[fltsim.0] title=Boeing 757-200 (RR) sim=b757-200 model= panel= sound= texture= kb_checklists=b757-200_check kb_reference=b757-200_ref atc_id= atc_id_color=0xffffffff atc_airline=UPS atc_flight_number=275 ui_manufacturer=Boeing ui_type=757-200 Cargo ui_variation=UPS Air Cargo, United Parcel Service visual_damage=1 description=United Parcel Service, Boeing 757-200. \n\nBoeing launched development of the 757 in March 1979 following orders from British Airways and Eastern Airlines. Developed in tandem with the larger widebody 767, the two share a number of systems and technologies, including an early generation EFIS flightdeck. \n\nAfter almost three years in development, the Boeing 757-200 first soared to the air on February 19th, 1982. Eastern took delivery of the first Boieng 757-200 on December 22nd, 1982, and then entered it into service on January 1st, 1983. \n\nGMAX model by Mike Stone, authentic textures by Kevin Stewart. atc_heavy=0 [General] atc_type=BOEING atc_model=B752 editable=0 performance=Max cruising speed 493kts (914km/h), economical cruising speed 460kts (850km/h). \n\nRange with P&W engines and 186 passengers 2728nm (5053km), with RR engines 2569nm (4758km). \n\nRange at optional max takeoff weight with P&W engines 3929nm (7277km), with RR engines 3719nm (6888km). \n\n757-200PF - Speeds same. \n\nRange with maximum payload and P&W engines 3885nm (7195km), with RR engines 3700nm (6857km). [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] reference_datum_position=0.000,0.000,0.000 empty_weight_CG_position=0.000,0.000,0.000 max_number_of_stations=50 station_load.0=39083.000,0.000,0.000,0.000 max_gross_weight=255000.000 empty_weight=128730.000 ;Moments of Inertia empty_weight_pitch_MOI=3515230.840 empty_weight_roll_MOI=942525.124 empty_weight_yaw_MOI=4075745.891 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.175 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=0.775 induced_drag_scalar=0.975 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [SMOKESYSTEM] smoke.0=90.0,-27.3,-61.0, fx_WingVortex smoke.1=90.0,-27.3,-48.0, fx_WingVortex smoke.2=90.0,-27.3,48.0, fx_WingVortex smoke.3=90.0,-27.3,61.0, fx_WingVortex [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 [TurbineEngineData] fuel_flow_gain=0.004340 inlet_area=48.103440 rated_N2_rpm=29920.000 static_thrust=40150.000 afterburner_available=0 reverser_available=1 [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=0.000 static_cg_height=10.750 [Views] eyepoint=43.75,-1.35,3.75 //(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, -84.10, 0.00, 6.34, 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=2000.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=95.000 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8.000 use_no_default_pitch=0 use_no_default_bank=1 [fuel] Center1=0.000, 0.000, 0.000, 4650.000, 0.000 //Capacity: 11,526 U.S. Gallons LeftMain=-3.000, -19.000, 0.000, 3438.000, 0.000 RightMain=-3.000, 19.000, 0.000, 3438.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=1998.000 wing_span=124.833 wing_root_chord=16.000 wing_dihedral=4.998 wing_incidence=-1.000 wing_twist=1.000 oswald_efficiency_factor=0.753 wing_winglets_flag=0 wing_sweep=25.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=676.000 htail_span=49.916 htail_pos_lon=-65.000 htail_pos_vert=4.000 htail_incidence=0.000 htail_sweep=30.000 vtail_area=495.000 vtail_span=25.367 vtail_sweep=35.000 vtail_pos_lon=-60.000 vtail_pos_vert=5.833 elevator_area=169.250 aileron_area=79.720 rudder_area=84.150 elevator_up_limit=27.501 elevator_down_limit=20.626 aileron_up_limit=19.480 aileron_down_limit=14.896 rudder_limit=23.491 elevator_trim_limit=19.480 spoiler_limit=59.998 spoilerons_available=1 aileron_to_spoileron_gain=1.500 min_ailerons_for_spoilerons=5.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=133.000000 full_flaps_stall_speed=106.400000 cruise_speed=492.678215 [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 [Flaps.0] type=1 span-outboard=0.300 extending-time=20.000 system_type=1 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.500 drag_scalar=0.500 pitch_scalar=0.500 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=20.000 system_type=1 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.400 drag_scalar=0.400 pitch_scalar=0.400 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=3.000 system_type=1 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.100 drag_scalar=0.100 pitch_scalar=0.100 flaps-position.0=0.000, 0.000 flaps-position.1=8.000, 0.000
