[fltsim.0] title=Embraer 170 BA Cityflyer sim=embraer170 model= panel= sound= texture=bacity kb_checklists= description=Embraer 170 \n\nEngine Type: General Electric CF34-8E\n\nModel Designer\n Carl Selin\n\nTexture Designer\n Tommy Hansson\n\nFlight Dynamics\n John Cillis\n\nSound\n Albert Ramic\n\nTest flown by Dream Wings mebmbers\n ui_manufacturer=Embraer ui_type=170 ui_variation=BA Cityflyer ui_typerole=Regional Jet ui_createdby=Dreamwings atc_heavy=0 atc_id=G-LCYD atc_airline=FLYER atc_flight_number=3497 [General] performance=Maximum Cruise Speed: mach 0.80, Passangers: 70, Range: 2000 nm atc_type=EMBRAER atc_model=E-170 editable=1 Category=airplane [pitot_static] vertical_speed_time_constant=1 pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight=82012.000 empty_weight=46165.000 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=8 //Weight-Fore/AFT-Right/Left-Up/Down //Cabin station_load.0=2096.000000,20.000000,-3.000000,4.000000 //FWD Left station_load.1=2096.000000,20.000000,3.000000,4.000000 //FWD Right station_load.2=2096.000000,0.000000,-3.000000,4.000000 //Center Left station_load.3=2096.000000,0.000000,3.000000,4.000000 //Center Right station_load.4=2096.000000,-15.000000,-3.000000,4.000000 //Rear Left station_load.5=2096.000000,-15.000000,3.000000,4.000000 //Rear Right //Baggage Cmpt station_load.6=1194.000000,20.000000,0.000000,-2.000000 //FWD station_load.7=1194.000000,-15.000000,0.000000,-2.000000 //Rear ;Moments of Inertia empty_weight_pitch_MOI=2172439.000 empty_weight_roll_MOI=2262183.000 empty_weight_yaw_MOI=2337024.000 empty_weight_coupled_MOI=1300.000 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=2.000 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=1 Engine.0=4.750, -16.100, -2.500 Engine.1=4.750, 16.100, -2.500 fuel_flow_scalar=1.000000 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002000 inlet_area=17.75 static_thrust=14200.000000 afterburner_available=0 reverser_available=1 rated_N2_rpm=29920.000000 [jet_engine] thrust_scalar=1.000 [electrical] 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 [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 point.0= 1.000, 36.500, 0.000, -10.200, 1574.000, 0.000, 1.500, 56.000, 0.355, 2.500, 0.595, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, -4.000, -10.000, -10.300, 1574.000, 1.000, 1.500, 0.000, 0.355, 2.500, 0.595, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -4.000, 10.000, -10.300, 1574.000, 2.000, 1.500, 0.000, 0.355, 2.500, 0.595, 5.000, 5.000, 3.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=9.796 gear_system_type=1 [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=5.0 //Flap angle that activates warning at idle flap_limit_power=25.5 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=0.885 //Brake scalar auto_brakes=4 [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,0,0 //pumps on Eng1,2 [Flaps.0] type=1 span-outboard=0.800 extending-time=20.000 system_type=1 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=5.000, 0.000 flaps-position.2=10.000, 0.000 flaps-position.3=20.000, 0.000 flaps-position.4=35.000, 0.000 [Flaps.1] type=2 span-outboard=0.800 extending-time=2.000 system_type=1 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=1.000, 0.000 [Flaps.2] type=2 span-outboard=0.800 extending-time=3.000 system_type=1 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=0.500, 0.000 flaps-position.2=1.000, 0.000 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=4, 42.5, 0.00, 1.7, fx_vclighth , light.1=2, -48.50, 0.00, 2.80, fx_strobeh , light.2=2, 10.35, 0.00, -6.15, fx_beaconb , light.3=1, 21.65, 0.00, 5.9, fx_beaconh [Views] eyepoint=40, -1.31, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum [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 [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=0,0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.1 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [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=10.000000 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=1.0 use_no_default_pitch=1 default_pitch_mode=0 [fuel] Center1=0.000, 0.000, 0.000, 1317.000, 0.000 LeftMain=-3.000, -19.000, 0.000, 900.000, 0.000 RightMain=-3.000, 19.000, 0.000, 900.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=750.000 wing_span=85.750 wing_root_chord=16.000 wing_dihedral=6.200 wing_incidence=1.000 wing_twist=-0.500 oswald_efficiency_factor=0.750 wing_winglets_flag=0 wing_sweep=25.000 wing_pos_apex_lon=8.000 wing_pos_apex_vert=0.000 htail_area=260.000 htail_span=32.700 htail_pos_lon=-35.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=30.000 vtail_area=150.000 vtail_span=17.000 vtail_sweep=35.000 vtail_pos_lon=-35.800 vtail_pos_vert=5.800 elevator_area=70.500 aileron_area=26.900 rudder_area=56.200 elevator_up_limit=22.500 elevator_down_limit=19.500 aileron_up_limit=20.000 aileron_down_limit=20.000 rudder_limit=26.000 elevator_trim_limit=20.000 spoiler_limit=60.000 spoilerons_available=1 aileron_to_spoileron_gain=.5 min_ailerons_for_spoilerons=10.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed=142.000 full_flaps_stall_speed=113.000 cruise_speed=477.000 max_indicated_speed=340.000000 max_mach=0.820020 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
