[fltsim.0]
title=Boeing 757-200 (PW)
sim=b757-200
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=N67IIM
atc_id_color=0xffffffff
atc_airline=Delta
atc_flight_number=587
ui_manufacturer=Boeing
ui_type=757-200
ui_variation=Delta
description=After a slow sales start, the medium range single aisle 757 has become yet another sales success story for Boeing. Boeing considered a number of proposals for a successor to the 727 trijet during the 1970s, with many of these designs featuring the nose and Ttail of the earlier jet. It was not until later in that decade however that Boeing settled on a more conventional design featuring the same cross section as the 727 (not to mention the 737, 707 and 720) but with the fuselage considerably longer in length, an all new wing, nose and flightdeck and fuel efficient high bypass turbofan engines. Boeing launched development of the 757 in March 1979 following orders from British Airways and Eastern. Developed in tandem with the larger widebody 767 the two types share a number of systems and technologies, including a common early generation EFIS flightdeck. First flight was on February 19 1982 and the 757 entered service in January the following year. Subsequent versions to appear are the 757-200PF Package Freighter, a pure freighter, and the 757-200M Combi (only one has been built). The standard passenger aircraft is designated the 757-200, there being no 100. The stretched 757-300 is described separately. Initial sales of the 757 were fairly slow, however orders picked up significantly in the mid to late 1980s as traffic on routes previously served by smaller 727s and 737s grew to require the 757's extra capacity. Today 757 sales comfortably exceed those of the 767, a position that was reversed until the late 1980s.
atc_heavy=0
[General]
atc_type=BOEING AIRCRAFT
atc_model=B752
editable=1
performance=Max cruising speed 914km/h (493kt), economical cruising speed 850km/h (460kt). Range with P&W engines and 186 passengers 5053km (2728nm), with RR engines 4758km (2569nm). Range at optional max takeoff weight with P&W engines 7277km (3929nm), with RR engines 6888km (3719nm). 757-200PF - Speeds same. Range with 22,680kg payload and P&W engines 7195km (3885nm), with RR engines 6857km (3700nm).
[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
station_load.0 = 19000.000, 0.000, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 10000000.000
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
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
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 =0.502
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
[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
[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
[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;
[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
[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 = -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 = 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 = 477.000
[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= 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
