear_warning_system] gear_warning_available =1 pct_throttle_limit =0.10000 flap_limit_idle =5.00000 flap_limit_power =25.50000 [brakes] parking_brake =1 toe_brakes_scale =1.24000 auto_brakes=1 hydraulic_system_scalar=0.00000 differential_braking_scale=0.20000 [hydraulic_system] normal_pressure =3000.00000 electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 7=recognition light.0 =3, -8.25, -43.70000, -2.6, fx_navred light.1 =3, -8.25, 43.70000,-2.6, fx_navgre light.2 =3, -45.020, 0.000, -2.500, fx_navwhi light.3 =2, -8.800000, -43.8, -2.6, fx_strobeh light.4 =2, -8.800000, 43.8,-2.6, fx_strobeh light.5 =1, -43.5000, 0.000000, 13.500, fx_beaconh light.6= 3, 5.750, -3.260, -0.750, fx_navwhi light.7= 3, 5.750, 3.260, -0.750, fx_navwhi [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [TailHook] tailhook_length= 4.000 tailhook_position = -15.000, 0.000, -1.000 cable_force_adjust = 1.0 [exits] number_of_exits = 2 exit_rate.0 = 0.1 ;Percent per second exit_rate.1 = 0.1 ;Percent per second [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=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1 crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111 [stall_warning] type=2 stick_shaker=1 [GPWS] max_warning_height=0 sink_rate_fpm=-1500 excessive_sink_rate_fpm=-2000 climbout_sink_rate_fpm=-100 flap_and_gear_sink_rate_fpm=-100 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=0