[fltsim.0] title=Boeing 757-200 (RR) Privilege sim=b757-200 model= panel= sound= texture= panel_alias= sound_alias= kb_checklists= kb_reference= atc_id=EC-EFX atc_id_color=0xffffffff atc_airline=Hola Airlines atc_flight_number=0001 ui_manufacturer=Boeing ui_type=757-200 ui_variation=Privilege description=The Boeing 757-200, is a twin-engined, medium-to-long-range jetliner incorporating advanced technology through the use of lightweight composite materials and improved wing design.\nModel by Mike Stone, Repaint by Alejandro Hurtado. atc_heavy=0 [General] atc_type=BOEING AIRCRAFT atc_model=B752 editable=1 performance=Cruise Speed\t.80 - .84 Mach\nNever Exceed .86 Mach\nMaximum Range\t3,960 nm\nMTOW 255,500 lb\nSeating\t\t192 to 239\nCargo Capacity\t1,670 CU ft\n [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight=220000.000 empty_weight=125750.000 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=15000000.000 empty_weight_roll_MOI=2000000.000 empty_weight_yaw_MOI=6000000.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=2.001 induced_drag_scalar=2.001 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=2.002 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=0.504 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type=1 Engine.0=0.000, -22.000, -6.000 Engine.1=0.000, 22.000, -6.000 fuel_flow_scalar=1.000 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=24.000 rated_N2_rpm=29920.000 static_thrust=37400.000 afterburner_available=0 reverser_available=1.000 [jet_engine] thrust_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, 40.000, 0.000, -12.300, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1=1.000, -7.750, -8.580, -12.800, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 point.2=1.000, -7.750, 8.580, -12.800, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 point.3=2.000, -14.170, -47.330, -10.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -54.000, 0.000, 2.830, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points=21 static_pitch=0.620 static_cg_height=11.500 gear_system_type=0 [Views] eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [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, 5=landing light.0=3, -24.31, -62.04, 3.97, fx_navredm , light.1=3, -24.31, 62.04, 3.97, fx_navgrem , light.2=3, -86.15, 0.00, 6.30, fx_navwhih , light.3=2, -21.59, -61.95, 4.00, fx_strobeh , light.4=2, -21.59, 61.95, 4.00, fx_strobeh , light.5=1, 5.38, 0.00, -6.21, fx_beaconb , light.6=1, 29.30, 0.00, 9.79, fx_beaconh , light.7=4, 61.43, 0.00, 5.36, fx_vclight , [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 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [EFFECTS] wake=fx_wake_ss //water=fx_spray water=fx_waterland dirt=fx_tchdrt concrete=fx_sparks ;touchdown=fx_tchdwn_s, 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=0.000000 [fuel] Center1=0.000, 0.000, 0.000, 5000.000, 0.000 LeftMain=-3.000, -19.000, 0.000, 3600.000, 0.000 RightMain=-3.000, 19.000, 0.000, 3600.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=1994.000 wing_span=124.000 wing_root_chord=25.000 wing_dihedral=5.000 wing_incidence=-1.000 wing_twist=-1.000 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=600.000 htail_span=52.000 htail_pos_lon=-70.000 htail_pos_vert=4.000 htail_incidence=0.000 htail_sweep=30.000 vtail_area=360.000 vtail_span=24.000 vtail_sweep=35.000 vtail_pos_lon=-70.000 vtail_pos_vert=10.000 elevator_area=84.000 aileron_area=28.000 rudder_area=120.000 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=3.000 min_ailerons_for_spoilerons=10.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=142.000 full_flaps_stall_speed=113.000 cruise_speed=460.000 max_indicated_speed=493.000000 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 [brakes] toe_brakes_scale=0.885037 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type=1 span-outboard=0.300 extending-time=8.000 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-position.2=5.000, 0.000 flaps-position.3=15.000, 0.000 flaps-position.4=20.000, 0.000 flaps-position.5=25.000, 0.000 flaps-position.6=30.000, 0.000 [Flaps.1] type=1 span-outboard=0.400 extending-time=8.000 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-position.2=5.000, 0.000 flaps-position.3=15.000, 0.000 flaps-position.4=20.000, 0.000 flaps-position.5=25.000, 0.000 flaps-position.6=30.000, 0.000 [Flaps.2] 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